IMPROVED METHOD AND APPARATUS FOR REAL-TIME STRUCTURE PARAMETER MODIFICATION

Abstract: A method and apparatus for structural deflection control, as well as associated sequential controls that are based on new control laws. The apparatus of this invention is of relatively low cost and performs better than prior art devices. The essence of the invention is to adjust the dynamic parameters (mass, damping, stiffness coefficients of the structure and/or input forcing coefficients) adaptive to input dynamic loads, by using the new devices and the suggested control laws. In so doing, the structure performs an adaptive function to effectively counter the effects induced by multi-directional external excitations. The required control power can be nil, or many times lower than prior art active control devices, and the effectiveness can be equivalent or even better than the current state-of-the-art active controls. The devices used by the apparatus of this invention can readily be manufactured for immediate application in structures, buildings and contents, and other constructed facilities.

Description: IMPROVED METHOD AND APPARATUS FOR REAL-TIME STRUCTURE PARAMETER MODIFICATION TECHNICAL FIELD The present invention relates generally to a method and apparatus for controlling the displacement (or vibration) of a structure when subjected to external forces such as an earthquake or wind, the apparatus employing novel damping/coupling devices and mounts therefor; and more particularly to a method and apparatus to adjust the dynamic parameters (mass, damping, stiffness coefficients) of a structure by using new devices mounted in novel manners in accordance with novel processes developed from newly proposed control laws. BACKGROUND OF THE INVENTION It is well known that structures can fail when subjected to external forces of sufficient magnitude, as for example high winds or a moderate to strong earthquake. Many proposals have been made for improving the ability of a structure to withstand such forces without damage or failure of the structure. The approaches range from making the structure rigid, making it flexible, to mounting the structure upon the surface of the ground so that it can move relative to the ground, by coupling or uncoupling the structure to a mass to change its resonant frequencies, etc. One such example is shown in U.S. 5,036,633 invented by Kobori wherein an apparatus is disclosed for controlling the response of a structure to external forces such as seismic vibration and/or wind impacting against the structure, the control apparatus including variable stiffness means secured to and bracing the structure, variable damping means interposed between the structure and the variable stiffness means, and a computer which is programmed to monitor external forces impacting against the structure and to control the variable damping means by selecting a coefficient of damping suitable to render the structure non-resonant relative to the monitored external forces. The foregoing patent of Kobori, as well as other patents of Kobori, and patents of others, are based on feedback control principles which include changing stiffness to avoid resonance according to ground motion forecasting, changing damping coefficient according to preset damping standards, and varying the stiffness of a local member by locking or unlocking a device disposed between the ends of a member. The approach of the prior art emphasizes identifying individual structural vibration- reduction-devices, but does not perform an analysis of the whole structural system's behavior. Furthermore, the prior art analysis tends to focus on a single plane of the structure and the analysis is not three dimensional. SUMMARY AND OBJECTS OF THE INVENTION The major concept of the present invention is to provide a method and apparatus for controlling a structure to minimize time-varying motion of the structure by a real¬ time modification of structure parameters to achieve a cost-effective control of structural deformation, internal force, buckling, destructive energy and related damages caused by multi-directional loading such as earthquake, winds, traffic, and/or other type of ambient loading. The control is based upon the use of control devices in accordance with control principles which are non-linear, time dependent, and adaptive; the control devices making the system more robust, and hence more stable. Since this approach actually controls the physical parameters of the structure through adaptive control devices, it is called functional adaptive control, and a structure which is capable of modifying its dynamic performance is called an adaptive structure. The present invention contemplates changing within an adaptive structure the coefficients of the displacement, velocity and acceleration, namely the stiffness, damping, and mass. In addition, the present invention may also change certain coefficients of the input driving forces. For example, it may change the friction coefficients of base-isolation devices for structures to minimize the input force/energy for ground motion. Since the new approach actually controls the physical parameters of the structures, it therefore controls the characteristics or the functional behavior of the structure through the adaptive devices. The underlying theory of the present invention is based upon analysis of the whole structural system's behavior, and therefore is innervative (adaptive) , and is characterized by the following: 1) Control procedure - System's optimal approach by changing the physical parameters of the structure such as damping, and either mass or stiffness, or both. 2) Control mechanism - Through coupling/uncoupling of certain substructures and/or sub-members by means of functional switches. 3) Control Principle - Minimization of conservative energy through the use of a computer program which will perform a sequence of steps arranged in a hierarchical fashion. In addition, in the preferred embodiment no actuators apply force to the structure. Therefore, the control is not active. Each of the functional switches of the control mechanism can be in one of the following states: "on", "off", or "damp". By varying the state of each functional switch, the switches may control the physical parameters of an associated structure such as mass, damping, and stiffness, and the functional switches may also control the input-driving forces. When a functional switch is "on" portions of the switch are rigidly connected to each other and the switch can connect a heavy mass to add significant mass to the structure. Also, when a functional switch is "on" it can connect members of the structure to increase the stiffness of the structure to reduce the corresponding displacement and thereby increase the natural frequency of the structure. When a switch is "off", the connections are eliminated, thus the opposed portions of the switch are freely movable with respect to each other. When a switch is set at "damp", there is a viscous movement of the opposed portions and the switch can also increase the energy dissipation capacity of the structure. When this state is eliminated, the damping force can be significantly reduced, which may therefore reduce the input driving forces. Since there are only three output states of a functional switch, the control processes for the operation of the switches can be relatively simple. Thus the calculating speed will be increased significantly, which is a key issue in active or adaptive control. To better understand the control theory of this invention, a prior art active control system will be considered first. For a linear mechanical vibration system, the following equation may be used to describe its motion: f(t) = MX"(t) + CX'(t) + KX(t) (1) where f is the external force, M, C, and K are the mass, damping and stiffness coefficient matrices, X(t) , X' (t) , and X" (t) are the displacement, velocity and acceleration vectors, and the superscripts ' and " stand for the first and second derivatives with respect to time. In a single degree of freedom (hereinafter SDOF) system, in equation (1) , the work done by the internal force MX" can be described as the kinetic energy. The work done by the damping force CX' can be described as dissipated energy. The work done by the spring force KX can be described as the potential energy. The sum of these three energy terms equals the work done by the external force f. This can be stated as: E c = E ± - E d ± E^ (2) where E stands for energy, and the subscripts c, i, d, and t stand