Magnetic non-contact transport system

Abstract: A magnetic track positioning type magnetic levitation transport system which transports without contact a large variety of ferromagnetic objects without impairing the expandability of the track. The track is composed of unit support components ( 3 ), unit propulsion components ( 5 ) and unit guidance components ( 7 ). In unit support components ( 3 ), multiple magnetic support units ( 15 ) are mounted so that they are vertically moveable. Attraction control device ( 19 ) performs levitation control which contributes to the vertical movement of the centre of gravity of the part of steel plate ( X ) overlapping unit support component ( 3 ) and levitation control which contributes to the rolling of the same part of steel plate ( X ). The height of steel plate ( X ) is maintained at a specified position by controlling height adjustment mechanisms with height control system ( 53 ). Stabilization of the pitching of steel plate ( X ) is designed using coil springs ( 47 ) and dampers ( 49 ) which are provided in unit support components ( 3 ). Movement and at the same time, decrease of yawing of steel plate ( X ) is caused by unit propulsion component ( 5 ). Guidance of steel plate ( X ) in the left and right directions is performed by unit guidance component ( 7 ).

Description: BACKGROUND OF THE INVENTION 1. FIELD OF THE INVENTION This invention concerns a magnetic track positioning type magnetic levitation transport system which performs non-contact transport of objects to be transported by attraction type magnetic levitation; the objects to be transported being made of ferromagnetic bodies such as steel plate. 2. DESCRIPTION OF THE PRIOR ART For example, when transporting steel plate between steel plate processing equipment in the cold rolling process at a steel works, normally, a transport method using a roller track, in which multiple rollers are arranged in the direction of transport, is adopted. Also, in steel plate press processing at car plants and the like, generally, a transport method is adopted in which the steel plates to be pressed are transported to the pressing equipment using bogies or cranes. However, with the method using roller tracks, if there is any dirt, etc. on the rollers, the surface of the steel plate which the track transports is liable to be scratched. Thus, there is a risk of significant reduction of the product quality. For this reason, the rollers must always be serviced so that dirt and the like does not adhere to the rollers. Thus, there is the problem of requiring large amounts of labour and cost. Also, with the bogie or crane methods, there are the problems that, not only is the steel plate liable to scratching when loading or unloading, but also a great deal of time is expended on the movement. Therefore, currently, various systems are under development to resolve problems such as these. A system for the non-contact support of steel plate has been developed (Nikkei Mekanikaru, 12 June, 1989). In this, for instance, multiple electromagnets are laid in a track and these electromagnets are successively excited where the end of the steel plate, which moves along a track beneath the electromagnets, approaches the electromagnets. Here, the attraction of the electromagnets is used for supporting the weight of the steel plate and for imparting thrust to the steel plate. At the same time, adsorption of the steel plate to the electromagnets is prevented by jetting air on the steel plate from compressed air passages provided between the electromagnets and the steel plate. Also, a study on the support of thin steel plate by 4 electromagnets (Denki Gakkai Sangyo Oyo Bumon, Zenkoku Taikai Yokoshu, July 1989, p915) and the development of a system which guides steel plate without contact using specially shaped electromagnets (Japan Laid-Open Patent Gazette : Laid-Open Patent No. Heisei 2-270739) are in progress. However, with these techniques, the systems are complex, and the range of dimensions and weights of steel plate which can be transported is restricted. Also, it is presumed that the transporting of various weights and types of steel plate over long distances will be difficult. As described above, when transporting steel plate withot any scratching with devices which use mechanical contact, large amounts of labour and time are required for maintenace, shock prevention during transport, etc. Also, with prior art non-contact transport devices, there are problems such as that the dimensions and weights of transportable steel plates are limited, the systems are complex and performance of long-distance transport is difficult. DE-A-43 41 661 discloses a magnetic levitation system comprising magnet assemblies 31a-d including electromagnets 51, 52, a frame 25 for mounting the magnet units, a magnetic support control device 14A, 14B, 45a and 45b which controls the attraction of the elctromagnets of the magnet units for non-contact support of the transported object 15 fastened to the frame 25, an inclination device formed by the combination of the four magnet assemblies 31a-d disposed at each corner of the moving part of the system and a control device 41 for the inclination device. SUMMARY OF THE INVENTION Therefore, the aim of this invention is to provide a magnetic track positioning type magnetic levitation transport system which can transport various objects to be transported made of magnetic materials over long distances, and in which the transport line can be easily constructed. Accordingly the present invention provides a magnetic levitation transport system including a track with a magnetic force support system which is arranged to support the object to be transported without contact, the object having a flat, possibly slightly curved upper surface and at least partly comprising a ferromagnetic substance, the system comprising: multiple fixed support units arranged along the direction of transport, each support unit including a track frame; and magnetic assemblies including electro-magnets which are positioned in each track frame and extend in a direction orthogonal to the direction of transport and constitute means for supporting, transporting, and guiding the object; characterised by: mounting devices for the magnetic assemblies which permit movement in the vertical direction, and an attraction control device which is arranged to perform levitation control for both pitching and rolling motion of the object to be transported by moving each of the magnetic assemblies on its mounting device only when the object to be transported is below that assembly. The invention also extends to a magnetic levitation system for an object at least part of which comprises a ferromagnetic substance and having a flat, possibly slightly curved upper surface, the system comprising: a transporter which is movable along a track; magnet assemblies including electromagnets mounted on the transporter by support means; a magnetic support control device which controls the attraction of the electromagnets of the magnet assemblies for non-contact support of the object; characterised by: an inclination device which controls pitching and rolling of the object to be transported by changing the angular position of the support means; and a control device including sensors for the inclination device. When using this invention, levitation control on the perpendicular movement of the object to be transported and levitation control on rolling are performed at every unit supporting component. Also, it is possible to inhibit the pitching of the object to be transported between the unit supporting components by the magnetic support units being vertically moveable using the mounting device. For this reason, stable levitation can be performed by inhibiting the vertical movement and rolling of the object to be transported at every unit supporting component, even if, not only the whole length, but also the whole width, of the object to be transported varies. Also, pitching of the object to be transported can be inhibited by the mounting device. Therefore, non-contact support of the whole object to be transported is possible. Moreover, even when the weight and the inertial moment of the object to be transported differ, this difference is distributed to each unit supporting component. Thus, as a magnetic track positioning type magnetic levitation transport system as a whole which is formed of collection of individual unit supporting components, non-contact support is possible for objects to be transported which have a greater range of weights and inertial moments. Also, non-contact transport is possible for multiple objects to be transported by one track. Moreover, in a magnetic track positioning type magnetic levitation transport system in which a track provided with a magnetic support system is positioned along the transport route of the objects to be transported, and is designed for the non-contact transport of objects to be transported by controlling the magnetic attraction of the above magnetic support system, this invention has the characteristics that the track is composed by including multiple unit supporting components which are positioned in the direction of transport and these unit supporting components are composed by providing a track frame; multiple magnetic support units positioned approximately orthogonal to the transport direction of the objects to be transported via a mounting device which permits vertical movement of the track frame including the electromagnets; an attraction control device which performs levitation control on the perpendicular movement of the object to be transported and levitation control on the rolling of the object to be transported by controlling the electromagnets of each magnetic support unit only when the object to be transported is below each magnetic support unit; an inclination device which varies the angle of inclination of the object to be transported in the direction orthogonal to the transport direction and an angle of inclination control device which controls that angle of inclination. When using this invention, levitation control on the perpendicular movement of the steel plate and levitation control on rolling are performed at every unit supporting component. Also, it is possible to inhibit the pitching of the steel plate between the unit supporting components by the magnetic support units being vertically moveable using the mounting device. For this reason, stable levitation can be performed by inhibiting the vertical movement and rolling of the steel plate at every unit supporting component, even if, not only the whole length, but also the whole width, of the steel plate varies. Also, pitching of the steel plate can be stabilised by the mounting device. Therefore, it is possible to support the whole of the steel plate without contact. Moreover, when guiding the steel plate by controlling the inclination of the steel plate to the left or right in relation to the direction of advance at every unit supporting component, the guiding force which acts on the steel plate by inclining the magnetic support units is proportional to the weight of the steel plate. Since the acceleration of the steel plate to the left or right is unrelated to the weight, it is possible to achieve guidance control of the steel plate without being affected by the weight of the steel plate. For this reason, there is no requirement for the provision of a fresh guidance device. Therefore, it is possible to simplify the composition of the whole system and, at the same time it is possible to increase the number of unit supporting components per unit length of track. Even when the weight and the inertial moment of the steel plate differ, this difference can be divided into each unit supporting component. Thus, as a magnetic track positioning type magnetic levitation transport system as a whole which is formed of a collection of individual unit supporting components, non-contact support and guidance is possible for steel plates which have a greater range of weights and inertial moments. Also, non-contact transport is possible for multiple steel plates to be transported by one track. Furthermore, in a magnetic levitation system provided with magnet units having electromagnets; frames for mounting these magnet units and a magnetic support control device which controls the attraction of the electromagnets of the magnet units for the non-contact support of the object to be transported of which at least a part is formed by a magnetic body, this invention has the characteristic of being provided with an inclination device which varies the angle of inclination of the object to be transported in the direction of transport and an angle of inclination control device which controls this angle of inclination. When using this invention, the guiding force acts by the combined force of the gravitational force due to the inclination of the levitated object to be transported and the attraction of the magnetic unit. The guiding force can be adjusted by detecting the amount of movement and the speed of movement in the guidance direction of the object to be transported, and controlling the angle of inclination of the object to be transported. Therefore, there is no requirement for the provision of fresh electromagnets for guidance. Thus, the supporting mechanism can be simplified. Also, since the guiding force can be obtained by the inclination of the object to be transported, a guiding force can obtained which is relative in size to the mass of the object to be transported. Moreover, it is possible to obtain guidance of the object to be transported, even if the width of the object to be transported is greater than the gaps between magnet units in the direction of guidance. For this reason, it is possible to support various types of steel plate over long distances without contact. Also, the simple construction of a transport line can be achieved. BRIEF DESCRIPTION OF THE DRAWINGS Other objects and features of the invention will become apparent from the following detailed description of the preferred embodiments taken in conjunction with the accompanying drawings in which: Figure 1 Is an oblique view of the essential parts in the magnetic track positioning type magnetic levitation transport system concerned in an embodiment of this invention. Figure 2 Is an oblique view of the essential parts of a unit support component in the above system. Figure 3 Is a block diagram of the attraction control system in the above system. Figure 4 Is a block diagram of the height control system in the above system. Figure 5 Is an oblique view of a unit propulsion component in the above system. Figure 6 Is a block-diagram of the thrust control system in the above system. Figure 7 Is a diagram to illustrate the stator moving magnetic field in the above system. Figure 8 Is a block diagram of the height control system for propulsion in the above system. Figure 9 Is an oblique view of the essential parts of a unit guidance component in the above system. Figure 10 Is a block diagram of the guiding force control system in the above system. Figure 11 Is a cross-sectional view along the track central length direction to illustrate the operation in the above system. Figure 12 Is an oblique view of the essential parts in the magnetic track positioning type magnetic levitation transport system concerned in a different embodiment of this invention. Figure 13 Is an oblique view of the essential parts in the magnetic track positioning type magnetic levitation transport system concerned in another different embodiment of this invention. Figure 14 Is an oblique view of the essential parts in the magnetic track positioning type magnetic levitation transport system concerned in yet another different embodiment of this invention. Figure 15 Is a block diagram of the control system in the above system. Figure 16 Is a block diagram of another control system in the above system. Figure 17 Is an oblique view showing the magnetic track positioning type magnetic levitation transport system of another embodiment of this invention. Figure 18 Is a block diagram of the height control system used in the above transport system. Figure 19 Is a side elevation showing the lay-out state of the above transport system. Figure 20 Is front elevations of magnetic support units to illustrate the inclination guidance operation using the above transport system. Figure 21 Is an oblique view showing the essential parts of a unit supporting component of a further embodiment of this invention. Figure 22 Is an oblique view showing another embodiment of a magnetic support unit. Figure 23 Is an oblique view showing a further embodiment of the magnetic levitation transport system of this invention. Figure 24 Is an oblique view showing a transporter used in the above transport system. Figure 25 Is a block diagram of the running control system used in the above transport system. Figure 26 Is a block diagram of the magnetic support control system used in the above transport system. Figure 27 Is a block diagram of the angle of inclination control system used in the above transport system. Figure 28 Is illustrations of operations to illustrate the transport operation using the above transport system. Figure 29 Is illustrations of operations to illustrate a different transport operation using the above transport system. Figure 30 Is an oblique view showing a scalar type robot to which the magnetic levitation system of this invention has been applied. Figure 31 Is an oblique view showing another embodiment of the magnetic levitation system of this invention. Figure 32 Is an oblique view showing another embodiment of the magnetic levitation system of this invention. DETAILED DESCRIPTIONS OF THE PREFERRED EMBODIMENTS The following is a description of an embodiment of this invention with reference to the drawings. Figure 1 shows magnetic track positioning type magnetic levitation transport system 1 concerned in an embodiment of this invention. The composition of magnetic track positioning type magnetic levitation transport system 1 includes unit support components 3 , which form a track arranged along the transport route; unit propulsion components 5 arranged at strategic points on the track and which give thrust in transport direction 4 to the object to be transported made of ferromagnetic material, for instance steel plate X and unit guidance components 7 positioned at strategic points on the track and which apply guiding forces to steel plate X . As shown in Figure 2, the composition of unit support component 3 includes inverted U-shaped track frame 13 which has bases 11 secured to its two ends; a pair of magnetic support units 15a and 15b aligned on a line orthogonal to the transport direction and which exert magnetic attraction on steel plate X in order to support steel plate X , which is the object to be transported, without contact; mounting device 17 , which is present between track frame 13 and each magnetic support unit 15a and 15b , for mounting each magnetic support unit 15a and 15b on track frame 13 and attraction control device 19 which causes the non-contact support of steel plate X by controlling the magnetic attraction of each magnetic support unit 15a and 15b . Each magnetic support unit 15a and 15b is respectively composed in the same manner. Magnetic support unit 15a is composed of permanent magnet 21a sandwiched by two electromagnets 27a and 27b , made up of coils 23a and 23b and iron cores 25a and 25b. In the same way, magnetic support unit 15b is composed of permanent magnet 21b sandwiched by two electromagnets 27c and 27d, made up of coils 23c and 23d and iron cores 25c and 25d . Also, both coils 23a, 23b (coils 23c, 23d ) are connected in series so that their magnetic fluxes reinforce each other by using the same excitation current. Mounting device 17 is composed of two seats 31a and 31b welded to the underside of track frame 13 with a specified gap between them; baseplate 35 which is guided so that it is only free to move in the vertical direction via guide mechanisms 33a and 33b respectively provided beneath these two seats 31a and 31b ; substrate 39 , for the two magnetic support units 15a and 15b and attraction control device 19, on the underside of which are provided four gap sensors 37a, 37b, 37c and 37d which measure the gaps between each magnetic support unit 15a and 15b and steel plate X and height adjustment mechanism 41 which is secured to the upper face of substrate 39 and adjusts the height of substrate 39 by varying the distance between baseplate 35 and substrate 39 . Also, height adjustment mechanism 41 is composed of a total of four