for conservative, input, damping, and transfer energy, respectively. (For a pure SDOF system, E t = 0. However, if equation (1) is used to describe a vibrational mode of a multi-degree-of-freedom (hereinafter MDOF) structure, E t exists either positively or negatively.) When the mass, damping and stiffness coefficients are fixed, both the kinetic and the potential energy are conservative. Only the damping force dissipates energy. If the coefficients M, C, K can be changed as they are in real-time structural parameter modification (hereinafter RSM) devices of this invention, neither the kinetic nor the potential energy are completely conservative. Thus equation (1) can be rewritten as follows: M(t)X"(t) + C(t)X'(t) + K(t)X(t) = F(t) (3) Comparing equation (3) with equation (1) it is apparent that all parameters have become functions of time. A certain amount of energy may be transferred outside the structure by functional switches. The remaining energy is still conservative. It is intuitive that, to minimize the displacement of the structure, the conservative part of the kinetic and potential energy should be minimized. If the conservative energy is minimized, the displacement keeps the smallest value. This is the essence of the principle of minim-1 conservative energy. Thus: E kc + E pc = minimized (4) The energy equation of the entire system can be written as: W = E ko + E kf + E d + E df + E p . + E pf (5) Here, the letter W is the work done by the external forces, and the letter E stands for energy terms. The subscript k stand for kinetic, d for energy to be dissipated by damping force, p means potential, and c means conservative energy. The second subscript f stands for the energy transferred and is dropped later by the functional switches. To minimize the E^, + E kc from the above equation, it can be seen that an optimal result can be achieved by maximizing E kf , E df E df , and E pf and by minimizing W. Thus minimal E p< , is achieved by increasing the energy transfer E kf and E pf , increasing the energy dissipation E d and E df , and also by decreasing the work done by the external force W, which is equally important and is achieved by increasing the instantaneous impedance or the entire structure. While several SDOF systems may be used to approximate a MDOF structure, in a multiple degree of freedom system (MDOF) , minimization of Conservative energy becomes a somewhat more complex task. The complexity arises because the energy transfer between the various modes of vibration of a structure must be considered. The energy transfer among modes of a MDOF structure may be determined through the Complex Energy Theory as proposed by Liang and Lee ("Damping of Structures: Part I: Theory of Complex Damping", NCEER Report 91-0004, 1991). Under the Complex Energy Theory, systems may be classified as proportionally damped or nonproportionally damped. A proportionally damped system is one in which the damping coefficient may be represented as a proportion of mass and stiffness, that is, C = (A)M + (B)K (6) where A and B are constant coefficients, and M and K represent the mass and stiffness matrices of a system respectively. A fundamental characteristic of such a system is that there is no energy transfer between modes during vibration. However, for a nonproportionally damped system, Equation (6) will not hold. This is of particular relevance to the instant invention because as the stiffness, mass and damping matrices of the structure are modified with time, Equation (6) will not be satisfied, and the system will be classified as nonproportionally damped. Accordingly, energy transfer will occur between modes. The measure of energy transfer between modes may be expressed by a Modal Energy Transfer Ratio S ± , where Si « W τi /4rW i (7) and W τi = Energy transferred to the i th mode during one cycle of vibration and W ± = Energy stored in the i th mode before the cycle of vibration. The natural frequency for any given mode in a nonproportionally damped system is also dependent on the transfer of modal energy. The natural frequency, w if of the i th mode in a nonproportionally damped system accordingly becomes fi = ni exp(S ± ) (8) where Si is defined by Equation (7) and w ni = the natural frequency of the i th mode if the system was proportionally damped. In order to minimize conservative energy, it is necessary to minimize the modal energy transfer ratio of Equation (7) for each mode of the structure. This concept will be incorporated into Equation (5) in the Detailed Description section of this application. From the above it can be seen that it is a primary object of the present invention to provide a method and apparatus for controlling the displacement (or vibration) of a structure when subjected to the application of external energy due to external forces such as an earthquake or wind, the apparatus employing novel damping/coupling devices and control systems therefore. It is another object of the present invention to provide a control system capable of adjusting the dynamic parameters (mass, damping, and stiffness coefficients) of a structure by using new devices mounted in novel manners in accordance with novel processes developed from newly proposed laws. It is a further object of the present invention to provide a control system for modifying a structure to control its displacement when subjected to external forces, such as an earthquake or wind, the control system including functional switch devices which are coupled to the frame of a structure, and control means for operating the functional switch devices for minimizing the energy of a structure and/or preventing transfer of energy to the structure to thereby minimize the conservative energy of the structure when a sensor connected to the frame senses a change in a parameter, such as velocity, acceleration, or displacement of the frame. It is a further object of the present invention to provide a control system for varying structure parameters in real-time when a structure is being displaced by external forces, wherein the physical parameters of the structure are initially determined, wherein functional switches are mounted in the structure to minimize the conservative energy of the structure when external forces are applied to the structure, and which control system will control the functional switches in real-time in response to measured values of velocity, acceleration or displacement caused by the application of external forces to thereby minimize the conservative energy of the structure and control its displacement. It is a further object of the present invention to provide a control system for controlling the displacement of a structure due to the application of external energy, the structure being modified to include functional switches, and the control system including sequential or hierarchical controls which include a first loop for local control of each functional switch. It is a further object of the present invention to provide a control system of the type set forth above wherein a second loop for local control of each functional switch is provided, the second loop including an override function. It is a further object of the present invention to provide a control system of the type set forth above wherein a third loop for global control of each functional switch is provided. It is a further object of the present invention to provide a control system of the type set forth above wherein a fourth loop is provide which can be considered a fail-safe control loop. It is a further object of the present invention to provide a control system for controlling the displacement of a structure due to the application of external energy or forces, the structure being modified to include at least one pair of functional switches mounted in a structure in a push-pull (compression/tension) wherein the first and second switches of each pair of functional switches are switched between "on" and "off" states, respectively, and "off" and "on" states, respectively, as the structure moves in differing directions. It is a further object of the present invention to provide a control system for modifying the structural parameters of a structure in real-time, which control system involves providing functional switches having "on", "off", and "damp" states, mounting the functional switches in a structure in such a manner that when the functional switches are controlled that the structural parameters of the structure can be modified, and changing the states of the functional switches