linear guides 43a, 43b, 43c and 43d which are thrust through baseplate 35 and secured at both ends of baseplate 35 ; four rods 45a, 45b, 45c and 45d of which the lower ends are secured to substrate 39 and the upper ends are guided by linear guides 43a, 43b, 43c and 43d so that they are free to move in the vertical direction and actuators 51a and 51b , which are free to expand and contract, of which the tops are thrust through baseplate 35 and secured, and the lower ends are secured to the upper face of substrate 39 . The expansion and contraction of actuators 51a and 51b are controlled by height control system 53 in order to control the height of substrate 39 to a specified value. Guide mechanisms 33a and 33b are provided respectively at the two ends of the upper face of baseplate 35. Guide mechanism 33a is composed of a total of two linear guides (one of which is not illustrated) 43e (43f) which are thrust through seat 31a and secured to both ends of seat 31a ; two rods 45e and 45f of which the lower ends are secured to baseplate 35 and the upper ends are guided by linear guides 43e (43f) so that they are free to move in the vertical direction; coil springs 47a and 47b , as elastic components, which are fitted between baseplate 35 and linear guides 43e (43f) so that they encircle each rod 45e and 45f and damper 49a , as an inelastic component, of which the upper end is secured to the underside of seat 31a while the lower end is secured to the upper surface of baseplate 35 . In the same way, guide mechanism 33b is composed of a total of two linear guides (one of which is not illustrated) 43g (43h) which are thrust through seat 31b and secured to both ends of seat 31b; two rods 45g and 45h of which the lower ends are secured to baseplate 35 and the upper ends are guided by linear guides 43g (43h) so that they are free to move in the vertical direction; coil springs 47c and 47d , as elastic components, which are fitted between baseplate 35 and linear guides 43g (43h) so that they encircle each rod 45g and 45h and damper 49b , as an inelastic component, of which the upper end is secured to the underside of seat 31b while the lower end is secured to the upper surface of baseplate 35 . Out of the above linear guides 43a, 43b, ... , linear guide 43c and linear guide 43e have the dual purpose of travel distance measuring devices for measuring the vertical travel distances of respective rods 45c and 45e . As shown in the block diagram in Figure 3, attraction control device 19 is mainly composed of levitation sensor unit 57, levitation operation unit 59 and power amplifiers 61a and 61b . That is to say, attraction control device 19 is composed of levitation sensor unit 57 which is composed of four gap sensors 37a, 37b, 37c and 37d which are positioned close to the left and right of each magnetic support unit 15a and 15b in every unit support component 3 to measure the levitation gaps between the respective magnetic support units 15a and 15b and steel plate X , and current detectors 55a and 55b for measuring the excitation currents flowing in each coil 23a, 23b, 23c and 23d of electromagnets 27a and 27b ; operation unit for levitation 59 which takes as its inputs output signals za ~ zd, ia and ib from levitation sensor unit 57 and displacement signal Δzbs from the specified setting value for the height of substrate 39 obtained from height control system 53, and calculates excitation voltages ea and eb for every magnetic support unit 15a and 15b which are required to levitate steel plate X and power amplifiers 61a and 61b which are connected to a power source (not illustrated) and excite coils 23a, 23b, 23c and 23d of each magnetic support unit 15a and 15b based on outputs ea and eb of levitation operation unit 59. Levitation operation unit 59 of attraction control device 19 is composed of levitation gap setter 70 and levitation current setter 72 which output specified setting values which are set by, for instance, the main computer; subtractors 74a ~ 74d for subtracting the levitation gap setting value from output values za ~ zd of gap sensors 37a ~ 37d and subtractors 76a and 76b which subtract the current setting value from output values ia and ib of current detectors 55a and 55b; steel plate detector circuit 78 which detects the presence of steel plate X at a position below magnetic support units 15a and 15b from output values za ~ zd of gap sensors 37a ~ 37d; levitation gap deviation coordinates conversion circuit 80 for obtaining deviation Δz from the specified position of the centre of gravity coordinates of the part of steel plate X which overlaps unit support component 3 from the output values of subtractors 74a ~ 74d and roll angle Δ of the same part of steel plate X ; excitation current deviation coordinates conversion circuit 81 for obtaining coil excitation current Δiz which contributes to the vertical motion of the centre of gravity of the part of steel plate X which overlaps unit support component 3 and coil excitation current Δi which contributes to the rolling of the same part of steel plate X; control voltage operation circuit 84 which is provided with vertical motion mode control voltage operation circuit 82 which takes as its inputs signal Δzbs from height control system 53, which expresses the deviation from the specified height of substrate 39 in addition to outputs Δz and Δiz of levitation gap deviation coordinates conversion circuit 80 and excitation current deviation coordinates conversion circuit 81, and calculates coil excitation voltage ez which contributes to the vertical motion of the centre of gravity of the part of steel plate X which overlaps unit support component 3 and roll mode control voltage operation circuit 83 which takes as its inputs outputs Δ and Δ i  of levitation gap deviation coordinates conversion circuit 80 and excitation current deviation coordinates conversion circuit 81, and calculates coil excitation voltage e which contributes to the rolling of the part of steel plate X which overlaps unit support component 3 and control voltage coordinates inversion circuit 86 which takes as its inputs outputs ez and e of control voltage operation circuit 84 and detection signal TF from steel plate detector circuit 78, and, when steel plate X is present below magnetic support units 15a and 15b , calculates the excitation voltages ea and eb for exciting the respective magnetic support units 15a and 15b. In control voltage coordinates inversion circuit 86 , when steel plate detection signal TF changes from 'NO' to 'YES', a changeover from 0 and 0 to ea and eb is performed after specified time t1. Moreover, when the rolling of steel plate X is impaired due to external causes, the design is that output e of roll mode control voltage operation circuit 83 becomes zero through a device which is not illustrated. As shown in Figure 4, height control system 53 is composed of height adjustment sensor unit 63 , which is composed of linear guides 43c and 43e which are provided with travel distance meters; height adjustment operation unit 65 , which takes as its inputs the output signals of height adjustment sensor unit 63 and signal Δz for the displacement from the specified set value of the levitation gap length and steel plate X detection signal TF , which are obtained from attraction control device 19, and calculates the motor driving current ida of actuators 51a and 51b in order to maintain the height of steel plate X at the specified value during levitation and current driver 67 which is connected to a power source (not illustrated) and drives motors Ma and Mb of actuators 51a and 51b based on output ida of height adjustment operation unit 65. Height adjustment operation unit 65 is composed of substrate height setter 88 , which selectively outputs multiple specified setting values, which are set by, for instance, a main computer, based on steel plate detection signal TF from attraction control device 19 ; operator 90 for subtracting the base height set value from the sum of output values ha and hb of linear guides 43a and 43b ; changeover switch 92 which takes as its inputs displacement signal Δz and steel plate detection signal TF from attraction control device 19, and outputs Δz when steel plate X is levitated below magnetic support units 15a and 15b and 0 when that is not the case; adder 94 which adds the output of operator 90, which expresses signal Δzbs for the displacement from the specified setting value of the height of substrate 39, to the output of changeover switch 92 and excitation current operation circuit 96 which calculates motor driving current ida , for actuators 51a and 51b for maintaining the specified value of the height of steel plate X when levitated, from the output of operator 94. In changeover switch 92, when steel plate detection signal TF changes from 'NO' to 'YES', the changeover from 0 to Δz is performed after specified time t2. Unit propulsion component 5 is composed as shown in Figure 5. In the description of the structural parts used in this drawing, those parts which are the same as some of the structural components in the drawing described above have been given the same symbols and their descriptions have been omitted. In this unit propulsion component 5 , the ends of the two legs of its track frame 13 are secured to a single base 98. Stators 100a and 100b of two linear induction motors, as the propulsion device for imparting a thrust to steel plate X without contact, are secured to the upper surface of base 98. Stators 100a and 100b are respectively secured to the upper surfaces of cross-shaped substrates 102a and 102b. In order to guide stator 100a in the vertical direction, cross-shaped substrate 102a is mounted on base 98 via a pair of linear guides 104a and 104b which are thrust through substrate 102a and secured; rods 105a and 105b, which are guided by linear guides 102a and 102b, and of which the lower ends are secured to the upper surface of base 98 , and a pair of actuators 106a and 106b of which the upper ends are secured to the underside of substrate 102a while the lower ends are secured to the upper surface of base 98 , and which are positioned at the front and rear ends of substrate 102a. In the same way, in order to guide stator 100b in the vertical direction, cross-shaped substrate 102b is mounted on base 98 via a pair of linear guides 104c and 104d which are thrust through substrate 102b and secured; rods 105c and 105d, which are guided by linear guides 102c and 102d, and of which the lower ends are secured to the upper surface of base 98, and a pair of actuators 106c and 106d of which the upper ends are secured to the underside of substrate 102b while the lower ends are secured to the upper surface of base 98 , and which are positioned at the front and rear ends of substrate 102b . Gap sensors 108a and 108b, which detect the gap width between steel plate X and stators 100a and 100b , are respectively installed on the upper surfaces of the inner arms of the two substrates 102a and 102b . That is to say, base 98 , linear guides 104a, 104b, 104c and 104d, and actuators 106a, 106b, 106c and 106d compose height adjustment mechanisms 110a and 110b for stators 100a and 100b . Also, out of linear guides 104a, 104b, 104c and 104d, linear guides 104b and 104c have the dual purpose of respective travel distance meters for rods 105b and 105c. The structure of mounting device 112 between baseplate 35 and track frame 13 is the same as the structure of the above-mentioned unit support component 3 . Its description has therefore been omitted. The part below baseplate 35 of mounting device 112 of unit propulsion component 5 is composed by respectively suspending cross-shaped substrates 102a and 102b from the undersides of the two ends of baseplate 35 by respective actuators 51a and 51b, respective pairs of linear guides 43a, 43b and 43c, 43d and rods 45a, 45b and 45c, 45d which pass through these. Here, in'mounting device 112, the damping factor of damper 49 is infinity. Furthermore, in order to impart thrust to steel plate X (not illustrated) without contact, as propulsion devices, linear induction motor stators 114a and 114b are respectively installed on the undersides of substrates 102a and 102b so that they face stators 100a and 100b . Support plates 116 are secured on both sides of the central portion of baseplate 35 of mounting device 112 . As detection devices for the presence of steel plate X and the yawing of steel plate X , feed monitors for detecting left and right travel without contact are mounted below the two tips of support plate 116 via thrust control system 120 , height control system 122 and seating plates 124a and 124b . At the same time, at the left and right ends of cross-shaped substrates 102a and 102b of mounting device 112, two gap sensors 126a and 126b, which detect the respective gaps between steel plate X and stator 114a and between steel plate X and stator 114b, are mounted on the inner sides, while feed monitors 128a and 128b, for the non-contact detection of the presence of steel plate X and its travel along the track, are mounted on the outer sides. That is to say, height adjustment mechanisms 130a and 130b which can adjust the respective heights of stators 114a and 114b are each composed by two linear guides 43a, 43b and 43c , 43d which are thrust through and secured to baseplate 35; two rods 45a , 45b and 45c, 45d of which the lower ends are secured to substrates 102a and 102b, and which are guided by linear guides 43a, 43b and 43c , 43d so that they are free to move in the vertical direction and actuators 51a and 51b of which the upper parts are thrust through and secured to baseplate 35 while the lower ends are secured to the upper surfaces of substrates 102a and 102b , and which are free to expand and contract. The expansion and contraction of actuators 106a, 106b and 106c, 106d and actuators 51a and 51b are controlled by height control system 122 in order to control the respective heights of stators 100a and 100b and stators 114a and 114b at the specified values. Here, in feed monitors 118a and 118b and feed monitors 128a and 128b, zero is outputted when the absence of steel plate X is detected, and when the presence of steel plate X is detected, the amount of travel from the time of detection is outputted, taking the initial value as zero. The following is a description of propulsion control system 120 with reference to the block diagram shown in Figure 6. Propulsion control system 120 is composed of thrust sensor unit 132 which is composed of feed monitors 118a and 118b which detect and output left and right travel amounts ya and yb of steel plate X which is below stators 114a and 114b, and, at the same time, output steel plate X presence detection signal TF and feed monitors 128a and 128b which detect and output travel amounts xa and xb along the track of steel plate X which is below them, and, at the same time, output steel plate X presence detection signal TF; thrust operation device 134 , which takes as its inputs outputs xa, xb, ya and yb and the four TF of thrust sensor unit 132, for calculating excitation frequency ωa for exciting stator 100a and stator 114a and excitation frequency ωb for exciting stator 100b and stator 114b, based on these; 3-phase inverter 136a which is connected to a 3-phase power source (not illustrated) and excites stator 100a and stator 114a based on output ωa of thrust operation device 134 and 3-phase inverter 136b which similarly excites stator 100b and stator 114b. With this embodiment, inverters 136a and 136b are the excitation devices. Also, stator 100a and stator 114a, stator 100b and stator 114b are connected so that the travelling magnetic fields shown in Figure 7 are generated between stators which face each other. Thrust operation device 134 is composed of differentiator 138 for calculating the respective travel speeds from outputs xa and xb of thrust sensor unit 132; steel plate speed coordinates conversion circuit 140 for obtaining travel speed vx of the centre of gravity of the part of steel plate X which overlaps unit propulsion component 5 from speeds va and vb of differentiator 138; yaw direction coordinates conversion circuit 142 for obtaining angle of yaw  about the centre of gravity of the part of steel plate X which overlaps unit propulsion component 5 from outputs ya and yb of thrust sensor unit 132; AND circuit 144 which calculates the AND of the four steel plate X presence detection signals TF ; steel plate speed setter 146 which outputs a specified value set by, for instance, a main computer; yaw angle setter 148 which operates in a similar way to setter 146 ; subtractor 150 which subtracts the set value of steel plate speed setter 146 from output vx of steel plate speed coordinates conversion circuit 140, and outputs speed deviation Δvx; subtractor 152 which subtracts the set value of yaw angle setter 148 from output  of yaw direction coordinates conversion circuit 142, and outputs yaw angle deviation Δ ; excitation frequency operation circuit 158 which is made up of speed mode excitation frequency operation circuit 154 which calculates excitation frequency ωz of inverters 136a and 136b which is related to the travel speed of the centre of gravity of the part of steel plate X overlapping unit propulsion component 5 and is based on output Δvx of subtractor 150 and yaw mode excitation frequency operation circuit 156 which calculates excitation frequency ω of inverters 136a and 136b which is related to the yawing about the centre of gravity of the part of steel plate X which overlaps unit propulsion component 5 and excitation frequency coordinates inversion circuit 160 which takes as inputs outputs ωz and ω of excitation frequency operation circuit 158 together with detection signal TF of AND circuit 144, and, when steel plate X is present below stators 114a and 114b, calculates excitation frequency ωa of inverter 136a which excites stator 100a and stator 114a, and, at the same time, in the same case, calculates excitation frequency ωb which excites stator 100b and stator 114b. Height control system 122 is divided into four blocks of the same composition which separately control the individual heights of the four stators 100a, 100b, 114a and 114b. The composition of one block of height control system 122 is shown in Figure 8. One of the blocks of height control system 122 is composed of height adjustment sensor unit 162 , which is composed of gap sensors 126a and 126b or gap sensors 108a and 108b and linear guide 43b or linear guide 104b and which outputs output value h of gap sensors 108a and 108b or of gap sensors 126a and 126b and, at the same time, outputs output value I of linear guide 43b or linear guide 104b ; height adjustment operation unit 164 which takes as its inputs output signals h and I of height adjustment sensor unit 162 and steel plate X detection signal TF obtained from propulsion control system 120, and calculates motor driving current idt of actuators 51a and 51b or actuators 106a and 106b for maintaining the respective gaps between steel plate X and stators 100a and 100b or stators 114a and 114b at the specified values and current driver 165 , which is connected to a power source (not illustrated) and which drives motors M of actuators 51a and 51b or actuators 106a, 106b, 106c and 106d based on output idt of height adjustment operation unit 164 . Height adjustment operation unit 164 is composed of stator gap width setter 166 which selectively outputs multiple specified set values which are set by, for instance'a main computer, based on steel plate detection signal TF from propulsion control system 120 ; changeover switch 167 which takes as inputs output h of gap sensors 108a and 108b, output I of linear guides 43b and 104b and steel plate detection signal TF, and outputs h when steel plate X is present below stators 114a and 114b and outputs I when that is not the case; subtractor 168 which subtracts the output of stator gap width setter 166 from the output of changeover switch 167 and excitation current operation circuit 170 which calculates motor drive current idt of actuators 51a and 51b for maintaining the gap width between the stators and steel plate X at the specified value from output Δh of subtractor 168. Unit guidance component 7 is composed as shown in Figure 9. In the description of the structural parts used in this drawing, those parts which are the same as some of the structural components in the drawings described above have been given the same symbols and their descriptions have been omitted. In unit guidance component 7 , linear induction motor stators 172a and 172b , as the guidance devices, are respectively mounted on the upper