in response to one or more of the measured values of velocity, acceleration or displacement, which are caused by the application of external energy, in such a manner that energy applied to the structure is dissipated, and displacement of the structure is controlled, at least one functional switch being mounted in a plane which intersects the plane in which another functional switch is mounted to provide control in more than one plane simultaneously. It is yet a further object of the present invention to provide a novel functional switch having a cylinder provided with axially aligned first and second bores, first and second rods slidably mounted within the first and second bores, means coupling the first and second rods together for simultaneous movement, and a fluid passageway within the cylinder extending between adjacent ends of the first and second bores, the fluid passageway being provided with a valve, which valve may be controlled for varying the state of the functional switch between "off", "on", and/or "damp" states. The foregoing objects and other objects and advantages of the present invention, as well as the application of the control theory briefly outlined above, will become more apparent to those skilled in the art after a consideration of the following detailed description taken in conjunction with the accompanying drawings. BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 illustrates a building structure which may be deflected by an earthquake, strong winds, etc. FIG. 2 illustrates the X-Y movement of an earthquake over a period of time. FIG. 3 illustrates a portion of a building structure to which functional switches have been applied in accordance with the principles of this invention. FIG. 4A is a schematic diagram of a unidirectional functional switch. FIG. 4B illustrates the dynamic model of the functional switch shown in FIG. 4A. FIG. 5 is a graphical flow chart for the control program developed in accordance with this invention. FIG. 6 is a decision making flowchart of the RSM control process showing the hierarchical control loops. FIGS. 7A and 7B illustrate a typical arrangement of the control hardware at the initial local structural control level in this invention, FIG. 7A being a front view and FIG. 7B being a side view. FIG. 8 illustrates the switching of a functional switch while undergoing initial local structural control. FIG. 9A illustrates the Force vs Displacement plot for a functional switch operating under initial local structural control. FIG. 9B illustrates the structural overdraft deflection which may occur if initial local structural control is used in the absence of any higher level controls. FIG. 10 illustrates a structure provided with global loop control which simultaneously checks the status of all functional switches in real-time and issues .optimal commands according to a selected principle. FIG. 11 illustrates a simplified building structure which may be modified in accordance with the principles of this invention. FIG. 12 illustrates calculations on how the building shown in FIG. 11 would resonate when subjected to the earthquake of FIG. 2. FIG. 13A and 13B illustrate how the building of FIG. 11 may be modified in accordance with the principles of this invention to reduce its structural deflection during the earthquake of FIG. 2. FIG. 14A illustrates how the functional switches shown in FIGS. 13A and 13B will be turned "off" and "on." FIG. 14B shows the theoretical dynamic responses of a pair of prototype switches when used in a push-pull arrangement under certain excitations. FIGS. 15A and 15B show the calculated response of the structure of FIG. 6, FIG. 15A showing the response when modified in accordance with the RSM system of this invention, and FIG. 15B showing the response when modified by using stiff bracing. FIG. 16 shows actual test results of a test stand structure when either controlled or not controlled by the subject matter of this invention. FIG. 17 shows how this invention may be applied to a bridge. FIG. 18 illustrates a bidirectional functional switch which may be employed in the design shown in FIG. 17. FIGS. 19 - 21 show how this invention may be applied to other building structures. FIG. 22 shows yet another application of this invention to a building structure. FIG. 23 is a diagram showing the results of applying the RSM system to the building shown in FIG. 22. FIGS. 24 and 25 show the theoretical and experimental dynamic responses of a prototype switch under certain excitations. FIG. 26 is a side view of a four-way functional switch. FIG. 27 is a view taken generally along the line 27 - 27 in FIG. 26. FIG. 28 is a sectional view taken generally along the line 28 - 28 in FIG. 27. DETAILED DESCRIPTION First, with reference to FIG. 1, a building structure is indicated generally at 10. The structure illustrated has four generally vertically extending columns 12, 14, 16, and 18. In addition, there are a number of floors formed by horizontal beams 20, 22, 24, and 26. As indicated in this figure, the horizontal beams 22.1, 22.3, 24.1, 24.3, etc., extend in an east-west direction in an X-Z plane; and the beams 22.2, 22.4, 24.2, 24.4, etc., extend in a north- south direction in a Y-Z plane. The structure as shown is provided with a passive control such as the chevron bracing beams 30, 32. When the building 10 is subjected to a wind such as a westerly wind indicated by the arrow 34, the building will deflect towards the east. The wind will input energy into the building, the additional energy being stored within the bending columns, etc. When the velocity of the wind 34 decreases, this energy will be released to restore the building to its normal shape. As can be seen from the structure sketched in FIG. 1, all of the deformation to the building occurs in the X-Z plane, which deformation can be resisted by the chevron bracing beams 30, 32. When the building 10 is subjected to an earthquake, there will be horizontal movement of the ground in X and Y directions (which may be east-west, and north-south, respectively) . In addition, there will be ground waves which are indicated by the sinusoidal waves X and Z in FIG. 1. Because of these motions, during an earthquake the building will be subjected to at least five degrees of movement; namely, movement in the X-Y-Z directions, and rotational movement about the X and Y axes, and perhaps rotational movement about the Z axis. In most earthquakes, the excitation and most other dynamic loadings are typically random. This can best be seen from FIG. 2 which is the El Centro Earthquake Response Time History. The building 10, when subjected to such an earthquake, will be deflected and tends to vibrate. The vibration of such a building tends to be destructive. It has been determined by computer analysis and experimental tests that if the structural physical parameters are modified in real-time that the adaptive structure can withstand a large range vibration magnitudes. Such structural parameter modification may be achieved through the use of functional switches. While many forms of functional switches may be employed, the preferred form is a type which is both bidirectional and which may be used again and again. The functional switch may be set to "off", "on", or "damp" states. Depending upon the application, either a bidirectional or a unidirectional switch may be preferred. FIG. 3 is a view similar to FIG. 1 showing a portion of the structure shown in FIG. 1 but with an additional vertical column 15 in the Y-Z plane. This figure additionally shows paired unidirectional functional switches indicated generally at 36. (While unidirectional switches are illustrated in FIG. 3, it should be obvious that the preferred bidirectional switches could be employed, the directional switches being discussed below in connection with FIGS. 17, 18, and 26 - 28.) Thus, as illustrated, there are a pair of unidirectional functional switches 36.1 and 36.2 lying in the Y-Z plane and extending between the column 15 and the horizontal beam 24.2. At the corner of the structure are two additional functional switches 36.3 and 36.4, the functional switch 36.3 lying in the Y-Z plane and extending between the corner column 14 and the horizontal beam 24.2 and the other functional switch 36.4 lying in the X-Z plane and extending between the vertical column 14 and the horizontal beam 24. It is possible for the switches 36.3 and 36.4 to either transfer of dissipate energy from one plane to the other. A unidirectional reusable functional switch, indicated