surfaces of respective substrates 102a and 102b of height adjustment mechanisms 110a and 110b . Gap sensors 108a and 108b , which are structural components of height control system 122 shown in Figure 8, are secured on the inner side surfaces close to stators 172a and 172b and on the upper surfaces of substrates 102a and 102b. Also, mounting device 176 is composed by the provision of two plate-shaped substrates 174a and 174b, actuators 51a and 51b and linear guides 43a, 43b, 43c and 43d and rods 45a, 45b, 45c and 45d which pass through them, beneath baseplate 35 . Here, in mounting device 176 , the damping factor of dampers 49 is infinity, and they are secured between baseplate 35 and track frame 13 . Moreover, as the guidance device, linear induction motor stators 178a and 178b are mounted on the lower surfaces of substrates 174 so that they respectively face stators 172a and 172b in order to impart a guiding force to steel plate X without contact. Feed monitor 118, for detecting the presence of steel plate X and its left and right travel amounts without contact, is mounted on the underside of the central part of baseplate 35 , which is a structural component of mounting device 176 , via guiding force control system 180 and seat 124 . At the same time, gap sensors 126a and 126b, which detect the gap widths between steel plate X and stators 178a and 178b are mounted on the undersides of the inner ends of substrates 174a and 174b. That is to say, height adjustment mechanisms 182a and 182b, which adjust the respective heights of stators 178a and 178b , are each composed of two linear guides 43a, 43b and 43c, 43d which are thrust through baseplate 35 and secured; two rods 45a, 45b and 45c, 45d, which are guided by linear guides 43a, 43b and 43c, 43d so that they are free to move in the vertical direction, and actuators 51a and 51b , of which the upper parts are thrust through baseplate 35 and secured while the lower ends are secured to the upper surfaces of substrates 174a and 174b , and which are free to expand and contract. The amounts of expansion and contraction of actuators 106a, 106b, 106c and 106d and of actuators 51a and 51b are controlled by height control system 122, which is mounted on the end part of the upper surface of base 98 , for controlling the respective heights of stators 172a and 172b and stators 178a and 178b at the specified values. Height control system 122 is the same as that in unit propulsion component 5 . However, the steel plate X presence detection signal TF which is introduced to height adjustment operation unit 164 shown in Figure 8 comes from guiding force control system 180. Figure 10 shows the composition of guiding force control system 180. Guiding force control system 180 is composed of guidance detection device 184 which is composed of feed monitor 118 which detects and outputs the left/right travel amount y of steel plate X which is beneath stators 178a and 178b, and, at the same time, outputs steel plate X presence detection signal TF ; guiding force operation device 186 which takes as inputs y and TF outputted from guidance detection device 184 in order to calculate excitation frequency ωga for exciting stator 172a and stator 178a and excitation frequency ωgb for exciting stator 172b and stator 178b based on these inputs; 3-phase inverter 188a which is connected to a 3-phase power source (not illustrated) and which excites stator 172a and stator 178a based on output ωga of guiding force operation device 186 and 3-phase inverter 188b which similarly excites stator 172b and stator 178b based on output ωgb of guiding force operation device 186. With this embodiment, inverters 188a and 188b are the excitation devices. Also, stator 172a and stator 178a , stator 172b and stator 178b are connected so that the travelling magnetic fields shown in Figure 7 are generated between stators which face each other. At the same time, the directions of the travelling magnetic fields between stator 172a and stator 178a and between stator 172b and stator 178b are in the reverse direction to each other so that they are facing each other. Guiding force operating device 186 is composed of steel plate centre deviation setter 190 , which outputs a specified setting value set by, for instance, a main computer; subtractor 192 , which subtracts the set value of steel plate centre deviation setter 190 from output y of guidance detection device 184 to calculate positional deviation Δy of the part of steel plate X which overlaps unit guidance component 7 ; guide mode excitation frequency operation circuit 194 which calculates the incremental/decremental excitation frequency Δω of excitation frequency ωga of inverter 188a and of excitation frequency ωgb of inverter 188b, which are concerned in the guidance of the part of steel plate X which overlaps unit guidance component 7 , based on output Δy of subtractor 192 and individual excitation frequency operation circuit 196 , which takes as its inputs output Δω of guide mode excitation frequency operation circuit 194 and steel plate X presence detection signal TF, and calculates excitation frequency ωga of inverter 188a which excites stator 172a and stator 178a when steel plate X is present beneath stators 178a and 178b and, at the same time, calculates excitation frequency ωgb of inverter 188b which excites stator 172b and stator 178b in the same case. In individual excitation frequency operation circuit 196, ωga = ω - Δω, ωgb = ω + Δω are calculated for a standard frequency ω, which is set at a specified magnitude. The following is a description of the operation of the magnetic track positioning type magnetic levitation transport system concerned in the embodiment composed as described above. Here, the description uses Figure 11 for the case when the magnetic track positioning type magnetic levitation transport system concerned in this embodiment is set up along a transport route from the vicinity of the roller exit of a cold rolling mill. In Figure 11, 197 is the rollers of the cold rolling mill. In each unit support component 3, when steel plate X is not beneath magnetic support units 15, steel plate detection circuit 78 detects that there is no steel plate because the output values of gap sensors 37a ~ 37d are large. Thus, since the fact that there is no steel plate is transmitted to control voltage coordinates inversion circuit 86 by detection signal TF, zero is outputted in place of excitation voltages ea and eb , and no levitation control is performed. At this time, detection signal TF is also transmitted to height control system 53 . For this reason, zero is selected by changeover switch 92 and, at the same time, a value to make the expansion of linear guides 43 smaller than the set value when steel plate X is present is selected in substrate height setter 88. The sum of the outputs ha and hb of linear guides 43a and 43b expresses the height of substrate 39, and the set value of substrate height setter 88 is subtracted from the sum of ha and hb in operator 90. Then, when substrate 39 is not at the specified value, output Δzbs of operator 90 is introduced to excitation current operation circuit 96 of height control system 53, and ida is operated so that Δzbs converges to zero, and the motors of actuators 51 are driven by current driver 67. By this means, substrate 39 is set in a higher position than when steel plate X is present. When substrate 39 is set in a higher position in this way, even if steel plate X arrives by levitation at that unit support component 3, not only does steel plate X not make contact with magnetic support units 15, but also a sufficient gap width between magnetic support units 15 and steel plate X can be ensured. Neither is steel plate X adsorbed by the attraction of permanent magnets 21. In each unit propulsion component 5 and each unit guidance component 7 of height control system 122 also, the fact that steel plate X is not present is transmitted to stator gap width setter 166 and changeover switch 167 by detection signal TF. By this means, a smaller value than when steel plate X is present is selected in stator gap width setter 166 , while output 1 of linear guides 43 and 104 is selected in changeover switch 167. Then, in the case when 1 is not the same as the set value, Δh is introduced to excitation current operation circuit 170, and idt is operated so that Δh converges to zero and the motors of actuators 51 and 106 are driven by current driver 165. By this means, stators 114a , 114b, 178a and 178b are set higher, and also stators 100a, 100b, 172a and 172b are set lower, than when steel plate X is present. Thus, even if steel plate X arrives by levitation at the relevant unit propulsion component 5 or unit guidance component 7, no stator makes contact with steel plate X . Also, since the fact that steel plate X is not present is also transmitted by detection signal TF to excitation frequency coordinates inversion circuit 160 of thrust control system 120 and to individual excitation frequency operation circuit 196 of guiding force control system 180, zero is outputted in place of their outputs ωa , ωb and ωga , ωgb . Thus, there is no excitation of the stators. When steel plate X arrives beneath magnetic support units 15 of unit support component 3, since the output values of gap sensors 37a ~ 37d are smaller than the specified value, steel plate detection circuit 78 detects that a steel plate is present. Then, the fact that steel plate X has arrived beneath magnetic support units 15 of unit support component 3 is transmitted by detection signal TF to substrate height setter 88 and changeover switch 92 of height control system 53. Then, the set value for when steel plate X is present is selected in substrate height setter 88. With operator 90, the set value of substrate height setter 88 is subtracted from the sum of outputs ha and hb of linear guides 43a and 43b to output Δzbs . When there is no set value for substrate 39, the output of changeover switch 92, which selects zero, and Δzbs are added by adder 94. Thus, the output of adder 94 and Δzbs are introduced to excitation current operation circuit 96. In excitation current operation circuit 96, ida is operated so that Δzbs converges to zero, and the motors of actuators 51 are driven by current driver 67. By this means, substrate 39 is set at the set height when steel plate X is present. At this time, output Δzbs of operator 90 is introduced to vertical motion mode control voltage operation circuit 82 of attraction control device 19. At the same time, steel plate detection signal TF of steel plate detection circuit 78 is transmitted to control voltage coordinates inversion circuit 86. After substrate 39 has been set to the set height, that is to say after specified time t1 from receiving detection signal TF , excitation voltages ea and eb are outputted to commence levitation control. In levitation control, the output values za, zb, zc and zd of gap sensors 37a ~ 37d are subtracted from the output of levitation gap width setter 70 by subtractors 74a ~ 74d. These subtraction results are introduced to levitation gap width deviation coordinates conversion circuit 80, and deviation Δz from the specified position of the centre of gravity coordinates of the part of steel plate X which overlaps unit support component 3 and roll angle Δ of that part of steel plate X are calculated. Then, excitation current measured values ia and ib of electromagnets 27 detected by current detectors 55a and 55b are subtracted from the zero output of current setter 72 by subtractors 76a and 76b . These subtraction results are introduced to excitation current deviation coordinates conversion circuit 81, and coil excitation current Δiz , which contributes to the vertical motion of the centre of gravity of the part of steel plate X which overlaps unit support component 3 , and coil excitation current Δi , which contributes to the rolling of that part of steel plate X, are calculated. Out of Δz, Δ, Δiz and Δi, Δz and Δiz are introduced to vertical motion mode control voltage operation circuit 82, together with output Δzbs of operator 90. Here, coil excitation voltage ez, which contributes to the vertical motion of the centre of gravity of the part of steel plate X overlapping unit support component 3 , is calculated. When ez is calculated, Δiz converges to zero in the stationary levitation state of steel plate X , that is to say zero power control is performed. At the same time, Δ and Δi are introduced to roll mode control voltage operation circuit 83, and coil excitation voltage e , which contributes to the rolling of the same part of steel plate X , is calculated. When e  is calculated also, Δ i  converges to zero in the stationary levitation state of steel plate X , in other words zero power control is performed. Outputs ez and e of control voltage operation circuit 84 are introduced to control voltage coordinates inversion circuit 86 , and excitation voltages ea and eb for respective electromagnets 27 are calculated. By this levitation control, ia and ib in the stationary levitation state of steel plate X converge to zero, in other words, zero power control is achieved as a whole. In this way, if levitation control which contributes to the vertical motion of the centre of gravity of the part of steel plate X overlapping unit support component 3 and levitation control which contributes to the rolling of the same part of steel plate X are performed in every mode, it is possible to design levitation control systems in the respective modes. Therefore, robust levitation control can be performed for variations of weight per unit length of steel plate X and for variations of material and thickness. Also, during the time for levitation control to arrive at the stationary levitation state, the weight of steel plate X is loaded on coil springs 47 and dampers 49. Thus, even if output ha of linear guide 43a fluctuates, height control will be performed in height control system 53 to maintain substrate 39 at the set height. At the same time, since the fluctuation of Δzbs which accompanies height control is introduced to vertical motion mode control voltage operation circuit 82 , stable levitation control can be achieved. Furthermore, if steel plate X is stably levitated by zero power control, the levitation gap width between magnetic support units 15 and steel plate X becomes a width which balances the attraction of permanent magnets 21 and the load weight of steel plate X. If the levitation gap width at this time differs from the output value of levitation gap width setter 70, Δz is outputted in levitation gap width deviation coordinates conversion circuit 80. This output is introduced to changeover switch 92 of height control system 53 . Then, after specified time t2 from the reception of steel plate detection signal TF of steel plate detection circuit 78 to the stable levitation of steel plate X, it is outputted from changeover switch 92. By this means, (Δz bs + Δ z ) is outputted by adder 94 of height control system 53. Therefore, substrate 39 shifts to a position which is only Δ z higher than the specified height. In this way, even if the weight of steel plate X which is supported by unit support component 3 varies per unit length, its upper surface always levitates at a constant height. Here, if a levitation gap width setting value which takes into consideration thickness data for steel plate X is set in the main computer, it goes without saying that it is possible always to levitate the position of the centre of the thickness of steel plate X at a constant height. Since steel plate X can be levitated at a constant height in this way, not only does dimensional compatibility with other systems become simple, but also the initial values of the gap widths between magnetic support units 15 and steel plate X when levitation control is initiated in unit support components 3 by the fresh arrival of steel plate X are the same for each unit support component 3 . Therefore, the shocks at the initiation of levitation control applied to unit support components 3 which are already supporting steel plate X can be made the same. Thus, there is the advantage that control system design for the absorption of this shock by attraction control device 19 becomes simple. After the passage of steel plate X through unit support component 3 is completed, the output values of gap sensors 37a ~ 37d become larger and therefore steel plate detection circuit 78 detects that there is no steel plate. Then, by the operation in the above-mentioned case when steel plate X is not beneath magnetic support units 15, levitation control of unit support component 3 is stopped. At the same time, substrate 39 is set in a higher position than when steel plate X is present, and maintains this state until the arrival of the next steel plate. Steel plate X which is supported without contact by unit support component 3 travels by means of unit propulsion component 5. The above levitation control and height control are successively commenced by all the unit support components 3 at which steel plate X has arrived. At this time, bending in the vertical direction sometimes occurs along the direction of advance of steel plate X due to elasticity. This bending becomes a disturbance in the vertical direction in individual unit support components 3 . In two neighbouring unit support components 3, it becomes pitching of the steel plate parts supported by them. In attraction control device 19 of each unit support component 3 , levitation control is performed in relation to the vertical motion and the rolling of the centre of gravity of steel plate X by vertical motion mode control voltage operation circuit 82 and roll mode control voltage operation circuit 83 . However, if the respective spring constants and damping factors of coil springs 47 and dampers 49 of mounting device 17 are set at appropriate values, it becomes possible to accelerate the pitching convergence of the steel plate. In this embodiment, the bending of steel plate X can be effectively inhibited by accelerating the pitching convergence of the steel plate. In other words, levitation control in the pitch direction of steel plate X is performed by coil springs 47 and dampers 49 of mounting device 17. Therefore, the whole of steel plate X can be stably levitated. Also, as shown in Figure 11, when the rolling of steel plate X is impaired by the rollers, etc. of the cold rolling mill, output e of roll mode control voltage operation circuit 83 becomes zero through an appropriate device (not illustrated). In each unit propulsion component 5 , when steel plate X arrives beneath stators 114a and 114b , all feed monitors 118a, 118b, 128a and 128b detect that steel plate X is present and output steel plate detection signals TF. Then, the fact that steel plate X has arrived beneath stators 114a and 114b is transmitted to stator gap width setter 166 and changeover switch 167 via AND circuit 144 of thrust control system 120. Height adjustment mechanisms 110a, 110b, 130a and 130b which adjust the heights of each stator 100a, 100b, 114a and 114b are controlled by height control system 122 which is composed of 4 blocks each of the same composition. Therefore, the following is a description of its operation, taking height adjustment mechanism 130a as an example. In stator gap width setter 166, when the fact that steel plate X is present is transmitted by steel plate detection signal TF, the gap width set value between stator 114a and steel plate X is selected, while output h of gap sensor 126 is selected in changeover switch 167. Then, when h is not the same as the set value, Δh is introduced to excitation current operation circuit 170, and idt is operated so that Δh converges to zero. Thus, the motors of actuators 51 and 106 are driven by current driver 165. By this means, the gap width between stator 114a and steel plate X can always be maintained at the set value. The above operation is the same in height adjustment mechanisms 110a, 110b and 130b as well. Thus, the gap widths between stators 100a, 100b, 114a and 114b and steel plate X can always be maintained at the set values, independently of each other. Moreover, in unit guidance component 7, when steel plate X arrives beneath stators 178a and 178b, feed monitors 118 detect that steel plate X is present and output steel plate detection signals TF. Steel plate detection signals TF are transmitted to stator gap width setter 166 and changeover switch 167 of height control system 122. Height adjustment mechanisms 110a, 110b, 182a and 182b which adjust the heights of each stator 172a, 172b, 178a and 178b are controlled by height control system 122 which is composed of four blocks, each of the same composition. Therefore, in the same way as in the case of unit propulsion component 5 , the gap widths between each stator 172a, 172b, 178a and 178b and steel plate X can always be maintained at the set values, independently of each other. If each stator in unit propulsion component 5 or unit guidance component 7 always maintains a constant gap width for steel plate X, even when steel plate X is deformed by twisting or bending, not only will each stator not come into contact with steel plate X, but also the thrust and guiding force contributed to steel plate X can be made to depend solely on the excitation frequency of each stator. Thus, thrust control and guiding force control become simpler. At the same time, in unit propulsion component 5 , when the fact that a steel plate is present is transmitted to excitation frequency coordinates inversion circuit 160 via AND circuit 144, thrust control is commenced to maintain the speed of steel plate X at the specified value while damping the yawing of steel plate X . In thrust control, output values xa and xb of feed monitors 128a and 128b are differentiated by differentiator 138. Then, in steel plate speed coordinates conversion circuit 140, by operating the mean value of the differentiation results, travel speed vx of the centre of gravity of the part of steel plate X overlapping unit propulsion component 5 is outputted. Subtractor 150 subtracts the output of steel plate speed setter 146, that is to say the speed set value set by the main computer, from travel speed vx , and outputs speed deviation Δ vx . Speed deviation Δvx is introduced to speed mode excitation frequency operation circuit 154, and excitation frequency ω z of inverters 136a and 136b concerned in the travel speed of the centre of gravity of the part of steel plate X overlapping unit propulsion component 5 is outputted. Also, output values ya and yb of feed monitors 118a and 118b are introduced to yaw direction coordinates conversion circuit 142, and yaw angle  about the centre of gravity of the part of steel plate X overlapping unit propulsion component 5 is calculated. Output  of yaw direction coordinates conversion circuit 142 is compared with the zero output of yaw angle setter 148 by subtractor 152, and yaw angle deviation Δ is outputted by subtractor 152. Yaw angle deviation Δ is introduced to yaw mode excitation frequency operation circuit 156, and excitation frequency ω of inverters 136a and 136b relating to yawing about the centre of gravity of the part of steel plate X overlapping unit propulsion component 5 is outputted. Outputs ωz and ω of excitation frequency operation circuit 158 are introduced to excitation frequency coordinates inversion circuit 160 . There, excitation frequency ωa of inverter 136a which excites stator 100a and stator 114a is calculated on the basis that ωa = ωz + ω/2 , while excitation frequency ωb of inverter 136b which excites stator 100b and stator 114b in the same case is calculated on the basis that ωb = ωz - ω/2. For this reason, if the travel speed of steel plate X is less than the set value, the four stators 100a, 100b, 114a and 114b are excited so that steel plate X is accelerated, and if a yaw angle occurs, stators 110a and 114a are excited in the deceleration direction while stators 100b and 114b are excited in the acceleration direction. Thus, steel plate X travels without the occurrence of a yaw angle while maintaining the set speed. Furthermore, in unit guidance component 7, when the fact that steel plate X is present is transmitted to individual excitation frequency operation circuit 196 by feed monitors 118, guidance control of steel plate X is commenced. In guidance control, subtractor 192 subtracts the output of steel plate centre deviation setter 190 , that is to say the zero set value set by the main computer, from output value y of feed monitors 118, and outputs position deviation Δy of the left/right direction of the part of steel plate X overlapping unit guidance component 7. Position deviation Δy is introduced to guide mode excitation frequency operation circuit 194. There, excitation frequency incremental/decremental portion Δω of excitation frequency ωga of inverter 188a relating to the guidance of the part of steel plate X overlapping unit guidance component 7 and of excitation frequency ωgb of inverter 188b in the same case is calculated. In individual excitation frequency operation circuit 196, excitation frequency ωga for inverter 188a and excitation frequency ωgb for inverter 188b which relate to the guidance of the part of steel plate X overlapping unit guidance component 7 , based on fixed frequency ωgo preset by the main computer, are calculated on the basis that ωga = ωgo - Δω/2 and ωgb = -ωgo - Δω/2 . Here, stators 172a, 172b, 178a and 178b are excited so that steel plate X receives a guiding force in the y direction of Figure 1 if the respective values of ωga and ωgb are positive, and in the opposite direction if they are negative. If steel plate X has not drifted in the left/right direction, Δy is zero and Δω is also zero. Therefore, stators 172a and 178a are excited by ωgo , while stators 172b and 178b are excited by - ωgo . In this case, the guiding force acting on steel plate X is cancelled and steel plate X does not drift to the left or right. If steel plate X drifts in the y direction by only Δy under an external force, the excitation in the y direction of stators 172a and 178a weakens, while the excitation in the -y direction of stators 172b and 178b strengthens. Therefore, a guiding force acts on steel plate X as a whole in the opposite direction to the y direction. Then, Δy decreases and guidance of steel plate X is achieved. In this way, steel plate X travels to its destination while levitating without contact and without leaving the track which is composed by unit support components 3 , unit propulsion components 5 and unit guidance components 7 . In the above embodiment, mounting device 17 is composed of guide mechanisms, provided with coil springs, dampers, linear guides, etc., and height adjustment mechanisms, provided with actuators, linear guides, etc. However, this does not limit the composition of the mounting device in any way, and various modifications can be made, provided the magnetic support units have vertically moveable structures. For example, as shown in Figure 12, mounting device 17' is composed by securing baseplate 35 to track frame 13 by supports 198a, 198b, 198c and 198d , while sandwiching load cells 200a and 200b between actuators 51a and 51b and substrate 39. In this case, any force in the vertical direction applied to mounting device 17' is measured by load cells 200a and 200b . Thus, it goes without saying that, by performing height control using the outputs of load cells 200a and 200b , the same function can be achieved as in the case of using coil springs and dampers. Also, in the above embodiment, two magnetic support units 15a and 15b are provided on substrate 39 . However, this does not restrict the number of magnetic support units used in unit support component 3 in any way. For instance, the composition may be as shown in Figure 13. This unit support component 3a is composed by mounting device 217 having flat substrate 202 provided with six sets of magnetic support units 15c, 15d, ..., 15h at which gap sensors 37e, 37f; ..., ...; 37n, 37o are positioned on either side. Even if steel plate X is bending, the mean levitation gap width between steel plate X and individual magnetic support units 15c, 15d, ... can be obtained by gap sensors 37e, 37f; ... respectively provided on both sides of magnetic support units 15c, 15d , ... . The lower ends of rods 45a, 45b, 45c and 45d of linear guides 43a, 43b, 43c and 43d provided between it and baseplate 208 are connected to the upper surface of substrate 202 via universal joints 204a, 204b, 204c and 204d . Also, the lower ends of actuators 51a and 51b provided between it and baseplate 208 are connected to the upper surface of substrate 202 via links 206a and 206b which are capable of rotating in a plane parallel to the direction of advance of steel plate X. Baseplate 208 is provided with extensions 215a and 215b at its central part, apart from those at both ends. The following are provided at the two ends of central extensions 215a and 215b of baseplate 208 : linear guides 43i and 43j which are secured by thrusting through baseplate 208 ; rods 45i and 45j , provided with universal joints 204i and 204j at their lower ends and coil springs 47i and 47j, the lower ends of which are secured to substrate 202. Rods 45i 45j have a flexible proper structure to absorb mechanical measureing errer. Using this composition, substrate 202 is rotatable in the pitch direction, while detection of pitch angle and the amount of vertical travel is possible by the two linear guides 43i and 43j . Substrate 202 has no freedom in the vertical direction and the roll direction due to the action of links 206 . Therefore, by adapting zero power control, such as disclosed in Patent Application No. Heisei 4-351167 in the Japan Laid-Open Patents Gazette for instance, it is possible to support steel plate X without contact by using multiple unit support components 3a , while causing substrate 202 to follow the bending of steel plate X . In this case, needless to say, in the stationary levitation state, the coil currents of all magnetic support units 15c, 15d, ..., 15h converge to zero. When multiple magnets are provided in unit support components in this way, the load weight borne by each magnetic support unit becomes small. Therefore, the levitation gap width between the magnetic support unit and steel plate X can be made larger. Also, when substrate 202 is made to follow the bending of steel plate X, the support torque in the pitch direction acting on steel plate X becomes smaller. Thus, the deformation of steel plate X during levitation transport can be inhibited. In unit support component 3a, in the case when rods 45a, ... and actuators 51a, ... are secured to substrate 202 in place of universal joints 204a , ... and links 206a, ..., substrate 202 cannot be made to follow the bending of the steel plate. However, levitation control related to the pitching of substrate 202 is not required and so, needless to say, the system composition becomes simple. Moreover, in the above embodiment, unit support components are composed by mounting magnetic support units in inverse U-shaped track frames 13 , and control is performed only of the vertical motion and rolling of the steel plate centre of gravity, using steel plate X as the object to be transported. However, there is no restriction of any kind on the shape of the track frames, the mounting of the magnetic support units, the objects to be transported or the levitation control methods which are combinations of vertical motion and rolling control of the centre of gravity of the object to be transported. Various modifications are possible. For instance, there is no objection to arranging multiple unit support components provided with propulsion devices along the transport route, and causing the levitation and travel of the body to be levitated using an H-shaped cross-section provided with ferromagnetic bodies which are attracted to magnetic support units on both left and right sides. As a practical example, it may be magnetic track positioning type magnetic levitation transport system 1b, such as shown in Figure 14a. In magnetic track positioning type magnetic levitation transport system 1b, the track is formed of multiple U-shaped track frames 13b of unit support components 3b arranged along the transport route.- Magnetic support units 15 and stators 114a and 114b are mounted via mounting devices 17a, 17b, 112a and 112b by securing seats 31 to the inside side surfaces of the left and right extensions of the upper part of track frame 13b . Mounting devices 17a, 17b, 112a and 112b are composed by providing two baseplates 35a and 35b formed by dividing baseplates 35 of mounting devices 17 and 112 into two sections at their centres. Moreover, in mounting devices 17a and 17b , two substrates 39a and 39b are provided, formed by dividing substrate 39 into two sections at its centre. Stators 100a and 100b are positioned on the upper surface of the bottom of track frame 13b via height adjustment mechanisms 110a and 110b . Mounting devices 112a and 112b and height adjustment mechanisms 110a and 110b have the same positional relationships as in unit propulsion component 5, and the same height control is performed for each stator. Moreover, feed monitors 118a and 118b are arranged in positions at the front and rear ends of stators 100a and 100b which are provided on the upper surface of the bottom of track frame 13b. For linear guides 43a and 43b, two each are mounted on seats 31 of mounting devices 17a and 17b and mounting devices 112a and 112b and on baseplates 35a and 35b. Other than this, gap sensors 37, gap sensors 108, gap sensors 126 and each sensor of feed monitors 128a and 128b are arranged in the same way as in the cases of unit support components 3 and unit propulsion components 5 . At the same time, as shown in the essential part cross-section of Figure 14b , levitated body 216 , as the object to be transported, is composed by securing flat plate-shaped load bearer 210 and soleplate 212 via supporting plate 214 . Soleplate 212 is composed of flat plate 218 made of aluminium which is an electrically conductive, non-magnetic body. It is composed with ferromagnetic bodies, for instance iron strip-shaped flat plates 220, recessed into it in positions which will face stators 100a and 100b (positions to the left and right which sandwich supporting plate 214 ). Also, left and right strip-shaped plates 220 are positioned to face magnetic support units 15 as well, so that they generate levitating forces and guiding forces. In this embodiment, thrust control is the same as in unit propulsion component 5 . However, for levitation control, so-to-speak dual-purpose levitation and guidance control is performed, and rolling and left/right motion are stabilised by levitation control of the same roll direction as the left/right motion of the centre of gravity of levitated body 216 . Vertical motion of the centre of gravity is stabilised in the same way as in unit support component 3 . Moreover, stabilization of the yawing of levitated body 216 is designed by imparting thrusts, which differ to the left and right of levitated body 216, by stators 100a, 100b, 114a and 114b in the same way as in unit propulsion component 5. When the fore to aft length of soleplate 212 is determined so that it straddles at least three pairs of magnetic support units 15, a minimum of four support points is ensured, and the pitching of levitated body 216 is designed to be stabilised by determining the spring constants and damping factors of coil springs 47 and dampers 49 of mounting devices 17a and 17b at appropriate values. Also, height control is performed in the same way as in unit support components 3 for left and right magnetic support units 15 as well. Figure 15 shows a control block diagram for attraction control device 19b related to this embodiment. Figure 16 shows a control block diagram for height control system 122b , also related to this embodiment. In attraction control device 19b of Figure 15, roll/left and right motion modes control voltage operation circuit 222 , for dual-purpose levitation and guidance control, is provided in place of roll mode control voltage operation circuit 83 shown in Figure 3 mentioned above. In roll/left and right motion modes control voltage operation circuit 222 for dual-purpose levitation and guidance control, angles of inclination angles Δbs of substrates 39a and 39b of mounting devices 17a and 17b are introduced from height control system 122b , and are used for roll control of levitated body 216 . In height control system 122b of Figure 16, height adjustment sensor unit 63b is composed of linear guides 43a and 43b of mounting device 17a and linear guides 43a and 43b of mounting device 17b. Their outputs are introduced to height adjustment operation unit 65b, and deviations Δ zbsa and Δ zbsb of the respective heights of substrates 39a and 39b from the substrate height setting values of mounting devices 17a and 17b are calculated. Deviations Δzbsa and Δzbsb are introduced to substrate height coordinates conversion circuit 224, and mean deviation Δ zbs and inclination angle Δ bs are outputted from substrate height coordinates conversion circuit 224. At the same time, levitation height deviation Δz and levitation roll angle Δ of levitated body 216 relative to magnetic support units 15 are introduced to height adjustment operation unit 65b from height control system 122b. These are added to mean deviation Δzbs and inclination angle Δbs by two adders 94 via two changeover switches 92. The respective outputs of the two adders 94 are introduced to mean height mode excitation current operation circuit 226 and inclination mode excitation current operation circuit 228, and mode excitation currents izbs and ibs for actuators 51 in the respective modes are calculated. Outputs izbs and ibs of mean height mode excitation current operation circuit 226 and inclination mode excitation current operation circuit 228 are introduced to substrate height control current coordinates inversion circuit 230 , and motor excitation currents ida of the respective actuators 51 of mounting devices 17a and 17b are calculated. By this means, in magnetic track positioning type magnetic levitation transport system 1b also, it is possible to maintain the height of soleplate 212 of levitated body 216 constant, as in magnetic track positioning type magnetic levitation transport system 1. In this type of transport system, there is the advantage that the composition of the levitated body is extremely simple. Also, levitation control and guidance control in the roll direction of the levitated body is made dual-purpose using by levitation and guidance dual-purpose control. Thus, there is the advantage that there is no requirement to provide a separate guidance device and therefore the composition of the track is simple. Furthermore, in the embodiments described above, the control systems and their operations are expressed analogically. However, they are not limited to this type of control method, and digital methods may also be adopted. Also, a unit component composition which integrates several unit support components and unit guidance components or unit propulsion components may be used. Moreover, the system of this invention can be used in an entire painting process line, including the final drying process. In this way, this invention can be implemented in various modifications within limits which do not deviate from its purport. When using the magnetic track positioning type magnetic levitation transport system of the embodiment of this invention as described above, levitation control for perpendicular motion and levitation control for rolling of the object to be transported is performed at every unit support component. Moreover, it is also possible to inhibit pitching of the object to be transported between unit support components by the magnetic support units being capable of vertical movement due to the mounting devices. For this reason, even if, not only the total lengths of the objects to be transported, but also the total widths of the objects to be transported are varied, stable levitation can be performed by inhibiting the vertical motions and the rolling of the objects to be transported at every unit support component. Also, stabilization can be achieved by inhibiting the pitching of the objects to be transported using the mounting devices. Therefore, the whole of an object to be transported can be supported without contact. Furthermore, even if the weights and inertial moments of objects to be transported differ, this type of difference is distributed among the unit support components. Therefore, it is possible to support without contact objects to be transported with a wider range of weights and inertial moments as a magnetic track positioning type magnetic levitation transport system formed as a collection of individual unit support components. Also, it is possible to support multiple objects to be transported without contact on a single track. Furthermore, it can also respond smoothly to the shapes of objects to be transported. The following is a description of another embodiment of this invention with reference to the drawings. Figure 17 shows unit support component 303 which forms the track laid along the transport