generally at 36, is illustrated in FIG. 4A, this functional switch including a cylinder 38 and a rod 40 which is received within the cylinder 38. One end of the rod 40 is provided with a suitable eye 42 or the like which can be secured to a suitable fixture (not shown) carried by the beam 24. The end of the cylinder 38 remote from the rod end 42 is provided with a bracket 44 which can be suitably secured to the column 14 or 15 by a link (not shown) . In addition to the piston and rod assembly, the unidirectional functional switch 36 may also include a reservoir 46. The reservoir is connected with the fluid chamber 48 within the cylinder 38 through a suitable port 38.1. A fluid circuit extends between port 38.1 and the reservoir 46, the circuit being provided with parallel branch lines 50, 52. A regulator in the form of a variable orifice or restrictor 54 is provided in one of the branch lines 50, and a one-way check valve 56 is provided in the other branch line 52. When the structure 10 is deflected in a manner which may cause the functional switch 36 to be compressed, the check valve 56 will prevent flow through line 52 and the variable orifice may be set to a "damp" condition so that the energy of deflection will be absorbed by the switch. However, if the functional switch were to be extended, fluid may move freely from the reservoir 46 through line 52 and check valve 56, and also through port 38.1, the switch then being in an "off" condition. The variable orifice or restrictor may employ a mechanical controller, as for example by a bell crank which senses movement between the rod 40 and cylinder 38, the bell crank in turn being coupled to a suitable valve. Alternatively, the variable orifice may be controlled by an electro-mechanical device which is coupled to a suitable electronic device. Two unidirectional functional switches may be assembled together so that in both directions one can have •■ on", "off", and damp functions. A bidirectional functional switch will be discussed later. In FIG. 4B the dynamic model of the unidirectional functional switch is illustrated. (This model is also valid for a bi-directional assembly.) The connectors and other parts of the assembly always have stiffness and masses, the modified stiffness and masses being denoted 1^ and M,„, respectively. In this figure, the function of the variable orifice 54 is achieved by a variable valve 57 which may be progressively moved from a fully closed position to a fully open position by a suitable control such as a linear electrical device 58. The damping C [equation (1) ] is provided by the variable orifice of the valve as it is moved between its extreme positions. However, if the damping must be very high, and the orifice in the variable orifice valve 57 cannot supply such a high range of damping, an additional damping mechanism 59 may be used. However, the stiffness K,,, and mass M,,, can be mainly contributed by the switch system itself. The value of C, K,,, and M n are determined in the following criteria: The damping C must be high enough to dissipate the energy stored in the switch system during the half cycle when the switch is "off". However, overvalued C will decrease the response speed of the control valve. The value K,,, is determined in a manner set forth below in connection with equation (9) . The value of M,,, is determined to achieve optimal energy dissipation including optimal work done by the mass against the external force. However it is constrained by the response speed of the switch system. Overvalued M o will also decrease the response speed as does the damping C. FIG. 5 illustrates a graphical flow chart for a multi- degree of freedom seismic vibration control. According to this scheme, initially all of the switches are set to be "on". The dynamic responses, the internal and external forces, the modal energy status and/or ground motions are measured and calculated when the structure is subjected to multi-dimensional ground motion. The measured and calculated data are stored all the time. A system identification unit may be used to obtain certain modal parameters that are also stored in the storage unit. When the response level exceeds the preset threshold values, the central decision-making unit will give orders to initiate local decision-making units. The preset threshold values are decided as follows: 1) If the RSM system is used together with conventional controls of the prior art, the preset threshold values can be higher to allow these prior art devices to perform first; 2) If the RSM system is used alone, the threshold values should be lower, even zero. In this case, the preset values are to lower the required precision of the RSM system to lower the manufacturing cost. Another important function of the central decision-making unit is to identify the optimal set of specific functional switches and their on/off status with respect to global results. Thus, a local substructure may achieve a minimal response, but this minimal response may lead to very large deformation of another substructure. On the other hand, a local point may show a large deformation and absorb significant amount of vibrational energy and reduce the global vibrational level. After the central unit initiates the orders, the local decision-making units start to calculate the optimal results and give the on/off order to each functional switch individually. According to the orders, each switch is set to be "on", "off", or "damp" to reduce the vibration level. At the next time interval, the vibratory signals are measured again and a new cycle of control is initiated. When the external excitation and the structural vibrational levels are reduced to certain values, the central unit gives orders to stop the entire control process. The control system described above is implemented by a computer program which will perform a sequence of steps arranged in a hierarchical manner. The program performs local structural controls, global structural controls and safety checks to insure structural integrity in the event of a malfunction. FIG. 6 is a flowchart representation of the sequential control program for RSM. For the purpose of the flowchart of FIG. 6, it is assumed that a multi-storied structure is equipped with a number of functional switches and that the RSM system is not used with other controls. In this flowchart these switches are deemed to have only two physical states: "on" (stiff member) or "off" (zero stiffness member) . The control scheme begins with all functional switches set initially to the "on" position. The lowest level of control provided by the sequential control program is called the initial local structural control level or H α control loop. Each functional switch in the structure is equipped with the necessary control devices to perform H x control, and accordingly, each set of H α control devices controls only the local functional switch it is associated with. The general control loop utilized in the H α control loop consists of a functional switch, a velocity transducer and control electronics. The velocity transducer may be mounted in a variety of manners with the purpose of measuring the relative velocities between two adjacent floors in a multiple story structure. The functional switch associated with this velocity transducer is mounted between the same two adjacent floors as the velocity transducer. FIGS. 7A and 7B show a basic arrangement of a single functional switch 36.5 mounted in a structure such as that set forth in FIG. 3. The switch 36.5 may be of the type shown in FIG. 4A. In this figure the switch is connected to a lower horizontal beam 22.2 via a support 60 and to an upper horizontal beam 24.2 via a brace 61 and intermediate frame 62 which supports a mass 63. A velocity transducer 64 extends between the mass 63 and the upper beam 24.2. A force transducer 65 is mounted between the brace 61 and the functional switch 36.5. Finally, an accelerometer 66 is mounted on the frame 62. The velocity transducer measures the relative velocity of the upper floor 24.2 with respect to the lower floor 22.2, and initiates a signal to the H x control means or processor 67 which in turn sends a signal to the linear electrical device 58, which in this embodiment is a two position solenoid, to either turn the switch "on" or "off" by operation of valve 57. The Hj loop operates in the following fashion. The Hj . processor first analyzes the velocity transducer output and, as the relative velocity approaches zero, the ft x processor issues a command to the control valve of the functional switch which has the effect of reversing the current status of the device 58, either turning the switch "on" or "off" as required. The performance of the H α loop action is shown in FIG. 8. The net result is that the functional switch is alternated between "on" and "off" status at the time when the local velocity of the structure approaches zero. The control electronics embodied in the H x processor which are necessary to execute H x control are located near or on the associated functional switch. The electronics consist of a power amplifier to amplify the output of the velocity transducer 64, decision making electronics, and a power amplifier to send a suitable control command to the solenoid 58 of control valve 57 of the functional switch 36.5. The E-, control method has been described above as a method for switching stiffness elements "on" and "off", but it may readily be used to switch mass or damping elements. In a very simple form of structural control, the H α loop will provide significantly improved energy dissipation characteristics over conventional methods, and it can operate as an independent control system. FIG. 9A displays the results of the ^ loop as a stand-alone control device on a simple structure. The loop of energy dissipated is ideally a parallelogram. The two sides perpendicular to the x axis stand for the force drop without change of displacement. The other two sides stand for the stiffness of the entire system. It can be proven that, given a certain amount of stiffness, the parallelogram offers the maximum energy dissipation from RSM. In a SDOF system, this energy loop satisfies the Minimum Conservative Potential Energy described in equation (5) . In FIG. 24, the theoretical response of a switch is shown. At point 1, the switch starts to be compressed, since the orifice is set to be "on", no fluid can pass the orifice. At point 2, the force reaches its maximum value without any displacement allowed. However, when the force begins to change its direction, the orifice is suddenly released, the "off" condition is achieved and the switch is allowed to move, in a very short period, the force is dropped to its minimum value at point 3 and the maximum displacement between the switch is achieved, which equals to the maximum allowed displacement of the structure at the specific points where the functional switch is mounted. Shortly after the point 3, the switch is still in free movement of "off" condition but the displacement begins to decrease until the next compression begins at point 1. Note that, if the excitation is random, instead of sinusoidal, the response will not look like the experimental response shown in FIG. 25. It can be seen that the theoretical estimate of FIG. 24 agrees the experimental data shown in FIG. 25 very well. However, to achieve better system performance, hierarchical controls may be implemented to check other system criteria, which other criteria may override the local control of the H loop. A second level of control is known as the H 2 loop. This is similar to the H x loop in that it is also a form of local control. FIGS. 7A and 7B also represents the components associated with the use of this loop. A measurement of force is taken from the force transducer 65. The force measurement is taken at the same time as the U-, loop performs its velocity check. If the H α loop determines that the relative velocity is near zero, the H 2 loop will then be activated, and the force measured is compared to a small threshold force stored in the memory of the H x processor 67. If the force measured exceeds the threshold force, no action is taken by the controller. After a selected time interval, determined by a timer within the processor 67, the H 2 and H 2 control loops are again called into operation. The purpose of the H 2 loop is to avoid the development of unbalanced forces in a structure. As explained in the discussion of the E-, loop, switching occurs at the point where relative velocity approaches zero. For a typical structure, the dynamics of a building under vibration approximate sinusoidal motion. Thus at the instant velocity is zero, displacement will be at a maximum. Since the ground motions of an earthquake are random, there exists the possibility that a functional switch may be commanded to have zero stiffness at the same instant an undesirable external force propagates through the structure. The net effect will be to cause an overdraft in the deformation of the structure if the functional switch is controlled solely by the H-, loop. This phenomena is shown in FIG. 9B. The H 2 loop will thus override the command of the H x loop in this situation, causing the system to pause until the force situation becomes more favorable. The H 2 loop is intended to act at a local level. Thus each functional switch will have the H 2 control loop integrated into its own control electronics, along with the prior discussed H x control loop. The next level of hierarchical control in the sequential control program is in the H 3 loop. This is a global control loop which is responsible for overseeing the control of each functional switch in the structure. After the H 2 loop of each functional switch has performed its comparison, the command to the functional switch must be verified by the H 3 loop before allowing the command to be executed. The H 3 control loop operates by measuring structural displacement, velocity and acceleration at a number of strategic locations throughout the structure. These measurements are then utilized by the H 3 loop in order to calculate the conservative energy of the structure. The goal of this loop is to minimize the conservative energy. The H 3 loop then analyzes the command from the H 2 loop in order to determine whether or not the H 2 control signal to a given functional switch will tend to decrease the conservative energy of the structure. If the control signal will decrease the conservative energy, then it is sent to the functional switch. If the signal will tend to increase the conservative energy, then the command will not be allowed to issue to the functional switch. The H 3 loop is a global loop in that it simultaneously checks the status of all functional switches in real-time and issues optimal commands according to the principle of minimization of conservative energy. It acts as a central decision making unit. Thus, only one set of control electronics is utilized to implement the H 3 loop. The decision making process of the H 3 loop will be repeated at subsequent time intervals until external excitation and structural vibrations are reduced below pre-established levels. The application of the H 3 loop can best be appreciated from FIG. 10. This figure is similar to FIG. 3, but additionally shows the various control devices which are necessary for the performance of the H 3 control. In order to measure velocity, chevron bracing beams 30.1, 30.2, 31.1 and 31.2 are provided, these being secured at their lower ends to horizontal beams 22.1 and 22.2. The upper ends of the bracing beams are secured to each other and are interconnected with upper horizontal beams 24.1 and 24.2 via velocity transducers 70. Also mounted on the structure are sensors 73 which are capable of measuring displacement and/or acceleration. The output signals from sensors 70 and 73 are received by a computer 74 which processes the received signals and sends out suitable signals to the H α processor 67. The computer 74 also receives feedback signals from the H x processors. The H 3 loop may be implemented through a number of conventional controls, such as proportional-integral- derivative (PID) feedback, state space feedback or various optimization schemes. A neural network control scheme may also be utilized to perform the large number of calculations required to minimize conservative energy. One possible implementation is through the use of a self learning neural network utilizing a modified associative memory modification method. As an alternative to the principle of conservative energy, the H 3 loop may also utilize a velocity displacement theory as the control criteria for issuing commands to the functional switches. Under this type of control, the H 3 loop would only be activated to oversee those discrete portions of a structure where the velocity and/or displacement measurements provided by strategically located transducers exceed certain preset levels. The final level of control in this scheme is known as the malfunction control loop or H 4 loop. The