route of the magnetic track positioning type magnetic levitation transport system related to another embodiment of this invention. Structural components which are the same as structural components of the embodiment previously described are described by giving them the same symbols. Unit support component 303 is composed of inverse U-shaped track frame 13 , both ends of which are secured to bases 11 ; magnetic support units 15a and 15b which cause magnetic attraction to act on steel plate X in order to support the two ends of steel plate X , which is the object to be transported, in the width direction independently and without contact; mounting device 17 which is sandwiched between track frame 13 and magnetic support units 15a and 15b for mounting magnetic support units 15 on track frame 13 and attraction control device 19 which causes steel plate X to be supported without contact by controlling the attraction of magnetic support units 15a and 15b mounted in unit support component 303. Magnetic support unit 15a is for independently supporting without contact the right side in the width direction of steel plate X in the direction of travel. It is composed by sandwiching permanent magnet 21a by two electromagnets 27a and 27b which are made up of coils 23a and 23b and iron cores 25a and 25b . These two coils 23a and 23b are connected in series so that their magnetic fluxes reinforce each other by having the same excitation current. As opposed to this, magnetic support unit 15b is for independently supporting without contact the left side in the width direction of steel plate X in the direction of travel. It is composed by sandwiching permanent magnet 21b by two electromagnets 27c and 27d which are made up of coils 23c and 23d and iron cores 25c and 25d . These two coils 23c and 23d are connected in series so that their magnetic fluxes reinforce each other by having the same excitation current. Mounting device 17 is composed of two seats 31a and 31b which are each secured by welding to the under surface of the top of track frame 13 with a specified gap between them; baseplate 35 , on the centre of the lower side of which feed monitor 327 for detecting the presence and amount of left/right travel of steel plate X without contact is mounted via height control system 329 and seat 331 and, at the same time, which is guided so that it is permitted to move only in the vertical direction via guide mechanisms 33a and 33b; substrates 339a and 339b, on the underside of which are provided gap sensors 37a, ..., arranged on either side of each magnetic support unit 15a and 15b for measuring the gap widths between magnetic support units 15a and 15b, which are part of attraction control device 19, and steel plate X , together with magnetic support units 15a and 15b and height adjustment mechanisms 341a and 341b which are secured to the upper faces of substrates 339a and 339b and adjust the respective heights of substrates 339a and 339b by varying the distances between baseplate 35 and substrates 339a and 339b. Zero is outputted from feed monitor 327 when it is detected that steel plate X is not present. When the presence of steel plate X is detected, the amount of travel is outputted from the time of detection, taking the initial value as zero. Since guide mechanisms 33a and 33b have the same constructions as in the previously described embodiment, their descriptions have been omitted. Linear guides 43b and 43c have the dual purpose of travel distance meters for rods 45b and 45c . Also, height adjustment mechanisms 341a and 341b are composed of four linear guides 43a, 43b, 43c and 43d which are thrust through base plate 35 and secured; four rods 45a, 45b, 45c and 45d of which the lower ends are secured to substrates 339a and 339b, and the upper ends are guided by linear guides 43a, 43b, 43c and 43d so that they are free to move in the vertical direction and actuators 351a and 351b which are free to expand and contract, of which the tops are thrust through baseplate 35 and secured, and the lower ends are secured to the respective upper faces of substrates 339a and 339b . The expansion and contraction of actuator 351a is controlled by height control system 329 in order to control the height of substrate 339a at a specified value. Similarly, the expansion and contraction of actuator 351b is controlled by height control system 329 in order to control the height of substrate 339b to a specified value. The mean heights and angles of inclination of substrates 339a and 339b are controlled based on these expansions and contractions. In this embodiment, height adjustment mechanisms 341a and 341b have the dual purpose of inclination devices and height adjustment devices for steel plate X . Attraction control device 19 has the same composition as the attraction control device shown in Figure 3 of the previous embodiment. Its description has therefore been omitted. As shown in Figure 18, height control system 329 is composed by height adjustment sensor unit 361 which is composed of linear guides 43a and 43b and feed monitor 327 ; height adjustment operation unit 363, which takes as its inputs the output signals of height adjustment sensor unit 361, displacement signal Δz from the specified setting value of the levitation gap width and steel plate X detection signal TF obtained from attraction control device 19, and maintains the height of steel plate X during levitation at the specified value and, at the same time, when fluctuation occurs in the left/right position of steel plate X , calculates motor driving currents ida and idb of the respective actuators 351a and 351b of substrates 339a and 339b to guide steel plate X by adjusting the angles of inclination made by substrates 339a and 339b and current drivers 365a and 365b which are connected to a power source (not illustrated) and which drive the motors of actuators 351a and 351b based on outputs ida and idb of height adjustment operation unit 363 . In this way, height control system 329 has the dual-purpose of a height control device, which controls the height of steel plate X at a constant level, and an inclination angle control device, which controls the inclination of steel plate X . Height control operation unit 363 is composed of substrate height setter 389 which selectively outputs multiple specified set values, which are set for instance by the main computer, based on steel plate detection signal TF from attraction control device 19 ; operator 391a for subtracting the substrate height set value from the sum of output values he and hb of linear guide 43e and linear guide 43b which belongs to substrate 339a ; operator 391b for subtracting the substrate height set value from the sum of output values he and hc of linear guide 43e and linear guide 43c which belongs to substrate 339b; substrate height coordinates conversion circuit 393 which takes as its inputs outputs Δzbsa and Δzbsb of operators 391a and 391b, and outputs mean deviation Δ zbs obtained by averaging the deviations from the specified set values for the respective heights of substrates 339a and 339b and the angles of inclination Δ which are made by substrates 339a and 339b; guide position setter 395 which outputs a set value relating to the left/right guide position of steel plate X which is set by radio from the main computer (not illustrated); subtractor 397 for subtracting the output value of guide position setter 395 from output value ybs of feed monitor 327 ; guide angle of inclination operation circuit 399 which takes output Δybs of subtractor 397 as its input, calculates angles of inclination -Δbc made by substrates 339a and 339b, for guiding steel plate X in the left/right direction, based on this value, and outputs 0 when steel plate detection signal TF is 'NO' and outputs -Δbc after specified time t2 when TF changes from 'NO' to 'YES'; changeover switch 3101 which takes as its inputs deviation Δ z and steel plate detection signal TF from attraction control device 19 , and outputs Δ z when steel plate X is levitated beneath magnetic support units 15 and outputs 0 when that is not the case; adder 3102 which adds output Δzbs of substrate height coordinates conversion circuit 393 and the output of changeover switch 3101; subtractor 3105 which subtracts output -Δbc of guide angle of inclination operation circuit 399 from the same Δbs ; excitation current operation circuit 3111 composed of height mode excitation current operation circuit 3107 which calculates motor driving current izbs for actuators 351a and 351 related to the mean height of substrates 339a and 339b from the output of adder 3103 and angle of inclination mode excitation current operation circuit 3109 which calculates motor driving current ibs for actuators 351a and 351b related to the inclination made by substrates 339a and 339b from the output of subtractor 3105 and substrate height control current coordinates inversion circuit 3113 which takes as its inputs izbs and ibs of excitation current operation circuit 3111, and outputs control current values ida and idb which control the expansion and contraction of respective actuators 351a and 351b of substrates 339a and 339b . In changeover switch 3101, when steel plate detection signal TF changes from 'NO' to 'YES' switching from 0 to Δz is performed after specified time t2. The following is a description of the operation of the magnetic track positioning type magnetic levitation transport system related to the 'other' embodiment composed as described above. Here, Figure 19 shows the state when the magnetic track positioning type magnetic levitation transport system concerned in this embodiment is laid along a transport route, taking as its starting point the vicinity of the roller exit of a cold rolling mill. The magnetic track positioning type magnetic levitation transport system has a composition in which the transport path is formed by positioning the unit support components 303 concerned in this embodiment two by two between multiple unit propulsion components 5 which were illustrated by Figure 5. Three unit support components 303 are positioned at the exit of rollers 3191 of the cold rolling mill. In each unit support component 303 , when steel plate X is not present beneath magnetic support units 15 , no levitation control is performed, as in unit support components 303 shown by the symbol A . When steel plate X comes beneath magnetic support units 15, levitation control is performed by attracting the steel plate by lowering magnetic support units 15 , as in unit support components 303 shown by the symbol B. In the same way, with unit propulsion components 5 also, when steel plate X is not present between stators 100 and 114 of the linear induction motors, no propulsion control is performed, as in unit propulsion components 5 shown by the symbol C. When steel plate X comes between stators 100 and 114, propulsion control of the steel plate is performed by operating so that stator 100 rises and stator 114 falls, and so that they approach steel plate X , as in unit propulsion components 5 shown by the symbol D . Next, when describing the operation of this embodiment in practical terms by referring to Figure 3, Figure 18, etc., in each unit support component 303, when steel plate X is not present beneath magnetic support units 15, steel plate detection circuit 78 detects that steel plate X is not present since the output values of gap sensors 37a, ..., 37d, are large. Then, the fact that steel plate X is not present is transmitted to control voltage coordinates inversion circuit 86 by detection signal TF. Then, since zero is outputted instead of excitation voltages ea and eb , no levitation control is performed. Since detection signal TF is also transmitted to height control system 329 at this time, zero is selected by changeover switch 3101 and, at the same time, a smaller value than the set value when steel plate X is present is selected in substrate height setter 389. The sum of outputs he and hb of linear guides 43e and 43b expresses the height of substrates 339a and 339b . The set value of substrate height setter 389 is subtracted from the sum of he and hb in operators 391a and 391b. Then, when substrates 339a and 339b are not at the specified value outputs Δzbsa and Δzbsb of operators 391a and 391b are introduced to substrate height coordinates conversion circuit 393 of height control system 329. Also, since steel plate X is not present underneath, the output of feed monitor 327 becomes zero. At the same time, since detection signal TF which indicates that there is no steel plate X is transmitted from attraction control device 19, the output of guide angle of inclination operation circuit 399 also becomes zero. In substrate height coordinates conversion circuit 393, the mean heights and inclinations of substrates 339a and 339b are calculated based on Δzbsa and Δzbsb, and Δzbs and Δbs are outputted. In excitation cur'rent operation circuit 3111, ida and idb are operated so that Δzbs and Δbs converge to zero, and the motors of actuators 351a and 351b are driven by current drivers 365a and 365b. By this means, substrates 339a and 339b are set in a higher position than when steel plate X is present, while maintaining a horizontal positional relationship. When substrates 339a and 339b are set at the high position (shown by symbol A in Figure 19 ) in this way, even if steel plate X arrives under levitation at that unit support component 303, not only will steel plate X not come into contact with magnetic support units 15, but also a sufficient gap can be ensured between magnetic support units 15 and steel plate X. Therefore, steel plate X will not be adsorbed by the attraction of permanent magnets 21a and 21b either. The operation of unit propulsion components 5 is the same as described and shown in Figure 5 and Figure 6 of the previous embodiment. When steel plate X arrives beneath magnetic support units 15 of unit support component 303, the output values of gap sensors 37a ~ 37d become smaller than the specified value. Therefore, steel plate detection circuit 78 detects that steel plate X is present. Then, the fact that steel plate X has arrived beneath magnetic support units 15 of unit support component 303 is transmitted to substrate height setter 389 and changeover switch 3101 of height control system 329 by detection signal TF . Then, the setting value for when steel plate X is present is selected in substrate height setter 389. In operators 391a and 391b, the setting value of substrate height setter 389 is subtracted from the sum of outputs he and hb of linear guides 43e and 43b, and Δzbsa and Δzbsb are outputted. When substrates 339a and 339b are not at the set value, the output of changeover switch 3101, which selects zero, and Δzbs are added by adder 3103, and output Δzbs of substrate height coordinates conversion circuit 393 is introduced to height mode excitation current operation circuit 3107. At the same time, feed monitor 327 detects steel plate X and starts the output of travel amount ybs. In subtractor 397, the zero set value output of guide position setter 395 is subtracted from ybs, and Δybs is outputted. At this time, if specified time t2 has not elapsed, guide angle of inclination operation circuit 399 outputs zero. For this reason, the zero output of guide angle of inclination operation circuit 399 and Δbs are subtracted by subtractor 3105, and output Δbs of substrate height coordinates conversion circuit 393 is introduced to inclination mode excitation current operation circuit 3109. izbs and ibs are operated in excitation current operation circuit 3111 so that Δzbs and Δbs converge to zero. Current drivers 365a and 365b drive the motors of actuators 351a and 351b based on outputs ida and idb of substrate height control current coordinates inversion circuit 3113. By this means, substrates 339a and 339b are set at the set height when steel plate X is present. At this time, output Δzbs of substrate height coordinates conversion circuit 393 is also introduced to vertical motion mode control voltage operation circuit 82 of attraction control device 19. At the same time, steel plate detection signal TF of steel plate detection circuit 78 shown in Figure 3 is also transmitted to control voltage coordinates inversion circuit 86 . After substrates 339a and 339b have been set to the set height, that is to say after specified time t1 from receiving detection signal TF, excitation voltages ea and eb are outputted to start levitation control. In levitation control, output values za, zb, zc and zd of gap sensors 37a ~ 37d are subtracted from the output of levitation gap width setter 70 by subtractors 74a ~ 74d. The results of these subtractions are introduced to levitation gap width deviation coordinates conversion circuit 80, and deviation Δz from the specified position of the centre of gravity coordinates of the part of steel plate X which overlaps the unit support component and roll angle Δ of the same part of steel plate X are calculated. At the same time, excitation current measurement values ia and ib of electromagnets 23a and 23b detected by current detectors 55a and 55b are subtracted from the zero output of current setter 72 by subtractors 76a and 76b . The results of these subtractions are introduced to excitation current deviation coordinates conversion circuit 81, and coil excitation current Δ iz which contributes to the vertical motion of the centre of gravity of the part of steel plate X overlapping unit support component 303 and coil excitation current Δ i  which contributes to the rolling of the same part of steel plate X are calculated. Out of Δ z , Δ, Δ iz and Δ i , Δ z and Δ iz are introduced to vertical motion mode control voltage operation circuit 82 , together with output Δ zbs of substrate height coordinates conversion circuit 393 . Here, coil excitation voltage ez , which contributes to the vertical motion of the centre of gravity of the part of steel plate X overlapping unit support component 303, is calculated. When ez is calculated, Δiz converges to zero in the stationary levitation state of steel plate X , that is to say zero power control is performed. At the same time, Δ and Δi are introduced to roll mode control voltage operation circuit 83 of Figure 3, and coil excitation voltage e , which contributes to the rolling of the same part of steel plate X, is calculated. When e is calculated also, Δi converges to zero in the stationary levitation state of steel plate X , in other words, zero power control is performed. Outputs ez and e of control voltage operation circuit 84 of Figure 3 are introduced to control voltage coordinates inversion circuit 86, and excitation voltages ea and eb for respective electromagnets 27 are calculated. By this levitation control, ia and ib in the stationary levitation state of steel plate X converge to zero, in other words, zero power control (Laid-Open Patent No. Showa 61-102105 Gazette) is achieved as a whole. In this way, if levitation control which contributes to the vertical motion of the centre of gravity of the part of steel plate X overlapping unit support component 303 and levitation control which contributes to the rolling of the same part of steel plate X are performed in every mode, it is possible to design levitation control systems in the respective modes. Therefore, robust levitation control can be performed for variations of weight per unit length of steel plate X and for variations of material and thickness. Also, during the time for levitation control to reach the stationary levitation state, the weight of steel plate X is loaded on coil springs 47 and dampers 49. Thus, even if output ha of linear guide 43a fluctuates, height control will be performed in height control system 329 to maintain substrates 339a and 339b at the set height. At the same time, since the fluctuations pf Δzbs and Δbs which accompany height control are introduced to control voltage operation circuit 85 , stable levitation control can be achieved. Moreover, if steel plate X is stably levitated by zero power control, the levitation gap width between magnetic support units 15 and steel plate X becomes a width which balances the attraction of permanent magnets 21 and the load weight of steel plate X . The levitation gap width at this time differs from the output value of levitation gap width setter 70, and Δz is outputted in levitation gap width deviation coordinates conversion circuit 80. This output is introduced to changeover switch 3101 of height control system 329. Then, after specified time t2 from the reception of steel plate detection signal TF of steel plate detection circuit 78 to the stable levitation of steel plate X , it is outputted