purpose of this loop is to take control of all the functional switches in the structure in the event of a major malfunction in the lower control loop and/or control hardware. A number of measurements of displacement, velocity and acceleration are taken throughout the structure in a continuous fashion. The H 4 loop then compares these values to certain maximum preset levels. If the measurements are found to exceed the maximum allowable values, it is indicative of significant malfunctions in the lower level of controls. In the event that the maximum preset levels are exceeded, the H 4 loop will issue a signal to all of the switches in the structure which overrides the signal of the H 3 loop and will set all of the functional switches to a state so as to insure the safety and stability of the structure to the extent possible without RSM. This may entail either setting all of the switches in the structure "off", or only setting certain switches "off" based on a prior structural analysis. The H 4 loop is considered an independent control loop because it does not continuously monitor the status of each functional switch. Its sole purpose is to provide the appropriate default command signal in the event of system malfunction. The H 4 control does not need any additional hardware than that required for the H 3 control hardware shown in FIG. 10, but it will be necessary to load the computer with a malfunction program which may override the H 3 control output. Experimental tests were conducted utilizing the functional switch arrangement shown in FIG. 4A on a structure shown in FIGS. 7A and 7B. A shaking table was utilized to simulate ground motion in a two directional manner. The shaking table was operated to simulate two forms of ground motion: sweep sine wave input and random vibration input based on actual recorded earthquake motions. The results of the sweep sine wave input provide information on the equivalent damping ratio of the structure. The earthquake ground motion record is used to measure the effectiveness and capability of this invention. The results of Tables I - IV represent a comparison of structural response under a number of operating modes. Since these tests represent a single plane application of this invention, only H- and H 2 type control were utilized. Table I, set forth below, compares the experimental results of four prior art structural damping configurations with the results obtained through the use of a damping type functional switch controlled by the H 2 control scheme. The structure was excited with a controlled input acceleration of .1 g by the shaker table. The equivalent sinusoidal input displacement to the structure was approximately 4 mm. Configuration 1 represented the structure with one rigid brace with a stiffness equal to that of the functional switch maintained in the "on" position. Configuration 2 represented the structure with one viscous damper as a replacement to the rigid bracing of configuration 1. The damping characteristics were similar to that of the functional switch maintained in the "damp" position. Configuration 3 represented the structure with two viscous dampers mounted in the same plane with damping characteristics each equal to that of the functional switch in the "damp" mode. Configuration 4 is the same as configuration 3 except two conventional viscoelastic dampers were also utilized for vibration control. The "Functional Switch" columns of Table I represents the use of a single damping type functional switch controlled with Table I Table II Table III Config. 1 Config. 2 Functional Switch Functional Switch Experimental Theoretical Damping Ratio - (%) 8.3 17.2 32.2 34.0 Maximum deformation (mm) 88.2 68.1 25.4 25.0 RSM reduction (%) 71.2 62.7 Table IV Rigid Bracing Functional Switch Functional Switch Experimental Theoretical Damping Ratio - (%) 8.1 35.2 38.0 Maximum deformation (mm) 27.2 6.0 6.0 RSM reduction (%) 77.3 Maximum base shear (lbs) 507.8 127.0 RSM reduction (%) 77.0 E-, type control, the first column being experimental data and the second representing theoretical results. The maximum deflection and damping ratio of the structure are listed for comparison and reflect the benefits of the E x control of this invention in terms of higher damping ratios and lower structural deflections. Table II represents the results of a test on the same structure as described above, however the input in this test was a controlled constant sinusoidal displacement of 4 mm. The equivalent input acceleration level at the resonant frequency was approximately .1 g. The major difference between the results of Table I and Table II is that Table I shows the results of a feedback controlled acceleration test, whereas Table II shows the results of a feedback controlled displacement test. Table III represents the results of a test on the same structure as described above, however the input in this test was a controlled sinusoidal displacement of 12 mm. The equivalent input acceleration level at the resonant frequency was approximately .3 g. Configuration 1 represents the structure with two rigid braces, each having an individual stiffness equal to that of a functional switch maintained in the "on" position. Configuration 2 represented the structure with two viscous dampers as replacements to the rigid bracing of configuration 1. The damping characteristics of each damper were equal to that of a functional switch maintained in the "damp" mode. Two conventional viscoelastic dampers were also utilized in this configuration. The "Functional Switch" column of Table III represented the use of a single functional switch controlled with E x type control. Table IV represents the results of a test on the same structure as described above, except that in this test, two functional switches were employed in a push-pull arrangement instead of a single functional switch. The input in this test was a controlled input acceleration of .1 g. The equivalent input constant sinusoidal displacement to the structure was approximately 4 mm. The "Rigid Bracing" column of Table IV represents the structure with two rigid braces, each with a stiffness equal to the stiffness of the functional switches when maintained in the "on" position. The "Functional Switch" column represents the use of two push-pull functional switches controlled by both H x and H 2 type control. An application of the present invention when used in the push-pull arrangement of Table IV can be appreciated from a consideration of FIG. 11. In this figure, a one- story structural system is shown consisting of three inverted U-shaped frames 68R, 68C, and 68L, the three frames being connected at their tops by suitable beams 69. On top of the frames there are three concrete slabs 69S the size of 3 by 12 meters each. The weight of the concrete and other static and live loads are considered uniformly distributed over the top floor. Since the central frame 68C is to be treated with the real-time structural modification system of this invention, a structural analysis is performed for the frame wherein the weight, lateral stiffness, and natural frequency of the structure is determined. From this analysis, it is found that the total load on the middle frame is 35,100 kg. By carrying out a standard analysis, it is also found that the natural frequency of the frame is about 3 Hz and its horizontal stiffness K is 1,170,000 kg/m. The theoretical displacement response of the frame under a selected seismic excitation, such as the recorded 1940 El Centro earthquake (FIG. 2) , is calculated and shown in FIG. 12. It is seen that the peak value of the displacement is about 2 cm, which is 1/250 of the frame height of 5 m. According to building code specification, a horizontal displacement of over 1/700 of the story height will result in certain degrees of inelastic deformation of the building structure. Although this is not intolerable, it is desirable that the structure stay within its elastic deformation range. Therefore, the real-time structural modification system of this invention is used to suppress the vibration level back to the code suggest value. Thus a method is selected for minimizing the displacement response of the structure which is based upon the natural frequency of the structure and the percentage deviation from the building code. Normally two steps must be taken when using the RSM system. First a preliminary design is done by using the estimation formula X,,^ = αW/(K + 2K (9) wherein X^ is the maximum displacement allowed, αW is the lateral force, K is the