from changeover switch 3101. By this means, (Δzbs + Δz) is outputted by the adder of the height control system. Therefore, substrates 339a and 339b travel to a position which is only Δ z higher than the specified height. Furthermore, after specified time t2 from reception of steel plate detection signal TF of steel plate detection circuit 78 to the stable levitation of steel plate X , guide angle of inclination operation circuit 399 starts to output. At this time, as shown in Figure 20a, if steel plate X inclines to either the left or right direction with regard to the track centre, the left/right travel amount is detected by feed monitor 327, and Δybs is introduced to guide angle of inclination operation circuit 399 via subtractor 397 . In guide angle of inclination operation circuit 399 , the angles of inclination of substrates 339a and 339b are operated to make Δybs converge to zero, and Δbs + Δbc are introduced to inclination mode excitation current operation circuit 3109 via subtractor 3105. For this reason, as shown in Figure 20b, substrates 339a and 339b travel vertically to make an angle of inclination of -Δbc , and a force in a direction to cancel Δybs acts on steel plate X . By this means, Δybs converges to zero, and steel plate X is maintained in a position which corresponds to the guide position setting value of guide position setter 395. By this operation, even if the weight per unit length of steel plate X which unit support component 303 supports varies, its upper surface will always be levitated at a constant height. At the same time, even if a lateral external force acts on steel plate X , rolling will be rapidly damped, and it will be transported along the track while maintaining a stable state. Here, if a levitation gap width setting value which takes into consideration thickness data for steel plate X is set in the main computer, it goes without saying that it is possible always to levitate the position of the centre of the thickness of steel plate X at a constant height. If steel plate X can be levitated at a constant height in this way, not only does dimensional compatibility with other systems become simple, but also the initial values of the gap widths between magnetic support units 15 and steel plate X when levitation control is initiated in unit support components 303 by the fresh arrival of steel plate X are the same for each unit support component 303. Therefore, the shocks at the initiation of levitation control applied to unit support components 303 which are already supporting steel plate X can be made the same. Thus, there is the advantage that control system design for the absorption of this shock by attraction control device 19 becomes simple. Also, if a guide position setting value for steel plate X is set in the main computer taking account of the left/right position of the steel plate, it is possible to transport steel plate X while giving it a specified deviation in the lateral direction. Even if there is a unit support component 303 which is offset from the specified position in the track, if the guide position set value of the error potion of the set position is set, there will be no requirement to cause an excess guiding force to act on steel plate X . Therefore, there will be the advantage of being able to achieve smooth transport. Moreover, in this embodiment, zero power control is used for levitation control. However, steel plate X is supported without contact by this type of zero power control, the levitation gap width of magnetic support unit 15 in which the load is increased due to the inclination of steel plate X will decrease. Therefore, by inclining the steel plate in the opposite direction to the fore/aft left/right slippage of steel plate X , further effect will be given to guidance control. In other words, the attraction control device has the dual purpose of an angle of inclination control device. After the passage of steel plate X through unit support component 303 is completed, the output values of gap sensors 37a ~ 37d become larger and therefore steel plate detection circuit 78 detects that there is no steel plate. Then, by the operation in the above-mentioned case when steel plate X is not beneath magnetic support units 15, levitation control of unit support component 303 is stopped. At the same time, substrates 339a and 339b are set in higher positions than when steel plate X is present, and maintain this state until the arrival of the next steel plate. Steel plate X which is supported without contact by unit support component 303 travels due to unit propulsion component 5 . The above levitation control and height control are successively commenced by all the unit support components 303 at which steel plate X has arrived. At this time, bending in the vertical direction sometimes occurs along the direction of advance of steel plate X due to elasticity. This bending becomes a disturbance in the vertical direction in individual unit support components 303 . In two neighbouring unit support components 303 , it becomes pitching of the steel plate parts supported by them. In attraction control device 19, shown in Figure 3, of each unit support component 303 , levitation control is performed in relation to the vertical motion and the rolling of the centre of gravity of steel plate X by vertical motion mode control voltage operation circuit 82 and roll mode control voltage operation circuit 83. However, if the respective spring constants and damping factors of coil springs 47 and dampers 49 of mounting device 17 are set at appropriate values, it becomes possible to accelerate the pitching convergence of the steel plate. In this embodiment, the bending of steel plate X can be effectively inhibited by accelerating the pitching convergence of the steel plate. In other words, levitation control in the pitch direction of steel plate X is performed by coil springs 47 and dampers 49 of mounting device 17. Therefore, the whole of steel plate X can be stably levitated. Also, as shown in Figures 19, when the rolling of steel plate X is damaged by the rollers, etc. of the cold rolling mill, output e of roll mode control voltage operation circuit 83 of Figure 3 becomes zero through an appropriate device (not illustrated). In each unit propulsion component 5, as described in the previous embodiment, when steel plate X has passed through unit support component 303, linear motor excitation control of unit propulsion component 5 stops by the operation when the fact that steel plate X is not present is detected. At the same time, stators 114 are set in higher positions and stators 100 are set in lower positions than when steel plate X is present, and maintain this state until the next steel plate X arrives. In this way, steel plate X travels to its destination while being levitated without contact without leaving the track which is composed of unit support components 303 and unit propulsion components 5 . In the above embodiment, mounting device 17 is composed of guide mechanisms provided with coil springs, dampers and linear guides, etc. and height adjustment mechanisms provided with actuators, linear guides, etc. However, the composition of the mounting devices is not in any way limited to this. Various modifications are possible, provided magnetic support units 15 have compositions which are able to move vertically. For instance, unit support component 303 may be composed as shown in Figure 21. This unit support component 303 may be composed by securing baseplate 35 to track frame 13 by supports 319a , .... At the same time, mounting devices 313' may be composed by sandwiching load cells 3195 between baseplate 35 and substrates 339a and 339b . In this case, any forces in the vertical direction applied to mounting devices 313' are measured by load cells 3195 . Thus, it goes without saying that, by performing height control using the outputs of load cells 3195 , the same function can be achieved as in the case of using coil springs and dampers. Also, in the above embodiment, substrates 339a and 339b are respectively provided with one magnetic support unit 15 each. However, this does not restrict the number of magnetic support units used in unit support component 303 in any way. For instance, the composition may be as shown in Figure 22. Unit support component 303 shown in Figure 22 has flat plate-shaped substrate 202 provided with six sets of magnetic support units 15c, 15d, ..., 15h at which gap sensors 37e, 37f; ..., ...; 37n, 37o are positioned on either side. Even if steel plate X is bending, the mean levitation gap width between steel plate X and individual magnetic support units 15c, 15d , ... can be obtained by these gap sensors 37e, 37f; ... on both sides. Substrate 202 is provided with feed monitors 327a and 327b in the centre at the front and rear. By taking the mean of the outputs of these feed monitors 327a and 327b, the mean left/right travel amounts of steel plate X in relation to substrate 202 are obtained. Since the left/right travel amount components are cancelled by the yawing of steel plate X , more accurate guidance control can be obtained than in the case of unit support component 303. Moreover, substrate 202 is connected to rods 45a, ... and actuators 351a and 351b via universal joints 204a, 204b, ..., 204h on the lower ends of rods 45a , ... and on the lower ends of actuators 351a and 351b. Also, extensions are provided to baseplate 208 at both ends and in the centre part. The following are provided at the two ends of the central extensions of baseplate 208 : linear guides 43i and 43j which are secured by thrusting through baseplate 208 ; rods 45i and 45j, provided with universal joints 204i and 204j at their lower ends and coil springs 47i and 47j, of which the upper ends are secured to baseplate 208 and the lower ends are secured to substrate 202 . The universal joint has prepared with suitable flexible mechanical structure in order to absorb mechanical measureing errer. By this composition, substrate 202 becomes rotatable in the pitch direction. At the same time, detection of the pitch angle, the roll angle and the vertical travel amount of substrate 202 by three linear guides 43b, 43e and 43i becomes possible. Also, substrate 202 has no freedom in the vertical direction or the roll direction due to the actions of actuators 351a and 351b . Therefore, due to the application of the zero power control described in detail in the Specification of Patent Application No. Heisei 4-351167, steel plate X is supported without contact by the use of multiple unit support components 303a. At the same time, it is possible for substrate 202 to follow the bending in the transport direction of steel plate X. In this case, it goes without saying that all the coil currents of magnetic support units 15c, ... converge to zero. When a large number of magnets is provided in unit support component 303a in this way, the load weight exerted on each magnetic support unit 15a , ... decreases. Therefore, not only is it possible to increase the gap widths between magnetic support units 15 and steel plate X , but also the supported weight and magnetic flux per magnetic support unit 15, ... decrease. Thus, even if the object to be transported is a thin steel plate, saturation of magnetic flux can be avoided and stable non-contact support becomes possible. Also, since substrate 202 follows the bending of steel plate X, the supporting force in the pitch direction becomes smaller and deformation of the steel plate during levitation transport can be inhibited. Moreover, in the above embodiment, unit support component 303a is composed by mounting magnetic support units 15 , ... in inverse U-shaped track frame 13 , and levitation control is applied in relation to the vertical motion and rolling of the steel plate centre of gravity, taking steel plate X as the object to be transported. At the same time, guidance control is performed by inclining steel plate X in the transverse direction. However, there is no restriction of any kind on the shape of the track frames or the composition of the unit support components, nor on the objects to be transported. Various modifications are possible. When using the magnetic track positioning type magnetic levitation transport system of the embodiment described above, levitation control of the perpendicular motion of the steel plate and levitation control of its rolling are performed at every unit support component. At the same time, guidance control of the steel plate is performed by generating angle of inclination in the magnetic support units on the left and right of the unit support components. Also, it becomes possible to inhibit the pitching of the steel plate between unit support components by the fact that the magnetic support units are vertically movable due to the mounting system. For this reason, even if, not only the whole length of the steel plate, but also the whole width of the steel plate is varied, the vertical motion and the rolling of the steel plate can be stably levitated at every unit support component, and also, the pitching of the steel plate can be stabilised by the mounting devices. Also, the magnetic support units which provide levitation can have the dual purpose of guidance of the steel plate in the left/right direction. Thus, it becomes possible simultaneously to perform the non-contact support and guidance of the whole steel plate with a simple composition. Moreover, even in cases where the weights and inertial moments of steel plates differ, this type of deviation is distributed to each unit support component. At the same time, the guiding force which acts on the steel plate through the inclination of the magnetic support units is proportional to the distributed weight of the steel plate. Thus, the acceleration in the transverse direction of the steel plate becomes constant, despite the distributed weight. Therefore, it is possible for the magnetic track positioning type magnetic levitation transport system as a whole which is formed of a collection of individual unit support components to support without contact and guide steel plates possessing a broader range of weights and inertial moments. Also, it is possible to support multiple steel plates without contact on a single track. Furthermore, levitated bodies other than steel plates can be supported, and the composition of the levitated bodies can be made extremely simple. The following is a description of a further embodiment of this invention. A steel plate transport system which uses the magnetic levitation system concerned in an embodiment of this invention is shown in Figure 23 and Figure 24. Steel plate transport system 412 is composed of track 414 laid on a specified route and transporter 416 provided with magnetic levitation system 410 concerned in this invention. Track 414 is formed by installing track support units 422, made by securing L-shaped track support columns 418 on the upper surfaces of baseplates 420 , to the left and right of the transport route, and securing guide rails 424 with L-shaped cross-sections to respective track support units 422 . Track support columns 418 are formed of insulating components, while guide rails 424 are formed of conducting components. Left and right guide rails 424 are connected to a power source (not illustrated) by a specified method. Transporter 416 is composed by mounting driving units 426 on the upper four corners of magnetic levitation system 410. It is arranged so that it is free to run along track 414. Driving units 426 are composed of wheels 428 ; motors 430 which drive wheels 428 and running control system 432 which runs, stops and reverses transporter 416 by controlling motors 430 through external radio instructions. Wheels 428 are conductive members. They supply the required power to magnetic levitation system 412 and driving units 426 by making contact with left and right guide rails 424 . Magnetic levitation system 410 is composed of 'hash'-shaped substrate 434 ; inclining devices 436 mounted on the flat-shaped components at the front and rear parts of substrate 434 ; flat-shaped frame 438 joined to inclining devices 436 via universal joints 437 ; a total of six magnet units 440, three of which are positioned in a line on each of the left and right undersides of frame 438; gap sensors 444 which are positioned on both sides of each magnet unit 440 for non-contact measurement of the gap widths between magnet units 440 and steel plate 442 which is the object to be transported; feed monitors 446 which are positioned at the front and rear ends of the central parts of the underside of frame 438 for non-contact measurement of the travel amounts in the transverse direction of the parts of steel plate 442 which face them; feed monitors 448 which are positioned in the centre parts of the left and right sides of the underside of frame 438 for non-contact measurement of the travel amount in the fore and aft directions of the parts of the steel plate which face them; eight guide bars 450 which are positioned so that they enclose the four corners of frame 438 to prevent the escape of steel plate 442 from the available non-contact support region produced by magnet units 440 ; magnetic support control device 452 for the non-contact support of steel plate 442 by controlling the attraction of magnet units 440 and angle of inclination control device 454 for guiding steel plate 442 by controlling the angle of inclination of frame 438 using inclination device 436 for preventing the escape steel plate 442 from the available non-contact support region produced by magnet units 440 . Here, running control system 432, magnetic support control system 452 and angle of inclination control system 454 are secured on top of the 'hash'-shape left and right members of substrate 434 , as shown in Figures 23 and 24. Also, universal joints 437 have structures provided with appropriate flexibility for absorbing mechanical dimensional errors. Feed monitor 446 and feed monitor 448 are designed to output zero respectively when steel plate 442 is distanced from a specified position. As shown in Figure 24, magnet units 440 are each composed of permanent magnets 456 sandwiched by two electromagnets 452 made up of coils 458 and iron cores 460 . The two coils 458 are connected in series so that their magnetic fluxes reinforce each other by having the same excitation current. As shown in Figure 25, running control system 432 is composed of running constant voltage source 464 which introduces the power of a power source (not illustrated) from guide rails 424 via left and right wheels 428 and generates a specified constant 3-phase alternating current; four inverters 468 which excite each motor 430 based on frequency instruction value ω from excitation frequency operator 466 ; running control unit 474 which is provided with four speed detectors 470 for operating the running speed of transporter 416 from the number of revolutions of each wheel 428; speed instruction generator 472 which outputs the target running speed of transporter 416 through radio from outside and excitation frequency operator 466 which operates the four frequency instruction values ω from speed detectors 470 and speed instruction value generator 472 for exciting each motor 430 so that transporter 416 runs at the target running speed and control constant voltage source 476 which introduces the power source voltage from guide rails 424 via left and right wheels 428 and generates and supplies a specified constant voltage to running control unit 474 . In the control block diagrams from Figure 25 onwards, the solid lines show power routes, while the arrows show signal routes. Inclination device 436 is composed of four actuators 478 which are free to expand and contract in the vertical direction and are mounted on the front and rear flat plate-shaped members of 'hash'-shaped substrate 434 by being thrust through them at specified intervals; eight linear guides 480 mounted on the front and rear flat plate-shaped members of substrate 434 by being thrust through them and eight rods 482 which are moveable only in the vertical direction and are thrust through each linear guide 480 . Actuators 478 and rods 482 are connected to flat plate-shaped frame 438 via universal joints 437 . Also, the expansion and contraction of actuators 478 is controlled by angle of inclination control device 454. By this means, it is possible for inclination device 436 to support frame 438 at a specified inclination and a specified height. Here, linear guides 480 have the dual purpose of travel distance meters for rods 482. The following is a description of magnetic support control device 452 with reference to Figure 26. Magnetic support control device 452 is composed of twelve gap sensors 444 (gap sensors 444a-1, 444a-2, 444b-1, 444b-2, ..., 444f-1, 444f-2) which are close to the left and right of each magnet unit 440 , and measure the levitation gap widths between the respective magnet units 440 and steel plate 442 ; levitation sensor unit 486 composed of current detectors 484a , 484b, 484c, 484d, 484e and 484f for measuring excitation currents flowing in the coils of electromagnets 462 ; levitation operation unit 488 which takes as its inputs output signals za-1, za-2, ..., zf-1, zf-2 and ia, ib, ..., if of levitation sensor unit 486, and calculates excitation voltages ea, eb, ..., ef for every magnet unit 440 required for the levitation of steel plate 442; levitation constant voltage source 490 which introduces the power of a power source (not illustrated) from guide rails 424 via left and right wheels 428 , and generates a specified constant voltage; power amplifiers 492a, 492b, ..., 492f which are connected to levitation constant voltage source 490 , and excite coils 458 of magnet units 440 based on outputs ea, eb, ..., ef of levitation operation unit 488 and control constant voltage source 493 which is supplied with power from a power source (not illustrated) via guide rails 424 and wheels 428 , and supplies a specified constant voltage to gap sensors 444 and levitation operation unit 488 . Levitation operation unit 488 is composed of levitation gap width setter 494 and levitation current setter 496, which output specified setting values which are set by, for instance, radio from the main computer; mean value operation circuit 498 which averages the outputs of gap sensors 444 positioned to the left and right of each magnet unit 440 , and outputs mean levitation gap widths za, zb, ..., zf for steel plate 442 and magnet units 440; subtractors 500a, 500b, ..., 500f for subtracting the levitation gap width set values from the respective output values za, zb, ..., zf of mean value operation circuit 498 ; subtractors 502a, 502b, ..., 502f for subtracting the current set value from outputs ia, ib, ..., if of current detectors 484a, 484b, ..., 484f ; steel plate detection circuit 504 which judges from output values za-1, za-2, ..., zf-1, zf-2 whether steel plate 442 is present in a position beneath all magnet units 440 and within the available levitation region due to magnet units 440 and, at the same time, commences this judgement based on a transport initiation instruction from the main computer (not illustrated); levitation gap width deviation coordinates conversion circuit 506 for obtaining from the output values of subtractors 500a, 500b, ..., 500f deviation Δz from the specified position of the centre of gravity coordinates of steel plate 442; pitch angle Δξ of steel plate 442; roll angle Δ of steel plate 442 and the three twist mode deviations relating to the twisting of steel plate 442 beneath the four corner positions of frame 438 ; the twisting of steel plate 442 below the front and rear ends of frame 438 and the position in the centre of frame 438 and the bending of steel plate 442 below the front and rear ends of frame 438 and the position in the centre of frame 438 ; excitation current deviation coordinates conversion circuit 508 for obtaining coil excitation current Δiz which contributes to the vertical motion of the centre of gravity of steel plate 442 ; coil excitation currents Δiξ and Δi which contribute to the pitching and rolling of steel plate 442 and the three twist mode excitation currents relating to the twisting of steel plate 442 beneath the four corner positions of frame 438; the twisting of steel plate 442 below the front and rear ends of frame 438 and the position in the centre of frame 438 and the bending of steel plate 442 below the front and rear ends of frame 438 and the position in the centre of frame 438; control voltage operation circuit 518 composed of vertical motion mode control voltage operation circuit 510 which takes as it inputs outputs Δz and Δiz of levitation gap width deviation coordinates conversion circuit 506 and excitation current deviation coordinates conversion circuit 508 , and calculates coil excitation voltage ez which contributes to the vertical motion of the centre of gravity of steel plate 442 ; pitch mode control voltage operation circuit 512 which takes as its inputs outputs Δξ and Δiξ of levitation gap width deviation coordinates conversion circuit 506 and excitation current deviation coordinates conversion circuit 508, and calculates coil excitation voltage eξ which contributes to the pitching of steel plate 442 ; roll mode control voltage operation circuit 514 which takes as its inputs outputs Δ and Δi of levitation gap width deviation coordinates conversion circuit 506 and excitation current deviation coordinates conversion circuit 508, and calculates coil excitation voltage e which contributes to the rolling of steel plate 442 and twist mode control voltage operation circuit 516 which takes as its inputs the above three twist mode deviations and twist mode excitation currents, and calculates the three excitation voltages which relate to the respective twist modes; and control voltage coordinates inversion circuit 520 which takes as its inputs outputs ez, eξ and e of control voltage operation circuit 518 and detection signal TF of steel plate detection circuit 504, and calculates excitation voltages ea, eb, ..., ef which excite respective magnet units 440 when steel plate 442 is present below frame 438. In control voltage coordinates inversion circuit 520, when steel plate detection signal TF changes from 'NO' to 'YES', changeover is performed from six zero outputs to ea, eb, ..., ef after specified time t1 . The following is a description of angle of inclination control device 454 with reference to Figure 27. Angle of inclination control device 454 is composed of four linear guides 480a, 480b, 480c and 480d which output the travel distances zbsa ~ zbsd of linear guides 480, which are frame 438 height information; guidance sensor unit 522 made up of feed monitors 448a and 448b, which output the fore and aft travel amounts xbsa and xbsb of the left and right parts of steel plate 442 , and feed monitors 446a and 446b which output transverse travel amounts ybsa and ybsb of the front and rear parts of steel plate 442 ; guidance operation unit 524 which introduces presence detection signal TF for steel plate 442 and steel plate 442 centre of gravity gap width deviation signal Δz which are outputted from magnetic support control device 452 and output signals zbsa ~ zbsd, xbsa, xbsb and ybsa, ybsb of guidance sensor unit 522 , and calculates control current values ida ~ idd which control the expansion and contraction of four actuators 478 for guiding steel plate 442 in the fore and aft and transverse directions; guidance constant voltage source 525 which generates a specified constant voltage; current drivers 526a ~ 526d which are connected to guidance constant voltage source 525, and which cause actuators 478 to expand and contract by driving the motors of actuators 478 based on outputs ida ~ idd of guidance operation unit 524 and control constant voltage source 527 which is supplied with power from a power source (not illustrated) via guide rails 424 and wheels 428 , and supplies a specified constant voltage to guidance sensor unit 522 and guidance operation unit 524 . Guidance operation unit 524 is composed of frame height setter 528 which selectively outputs multiple set values related to the height of the centre of gravity of frame 438 , which are set by radio from the main computer (not illustrated), based on steel plate detection signal TF from magnetic support control device 452 ; front and rear position setter 530 which outputs set values related to the front and rear positions of steel plate 442 which are set by radio from the main computer (not illustrated) ; left and right position setter 532 which outputs set values related to the left and right positions of steel plate 442 which are set in the same way; subtractor 534 for subtracting the output values of frame height setter 528 from output values zbsa ~ zbsd of linear guides 480 ; subtractor 536 for subtracting the output values of front and rear position setter 530 from outputs xbsa and xbsb of feed monitors 448 ; subtractor 538 for subtracting the output values of left and right position setter 532 from outputs ybsa and ybsb of feed monitors 446; frame height coordinates operation circuit 540 which takes as its inputs outputs Δzbsa ~ Δzbsd of subtractor 534, and calculates deviation Δzbs from the set value of the centre of gravity height of frame 438 and pitch angle Δξbs and roll angle Δbs of frame 438; guidance control circuit 546 which consists of front and rear angle of inclination operation circuit 542 which takes as its inputs outputs Δxbsa and Δxbsb of subtractor 536 , and calculates pitch angle Δξbc of frame 438 based on these values for guiding steel plate 442 in the front and rear directions and left and right angle of inclination operation circuit 544 which takes as its inputs outputs Δybsa and Δybsb of subtractor 538, and calculates roll angle -Δbc of frame 438 based on these values for guiding steel plate 442 in the transverse direction, and which outputs 0 and 0 when steel plate detection signal TF is 'NO', and outputs Δξbc and -Δbc after specified time t2 when TF changes from 'NO' to 'YES'; changeover switch 548 which takes as its inputs deviation Δz and steel plate detection signal TF from magnetic support control device 452, and outputs Δz when steel plate 442 is levitated beneath all magnet units 440, but outputs 0 when that is not the case; adder 550 which adds output Δzbs of frame height coordinates operation circuit 540 and the output of changeover switch 548; subtractor 552 which subtracts output Δξbc of guidance control circuit 546 from output Δξbs of frame height coordinates operation circuit 540; subtractor 554 which subtracts output -Δbc of guidance control circuit 546 from output Δbs of frame height coordinates operation circuit 540 ; excitation current operation circuit 562 which consists of mean height mode excitation current operation circuit 556 which calculates motor drive current izbs of actuators 478 related to the centre of gravity height of steel plate 442 from the output of adder 550 ; front and rear inclination mode excitation current operation circuit 558 which calculates motor drive current iξbs of actuators 478 related to the pitching of frame 438 from the output of subtractor 552 and left and right inclination mode excitation current operation circuit 560 which calculates motor drive current ibs of actuators 478 related to the rolling of frame 438 from the output of subtractor 554 and frame height control voltage coordinates inversion circuit 564 which takes as its inputs outputs izbs, iξbs and ibs of excitation current operation circuit 562 , and outputs control current values ida ~ idd which control the expansion and contraction of the four actuators 478 . In frame height setter 528, selection of the set height is performed after specified time t2 when steel plate detection signal TF changes from 'NO' to 'YES'. At the same time, in changeover switch 548, changeover from 0 to Δz is performed after specified time t3 when steel plate detection signal TF changes from 'NO' to 'YES'. The following is a description of the operation of the magnetic levitation system concerned in this embodiment which is composed as described above. First, the case in which steel plates 442 placed in a specified location on track 414 are transported to another specified location by multiple transporters 416 is described using Figure 28. In Figure 28, 566 is a pedestal on which steel plate 442 is to be placed. First, the circumstances in Figure 28(a) are described. When a running speed is instructed by the main computer, the instructed speed is set in speed instruction value generator 472 running control system 432 in transporter 416 . The actual wheel speed of speed detector 470 is compared with the speed instruction value. Excitation frequency ω which causes motor 430 to rotate is outputted by excitation frequency operator 466 so that these will agree. Thus, transporter 416 rapidly runs at the instructed speed. At this time, since transporter 416 is not transporting steel plate 442 , no transport initiation instruction is outputted from the main computer. For this reason, in magnetic support control device 452 , a TF signal indicating that there is no steel plate is outputted by steel plate detection circuit 504 which introduces the outputs of all gap sensors 444. This detection signal TF is transmitted to control voltage coordinates inversion circuit 520, and control voltage coordinates inversion circuit 520 outputs zero. Therefore, coil 458 is not excited. Also, detection signal TF is also transmitted to angle of inclination control device 454 . Thus, in frame height setter 528 , specified height h1, at which magnet unit 440 will not adsorb steel plate 442 by the attraction of permanent magnet 456, is outputted. At the same time, in guidance control circuit 546, 0 and 0 are outputted in place of Δξbc and -Δbc , and guidance control is not performed. Moreover, in feed monitors 446a and 446b and feed monitors 448a and 448b , front and rear and transverse travel amounts xbsa, xbsb and ybsa, ybsb become zero since steel plate 442 is not present. At the same time, when outputs zbsa ~ zbsd of linear guides 480a, 480b, 480c and 480d differ from output value h1 of frame height setter 528, Δzbs, Δξbs and Δbs are calculated by frame height coordinates operation circuit 540 based on outputs Δzbsa ~ Δzbsd of subtractor 534, while the three zero outputs from changeover switch 458 and guidance control circuit 546 are added/subtracted to/from Δzbs, Δξbs and Δbs in adder 550, subtractor 552 and subtractor 554 and introduced to control voltage operation circuit 518. In control voltage operation circuit 518, the respective excitation currents izbs, iξbs and ibs are calculated for the mode related to the centre of gravity height of frame 438 which converges deviation Δzbs to zero, the mode related to the inclination in the front and rear directions of frame 438 which converges deviation Δξbs to zero and the mode related to the inclination in the left/right directions of frame 438 which converges deviation Δbs to zero. Outputs izbs, iξbs and ibs of control voltage operation circuit 518 are converted to motor driving current values ida ~ idd in frame height control current coordinates inversion circuit 564 , and actuators 478 are driven via current drivers 526 . In this way, the expansions and contractions of actuators 478 are controlled, and frame 438 is maintained level at frame height set value h1 . In due course, when transporter 416 arrives above pedestal 566, the running speed instruction value is set at zero, and transporter 416 rapidly stops. At this time, steel plate 442 is positioned on pedestal 566 , as shown in Figure 28(a). When transporter 416 is in the state shown in Figure 28(a), a judgement on the presence or absence of a steel plate is caused by transmitting a transport initiation instruction from the main computer (not illustrated) to steel plate detection circuit 504 . If, at the same time, transport detection circuit 504 is caused to output specified height h2 , for the fact that there is a steel plate, to frame height setter 528, the above-mentioned control operation will occur in angle of inclination control device 454 . Thus, frame 438 will arrive at set height h2 , as shown in Figure 28(b), by the expansion of actuators 478 . Then, in magnetic support control device 452 , since the output values of all the gap sensors 444 will become smaller than the specified position, steel plate detection circuit 504 will detect that there is a steel plate. Then, the fact that the height of frame 438 has reached the levitation possible region for steel plate 442 due to magnet units 440 is transmitted to control voltage coordinates inversion circuit 520 by detection signal TF . After time t1 from this time, in other words after height control of frame 438 is completed, the following levitation control is commenced. That is to say, output values za-1, za-2, ..., zf-1, zf-2 of gap sensors 444a-1, 444a-2, ..., 444f-1, 444f-2 are outputted as mean values za ~ zf for the sensors positioned on both sides of magnet units 440 by mean value operation circuit 498. za ~ zf are subtracted from the output of levitation gap width setter 494 by subtractors 500a ~ 500f. The subtraction results are introduced to levitation gap width deviation coordinates conversion circuit 506. Here, deviation Δz from the specified position of the centre of gravity coordinates, pitch angle deviation Δξ and roll angle deviation Δ of frame 438, together with the three twist mode deviations relating to the twisting of steel plate 442 beneath the four corner positions of frame 438 ; the twisting of steel plate 442 below the front and rear ends of frame 438 and the position in the centre of frame 438 and the bending of steel plate 442 below the front and rear ends of frame 438 and the position in the centre of frame 438 are calculated. At the same time, the excitation current measured values ia ~ if of electromagnets 462 detected by current detectors 484a ~ 484f are subtracted from the zero output of current setter 496 by subtractors 502a ~ 502f and the subtraction results are introduced to excitation current deviation coordinates conversion circuit 508. Here, coil excitation current Δiz which contributes to the vertical motion of the centre of gravity, coil excitation current Δiξ which contributes to the pitching and coil excitation current Δi which contributes to the rolling of steel plate 442 , together with the three twist mode excitation currents relating to the twisting of steel plate 442 beneath the four corner positions of frame 438 ; the twisting of steel plate 442 below the front and rear ends of frame 438 and the position in the centre of frame 438 and the bending of steel plate 442 below the front and rear ends of frame 438 and the position in the centre of frame 438 are calculated. Out of the outputs of levitation gap width deviation coordinates conversion circuit 506 and excitation current deviation coordinates conversion circuit 508, Δz, Δiz, Δξ, Δiξ and Δ, Δi are respectively introduced to vertical motion mode control voltage operation circuit 510 , pitching mode control voltage operation circuit 512 and rolling mode control voltage operation circuit 514 , and coil excitation voltage e z which contributes to the vertical motion of the centre of gravity of steel plate 442 , coil excitation voltage eξ which contributes to the pitching of steel plate 442 and coil excitation voltage e which contributes to the rolling of steel plate 442 are calculated. During the calculation of ez, eξ and e , zero power control is performed in which Δiz, Δiξ and Δi converge to zero in the stationary levitation state of steel plate 442 . At this time, respective pairs corresponding to the three twist mode deviations and the three twist mode excitation currents are introduced to the three twist mode control voltage operation circuits 516 . Here, the three twist mode excitation voltages which contribute to the twisting of steel plate 442 beneath the four corner positions of frame 438 ; the twisting of steel plate 442 below the front and rear ends of frame 438 and the position in the centre of frame 438 and the bending of steel plate 442 below the front and rear ends of frame 438 and the position in the centre of frame 438 are calculated. During these calculations, zero power control is performed in which the three twist mode excitation currents converge to zero in the stationary levitation state of steel plate 442 . By this levitation control, so-called 'zero power control' in which ia ~ if converge to zero in the stationary levitation state of steel plate 442 is achieved as a whole, and steel plate 442 is stably levitated. At this time, levitation gap width deviation Δz converges to a value which corresponds to the weight of steel plate 442 . At the same time, the fact that the height of frame 438 has reached the levitation possible region for steel plate 442 due to magnet units 440 is also transmitted to angle of inclination control device 454 by detection signal TF . In angle of inclination control device 454 , detection signal TF is introduced to frame height setter 528 , guidance control circuit 546 and changeover switch 548 . In frame height setter 528 , specified set value h3 is selected when steel plate 442 is levitated, that is to