stiffness of the frame, and K., is the apparent stiffness contributed by RSM by the application of functional switches. From the above formula we learn that to insure the value of 1/700, I. should be equal to K, namely 1,170,000 kg/m. After the above calculations have been done, structural modification devices are mounted in the structure which are capable of minimizing the displacement of the structure. In FIG. 13A an RSM system employing functional switches in a push-pull arrangement is somewhat schematically shown installed on the central U-shaped frame 68C, and a push-pull control of the functional switches is shown in FIG. 13B. First, a special steel beam connector, indicated generally at 70, is welded or bolted on the central horizontal beam 68C.2 of the U-shaped frame, not shown in FIG. 13B. Two steel connectors 71 are securely fastened to the lower end of the vertical column portions 68C.1 and 68C.3 of the U-shaped frame 68. Two bracing members 72.1, 72.2, which incorporate functional switches 36.5, 36.6, are installed between the connectors 71 and the special connector 70 as shown in FIG. 13A. The functional switches 36 make the bracing members become adaptive components of the structure. The added functional switches and bracing members provide an additional stiffness which is 100% of the original stiffness contributed by each set of connector, the switch, and the member. The special connector 70 includes a sensor 73 which may be any suitable transducer capable of measuring the displacement, velocity and/or acceleration of the horizontal beam 68c.2 from the base of the columns 68C.1, 68C.3. The sensor 73 is connected to a computer 74 via a suitable electrical cable 75. The computer 74 has available to it stored data and system identification. In addition, as shown in FIG. 13A, each functional switch is provided with a local decision making unit capable of properly operating the associated switch. As the computer receives the information from the sensors, it will process the information and the computer 74 will in turn transmit signals to the local decision making units 76 via lines 78. The system identification and data storage unit is indicated at 80, and the power supply is indicated at 82. Each functional switch may be controlled independently of the other in FIG. 13A. However, in FIG. 13B a control is shown where the switched 36.5 and 36.6 are alternately "on" and "off". Thus the two valves 54 are coupled together by a rigid link 55. When the right hand switch 36.6 is "on", as shown if FIG. 13B, the left hand switch 36.5 will be off. When the right valve is switched to place the right switch in its "off" state, the left will be switched "on". The. control command to the functional switches 36.5 and 36.6 mounted as shown in FIG. 13B is approximately shown in FIG. 14A. Namely, the functional switches 36.5 and 36.6 are alternatively "on" and "off". Thus, two of the functional switches are used as a push-pull (complementary) pair controlled by adaptive programs to keep the apparent stiffness, damping, and mass unchanged but real stiffness, damping and mass of the structure modified. Suppose a structure with first and second push-pull switches are used to modify the stiffness. When the structure moves in one direction, the first switch is "on" against the movement while the second switch is "off." The member connected with the first switch is thus absorbing the displacement energy whereas the member connected with the second switch is releasing the energy which was absorbed in the last cycle. When the structure stops moving in this direction and starts to move in the opposite direction, the first switch is "off" and the corresponding member dumps the energy absorbed while the member connected with the second switch, which is now "on", starts to absorb the energy. A structure using two devices and push-pull arrangement with the simplest control loop, (HI loop) will have an energy dissipation loop (curve of force vs. displacement) of parallelogram (see Fig. 9A) . If we neglect the stiffness, the loop will become a square, as shown in Fig. 14B. From FIG. 14B it can be seen that maximum energy dissipation is achieved with given forces (see F,,^ and F,,^) and given displacements (D max and D^) . This means that the push-pull arrangement dissipates the maximum amount of energy for given maximum/minimum forces and displacements, and therefore it is superior than other arrangements. As a comparison to show the effectiveness of the functional switches as applied to the structure, the same El Centro earthquake record is used to calculate the displacement response of the frame with the functional switches applied. It can be seen from FIG. 15A that the peak value of the displacement response is now .7 cm., which is about 1/700 of the frame height. This is a 70% improvement over the results shown in FIG. 12 and it agrees with the preliminary design. Also, to illustrate the difference between using simple bracing and the functional switches, another treatment of the frame with simple bracing of 100% original stiffness is studied. The corresponding displacement is given in FIG. 15B. It is seen that the peak displacement is only reduced to about 1.6 cm. This improvement is less than 20%. While calculated results are shown in FIGS. 12, 15A and 15B, actual results comparable to those shown in FIGS. 12 and 15A are shown in FIG. 16. In the application just discussed in connection with the structure shown in FIGS. 11 and 13, the functional switches have been used to dissipate energy and to modify the stiffness of the structure in a single plane. However, it should be obvious from FIG. 3 that the functional switches may be used to dissipate energy in more than a single plane. Thus the functional switches 36.3 and 36.4 lie in differing planes. These devices are responsive to variable control (either mechanical or electrical) which is responsive to a measured displacement for controlling the energy displacement device or functional switch in response to the measured displacement to cause the functional switch to dissipate energy and control displacement. While one design of a functional switch has been shown in FIG. 4A, other designs may be employed. For example, a one-time purely mechanical functional switch may be used in some applications. In its simplest form it may consist of a tube coupled to a rod by a shear-pin. Such a device is suitable for both linear and rotational movement. The device shown in FIG. 4A is unidirectional in the sense that the rod is free to move to the left, the return from the reservoir 46 to the chamber 48 being unrestricted through the one-way valve 56. Thus, the switch is always "off" in one direction, but may be set at "off", "on", or "damp" in the other direction. The shear pin functional switch may also be coupled with a variable rate spring. This design is particularly suitable for small structures mounted on rigid substructures, such as mobil homes mounted on concrete piers. FIG. 17 shows a typical embodiment of the present invention used on a bridge. This embodiment includes a bridge 83 slidably mounted on base 84, and fixtures 85.1 and 85.2 which connect a bidirectional functional switch, indicated generally at 86, to the bridge 83 and base 84. In addition sensors 87 are provided which measure input signals such as displacement, velocity, acceleration, strain, etc. of the system. The sensors are connected to a computer 72 which controls the switch 86 in response to the signals received from the sensors. The switch may be nearly instantaneously switched between "on", "off", and "damp" states by the computer. It should be obvious from an inspection of FIG. 17 that the energy from the ground to the bridge, or vice versa, may be controlled. In addition, it should also be obvious that the structural parameters of the bridge may be varied. For example, the mass of the bridge may be varied by coupling or uncoupling the mass of the base to the bridge. Additionally, the stiffness of the switch may be varied, or the relative movements of the bridge and base may be damped. Thus, the bridge as modified in FIG. 17 is an adaptive structure. A design of a bidirectional reusable functional switch is illustrated in FIG. 18, the switch being indicated generally at 86. This design consists of two unidirectional switches of the type generally illustrated in FIG. 4A, with the cylinders 38a and 38b being mounted end to end with their rods 40a and 40b extending in opposite directions. The rods are connected together by means