say when steel plate 442 is supported without contact at time t2 after detection signal TF has changed from 'NO' to 'YES', and frame 438 rises. When the rising of frame 438 is completed, that is to say at time t3 after detection signal TF has changed from 'NO' to 'YES', Δ z is selected in changeover switch 548, and the levitation gap width deviation for when steel plate 442 is in the stationary levitation state is introduced to adder 550 . For this reason, in angle of inclination control device 454, the height of frame 438 is controlled so that this stationary deviation Δ z is cancelled, and steel plate 442 always levitates at the specified height, as shown in Figure 28(c), despite its weight. Also, guidance control is commenced at time t2 after detection signal TF has changed from 'NO' to 'YES'. That is to say, when frame 438 begins to descend from the state shown in Figure 28(a), since the distance to steel plate 442 becomes within the specified range, front and rear and transverse travel amounts xbsa, xbsb and ybsa, ybsb are outputted in feed monitors 446a and 446b and feed monitors 448a and 448b . At the same time, at time t2 after detection signal TF has changed from 'NO' to 'YES', the output of guidance control circuit 546 switches from 0 and 0 to Δξbc and - Δbc . At this time, xbsa, xbsb, and ybsa, ybsb are compared with the zero outputs of front and rear position setter 530 and left and right position setter 532 in subtractor 536 and subtractor 538. The respective outputs Δxbsa, Δxbsb and Δybsa, Δybsb of subtractor 536 and subtractor 538 are introduced to front and rear angle of inclination operation circuit 542 and left and right angle of inclination operation circuit 544 . In front and rear angle of inclination operation circuit 542, pitching angle Δξbc for cancelling ( Δxbsa + Δxbsb)/2 is calculated. At the same time, in left and right angle of inclination operation circuit 544, rolling angle -Δbc for cancelling ( Δybsa + Δybsb)/2 is calculated. Pitch angle Δξbc is subtracted from output Δξbs of frame height coordinates operation circuit 540 in subtractor 552, and the subtraction result is introduced to front and rear inclination mode excitation current operation circuit 558. Also, roll angle -Δbc is subtracted from output Δbs of frame height coordinates operation circuit 540 in subtractor 554 , and the subtraction result is introduced to left and right inclination mode excitation current operation circuit 560 . In front and rear inclination mode excitation current operation circuit 558, excitation current iξbs is calculated for making ( Δξbs - Δξbc ) zero. Therefore, frame 438 is inclined by controlling the expansion and contraction of actuators 478 so that the slippage of steel plate 442 in the front and rear directions is cancelled. In left and right inclination mode excitation current operation circuit 560, excitation current ibs is calculated for making (Δbs + Δbc ) zero. Therefore, frame 438 is inclined by controlling the expansion and contraction of actuators 478 so that the slippage of steel plate 442 in the left and right directions is cancelled. By this guidance control, steel plate 442 is always maintained in a state facing frame 438 . When transporter 416 is in the state in Figure 28(c), if the instructed running speed is gradually increased by the main computer, transporter 416 will accelerate. When accelerating, steel plate 442 will shift toward the rear of frame 438 . However, by the above guidance control system, frame 438 will be inclined as shown in Figure 28(d) and steel plate 442 will follow frame 438. When transporter 416 is running at constant speed by a constant instructed speed, frame 438 will be level, as shown in Figure 28(e). In due course, transporter 416 approaches its destination, and when the instructed running speed begins gradually to decrease, transporter 416 will decelerate. When decelerating, steel plate 442 will shift toward the front of frame 438 . However, by the above guidance control system, frame 438 will be inclined as shown in Figure 28(f) and steel plate 442 will follow frame 438 . In this way, when it arrives at its destination and the instructed speed becomes zero, transporter 416 will stop, as shown in Figure 28(g). During this time, if external forces are applied in the transverse direction to steel plate 442 under levitation, guidance control is performed which returns steel plate 442 to its original position by inclining frame 438 as shown in Figure 29(a) for the case of steel plate 442 offset to the left as in Figure 29(b), and as shown in Figure 29(d) for the case of offset to the right as in Figure 29(c). Thus, a state in which steel plate 442 and frame 438 face each other is maintained. When transporter 416 stops and specified height h4 is outputted to frame height setter 528 by the main computer at the moment steel plate 442 is stopped by guidance control, steel plate 442 is landed on pedestal 566 by the descent of frame 438 . At this time, when a 'transport completed' signal is transmitted from the main computer, steel plate detection circuit 504 outputs a TF signal which indicates that steel plate 442 is not present. Then, levitation control and guidance control are stopped by outputting zero in control voltage coordinates conversion circuit 520 and guidance control circuit 546. At the same time, specified frame height h1 is outputted in frame height setter 528, and frame 438 rises, leaving steel plate 442 on pedestal 566, as shown in Figure 28(h). The frame height becomes h1 , and transport is completed in the state shown in Figure 28(i). In this embodiment, gap sensors 444 are arranged on both sides of magnet units 440 . By this means, even if there is bending in the steel plate to be transported, it is possible to detect the levitation gap width between magnet units 440 and steel plate 442 more accurately. Also, in levitation control, the movement of steel plate 442 is divided into modes by movement coordinate systems, and levitation control is performed mode by mode. For that reason, it is possible to design respective levitation control systems for every mode. Therefore, robust levitation control can be performed for variations in the weight, material and thickness of the steel plate. Moreover, zero power control is used in levitation control. However, when supporting steel plate 442 without contact by this type of zero power control, the levitation gap widths of magnet units 440 on which the load is increased by the inclination of steel plate 442 decrease. Therefore, the effect of guidance control for the front and rear left and right positional slippage of steel plate 442 is further contributed to by inclining the steel plate in a direction which will return it to its original position. In other words, the magnetic support control device has the dual purpose an angle of inclination control device. In the above embodiment, magnetic levitation system 410 is assembled in transporter 416 . However, this does not place any limits on whether or not there is a steel plate transport device, nor on the inclination device. For example, as shown in Figure 30, there is no objection of any kind to mounting joint mechanism 572 , which is capable flexion with two degrees of freedom, on the lower end of tip 570 of scalar type robot 568 and using this as the inclination device for magnetic levitation system 410 . Scalar type robot 568 has the degree of freedom of rotation about its axis shown in Figure 30, while tip 570 is constructed so that it moves vertically through actuator 574 . Using this type of composition, the inclination of frame 438 is controlled via the two degrees of freedom of the lower end of joint mechanism 572 of the flexion action and the vertical motion of actuator 574 in response to the travel of tip 570 . Thus, steel plate 442 is always supported without contact in a state facing frame 438 . Needless to say, this invention can be widely used for transport and delivery purposes other than the above scalar type robot. Also, in the above embodiment, the magnetic units are mounted on flat plate-shaped frame 438 , and guidance control is achieved by inclining the steel plate by causing the inclination of frame 438 . However, this in no way limits the methods of mounting the magnetic units. For example, as shown in Figure 31, instead of frame 438 in magnetic levitation system 410 of Figure 24, magnetic levitation system 578 may be composed by securing narrow strip-shaped members 576 to the lower ends of actuators 478 and rods 482 which are thrust through linear guides 480 on their left and right sides, and arranging magnet units 440 and gap sensors 444 on the underside of narrow strip-shaped members 576 . In this case, substrate 434 may be regarded as a frame for mounting magnet units 440 . Also, feed monitors 446 and 448 mounted on the underside of narrow strip-shaped members 580 are secured to substrate 434 via pedestals 582 . In this type of composition, guidance control is performed by inclining the steel plate by changing the heights of respective magnet units. At the same time, magnetic levitation of objects to be transported with large bends, such as steel plate 442' , is possible. Moreover, in the above embodiment, a steel plate is supported without contact by six magnet units. However, this does not limit the number of magnet units in any way. For example, as shown in Figure 32, there is no objection to using twelve magnet units. When a large number of magnet units are used in this way, weight increases of the objects to be transported can be coped with, while the supported weight and magnetic flux per magnet unit can be reduced. Thus, even if the object to be transported is thin steel plate, saturation of magnetic flux can be avoided, and stable non-contact support becomes possible. In addition, in this embodiment, U-shaped magnet units are provided with permanent magnets. However, this does not limit the configurations and compositions of the magnet units in any way. For example, there is no objection of any kind even if the magnet units are composed of various configurations of electromagnets, such as E-shaped or tubular. Also, in this embodiment, the object to be transported is a flat plate-shaped steel plate. However, this does not limit the material or configuration of the object to be transported in any way. provided the object to be transported is composed of a magnetic substance or a ferromagnetic substance, there is no objection to its being of any configuration. Moreover, in the embodiment described above, the control system and its operation are expressed analogically. However, it is not limited to this type of control method, and a digital method may be used. Needless to say, in this way, this invention can be implemented by various modifications within limits which do not deviate from its purport. When the magnetic levitation system of this invention is used as described above, guiding forces act on the object to be transported through the resultants of the gravitational forces due to the tilting of the levitated object to be transported and the attractions of the magnet units. The guiding forces can be adjusted by detecting the amount of travel or the speed of travel of the object to be transported in the guidance direction and controlling the angle of inclination of the object to be transported. Therefore, there is no requirement to provide fresh electromagnets for guidance and thus the support mechanism is simplified. Also, the guiding force is obtained by inclining the object to be transported. Therefore, a size of guiding force which corresponds to the mass of the object to be transported can be obtained. Moreover, guidance of the object to be transported is possible, even if the width of the object to be transported is broader than the gap between magnetic units in the guidance direction. For this reason, it is possible to support without contact a large variety of magnetic bodies over long distances. Also transport lines can be of simple construction.

Claims: A magnetic levitation transport system including a track with a magnetic force support system which is arranged to support the object to be transported without contact, the object having a flat, possibly slightly curved upper surface and at least partly comprising a ferromagnetic substance, the system comprising: multiple fixed support units (3) arranged along the direction of transport, each support unit including a track frame (13); and magnetic assemblies (15a; 15b) including electro-magnets (27a, 27b; 27c, 27d) which are positioned in each track frame and extend in a direction orthogonal to the direction of transport and constitute means for supporting, transporting, and guiding the object; characterised by : mounting devices (17) for the magnetic assemblies which permit movement in the vertical direction, and an attraction control device (19) which is arranged to perform levitation control for both pitching and rolling motion of the object to be transported by moving each of the magnetic assemblies (15a, 15b) on its mounting device only when the object to be transported is below that assembly. A track magnetic levitation transport system according to claim 1, in which each of the magnetic assemblies also includes a permanent magnet (21a; 21b); the magnetic circuit produced by the electromagnet (27a, 27b; 27c, 27d) and the permanent magnet (21a; 21b) both pass through the air gap between the electromagnets and the object (X) to be transported; and the attraction control device has a zero power control capability which causes the excitation current of the electromagnets to converge to zero when the object to be transported is stably levitated regardless of its weight. A magnet levitation transport system according to claim 1 or claim 2 in which the mounting device includes elastic components (47a, 47b; 47c, 47d) and inelastic components (49a; 49b) provided between the track frame and the magnetic support units. A magnetic levitation transport system according to any preceding claim in which each mounting device includes a height adjustment device (41) which varies the mounting heights of the magnetic assemblies. A magnetic levitation transport system according to claim 4, in which the height adjustment device includes a height control device (53) which is arranged to levitate the object to be transported at a constant height. A magnetic levitation transport system according to any preceding claim and comprising a propulsion device (5) in the track frame which applies thrust in the direction of transport to the object to be transported. A magnetic levitation transport system according to claim 6, wherein the propulsion device comprises: multiple linear induction motor stators (100a, 100b, 114a, 114b) arranged so that the object to be transported acts as a secondary conductor; a yaw detection device (118a, 118b) which detects yawing of the transported object; a propulsion operating device (120) which separately calculates thrust applied to each side of the object based on an output of the yaw detection device; and an excitation device (156) for generating travelling magnetic fields in individual ones of the linear induction motor stators based on calculation results of the propulsion operation device. A magnetic levitation transport system according to any preceding claim further comprising: a guidance device in the track frame which guides the object to be transported along the track without contact. A magnetic levitation transport system according to claim 8, wherein the guidance device comprises: a plurality of linear induction motor stators (172a, 172b, 178a, 178b) which apply thrust in a guidance direction to the transported object as a secondary conductor; a guidance detection device (118) which detects drift of the object from the direction of the track; a guiding force operation device (180) which calculates the thrust applied to the object based on an output of the guidance detection device (118); and an excitation device (188a, 188b) for generating moving magnetic fields in the linear induction motor stators based on the calculation results of the guiding force operation device. A magnetic levitation transport system according to claim 9, wherein the guidance device comprises: at least one pair of linear induction motors (172a, 172b; 178a, 178b) which generate mutually opposite thrusts in a direction orthogonal to the direction of transport. A magnetic levitation transport system according to claim 8, wherein the guidance device comprises: electromagnets arranged so that rolling occurs in the object to be transported due to fluctuation in attraction when the centre of gravity of the object leaves a centre line of the track; and a control device (19b) which controls guidance by controlling levitation of rolling of the object to be transported. A magnetic levitation system according to any preceding claim further comprising: an inclination device (436) which causes a variation of an angle of inclination of the object to be transported in a direction orthogonal to the direction of transport; and control means for the inclination device. A magnetic levitation transport system according to claim 6 wherein the propulsion device comprises: thrust application devices (11a, 100b, 114a, 114b) on each side of the track which apply thrust in a direction along the track to the object to be transported; a yaw detection device (118a, 118b) which detects yawing of the object to be transported; a thrust operation device (120) which separately calculates the thrusts applied to each side of the object based on an output of the yaw detection device; and a thrust generation device (156) for causing generation of thrust in the thrust application devices based on a calculation result of the thrust operation device. A magnetic levitation transport system according to claim 13, wherein the thrust application devices comprise; linear induction motor stators (100a, 100b, 114a, 114b) which cause the object to be transported to act as a secondary conductor; and an excitation device which generates travelling magnetic fields in the linear induction motor stators. A magnetic levitation transport system according to claim 12 in which the inclination device (436) is included in the mounting device. A magnetic levitation transport system according to claim 13 wherein each mounting device comprises; an angle of inclination control device (454) which is provided in the attraction control device (452); and the magnetic assembly (440). A magnetic levitation system for an object at least part of which comprises a ferromagnetic substance and having a flat, possibly slightly curved upper surface, the system comprising: a transporter (416) which is movable along a track; magnet assemblies (440) including electromagnets mounted on the transporter by support means (438); a magnetic support control device (452) which controls the attraction of the electromagnets of the magnet assemblies for non-contact support of the object; characterised by : an inclination device (436) which controls pitching and rolling of the object to be transported by changing the angular position of the support means (438); and a control device (454) including sensors (446,448) for the inclination device. A magnetic levitation system according to claim 17, wherein: the inclination device (436) is arranged to cause inclination of the frame (438). A magnetic levitation system according to claim 17, wherein: the magnet units are mounted on the frame via the inclination device. A magnetic levitation system according to claim 19, wherein: the inclination device moves the magnet units (440) in a vertical direction. A magnetic levitation system according to claim 17, wherein the inclination device comprises: an angle of inclination control device (542, 544) in the magnetic support control device; and the magnet units (440). A magnetic levitation system according to claim 17, wherein: the magnet assemblies include permanent magnets (21a; 21b); and the magnetic circuits of the electromagnets (27a, 27b; 27c, 27d) and the permanent magnets both pass through the gap between the electromagnets and the object to be transported. A magnetic levitation system as stated in claim 22, wherein: the magnetic support control device has a zero power control capability which causes an excitation current of the electromagnets to converge to zero when the object to be transported is stably levitated regardless of its weight.

Inventors: MORISHITA MIMPEI, MORISHITA, MIMPEI, Morishita, Mimpei, c/o Intell.Prop.Div.Tosh.Corp.
Applicants: TOSHIBA KK, KABUSHIKI KAISHA TOSHIBA
Application year: 1995
Main classification: B65G54
IPC codes: B65G54