of a yoke assembly which includes two transversely extending bars 88 held in place on the threaded ends 40a.1 a; :ϊ 40b.1 of the rods by means of nuts 89. The bars are in turn coupled together by means of shafts 90, opposite ends of each shaft being suitably connected to an end of an associated bar 88. The yoke assembly may be suitably connected to a fixture 85.2, or any other suitable connector. The cylinders 38 are each provided with brackets 91 which may be coupled to a suitable fixture 85.1 or the like. Each of the cylinders is provided with a port 38a.1 or 38b.1, the ports being in communication with a reservoir 46 via a three position valve 92. The position of the valve may be determined by an electrical controller 58 which is in turn preferably coupled to a computer 72. While the bidirectional switch 86 may act as a damper when the valve is in its damp position, additional dampers 59 (not shown) may be provided. While the mechanism for controlling the valve may be electrical, a variable orifice valve may be used which can be controlled electrically or through a mechanical device, for example a bell crank which senses movement between the cylinder 38 and the rod 40, or the structures to which the cylinder and rod are connected. If controlled electrically, there is typically only a single "damp" setting in order to improve the response time. While in FIGS. 3, 13, and 17 the functional switches are shown being mounted for tension-compression, the functional switches may also be mounted for bending, torsion, or shear. Added damping and stiffness (ADAS) has been used in the prior art to modify a building structure to improve its deflection characteristics. However, it is well known that fixed higher stiffness and fixed higher damping does not always help a structure to reduce its vibration level. Varying damping stiffness and damping can achieve much better results. Besides, functional switches can also change the mass of a structure, which can also help to reduce the vibration level. Therefore, by utilizing the functional switches disclosed above, it is possible to modify structural parameters of mass, damping, and stiffness in real-time. With reference now to FIG. 19, a two story structure is shown having vertical columns 93 and a roof truss 94. Functional switches 36 are mounted between intermediate columns 93.2 and 93.3 in the manner indicated. By setting the functional switches "on" or "off" the central columns are either strongly braced or are not braced at all. Therefore the stiffness of the frame can be changed. The functional switches can also be connected to dampers instead of rigid members. Therefore, the physical parameters of mass, damping and stiffness can be changed simultaneously. The functional switches shown in FIG. 19 may be designed to be subject to extension forces only. Therefore, no buckling caused by compression forces will happen. In this way the links and support for the functional switches need much less cross sectional area so that the cost may be lowered. FIG. 20 illustrates a tall building mounted upon a base isolation unit. The tall building is indicated generally at 10, the base at 96, the base including a hard surface 96.1 and the building including rigid base 10b. Rollers 98 or the like are disposed between the rigid base 10b and the hard surface 96.1 so that the building structure 10 can move relative to the base 96. A functional switch 86 extends between the building 10 and the base 96. This system is different from the design shown in FIG. 19 because it changes the force transfer path and capability from external sources whereas the design shown in FIG. 19 changes the mass, damping, and stiffness of a structure. However, the basic principle is the same as changing the physical parameters of the structure only. FIG. 21 shows another concept of changing mass. In this design a building structure 10, which is mounted directly upon a base 96, is coupled to a mass 100 by means of a functional switch 86. The mass may be another building. As the building 10 and the mass may have different movements (different frequencies, different phases, and different amplitudes) and may be connected or disconnected by means of functional switch 86, the vibrations of the two objects may cancel each other to a certain degree. While the control theory of this invention has been referred to in the objects and summary of the invention, it may perhaps be better understood from a consideration of FIG. 22. Shown in FIG. 22 is a building structure which includes shear walls 102, 104, two spaced apart vertical columns 106, and a mass 108 supported by the columns 106. In addition, a first functional switch 110 is positioned between a column 106 and the shear wall 102, and a second functional switch 112 is positioned between the other column 106 and the shear wall 104. The first functional switch 110 is connected to associv ad shear wall and column by links 114 and 116, and the second functional switch is connected to the associated shear wall 104 and column 106 by links 118 and 120. Each of the shear walls has a stiffness, the stiffness of shear-wall 102 being expressed as K l t and the stiffness of shear wall 104 being expressed as K 2 . According to the principle of minimal conservative potential energy a simple and very effective algorithm is established by switching the stiffness between K- and K 2 to achieve maximum energy drop and minimum displacement. Assuming K- = K 2 switching between the two shear walls 102 and 104 maintains the apparent stiffness constant as K + K 2 or K + K 2 keeps constant. However, the two additional stiffness K α and K 2 , stores and drops potential energy alternately. When the mass 108 is caused to move in the direction of arrow 122 the functional switch 110 is switched "on", while the functional switch 112 is switched "off". If the maximum displacement of the mass caused by the ground motion in the direction of the arrow 122 is x l f the energy stored in the additional stiffness is K 1 x 1 2 /2. When the mass starts to move in the direction of the arrow 124 the switch 110 is switched to its "off" position, and the switch 112 is switched "on". At this time the stiffness K x can move freely and release the energy stored. Thus, the stored energy K 1 x 1 2 /2 is released. An energy dissipation mechanism, associated with the functional switch 110 dissipates this amount of energy within the duration of the movement of the mass in the direction of the arrow 124. Meanwhile, since the functional switch 112 is "on", the stiffness K 2 of shear wall 104 starts to work together with the stiffness K of the main frame 106. That is to say that the stiffness of shear wall 104 (K 2 ) starts to restore the potential energy until the mass reaches the maximum displacement in the direction of the arrow 124, the maximum displacement being denoted by x 2 . Similarly, this amount of energy is equal to K 2 x 2 2 /2 which is to be dropped in the next movement of the mass 108 in the direction of the arrow 122. The time history of this algorithm is conceptually shown in FIG. 23. In this figure the solid line 126 shows the deformation when the functional switch 110 is "on" and the functional switch 112 is "off". The dotted line 128 shows the deformation when the functional switch 110 is "off", and the functional switch 112 is "on". While the equation previously set forth at (5) is applicable to a single degree of freedom system, in a multi-degree of freedom structure the situation becomes a little more complicated. Thus equation (5) .becomes E\ c + E 1 ^ + E L d + E L dI + E 1 ^ + E * - pf = W 1 + T 1 (10) Here, comparing with equation (5) , the newly introduced superscript i describes the i th mode and the letter T stands for the energy transferred from modes other than the i th mode. The term T 1 can be either positive or negative. However, referring to the first mode, or even the first several modes, the term T 1 is positive in most cases [Liang and Lee, "Damping of structures: part I theory of complex damping", NCEER report 91-0004, 1991]. Therefore, the task to minimize the modal conservative potential energy includes minimizing the modal energy transferal also. This principle is that M, C, and K must be changed in such a way that the minimal conservative energy must be achieved. In other words, during the external excitation, the total external energy is treated as follows: prevent a portion of the energy from entering the structure; allow the remaining in, then damp some, and keep some which will be used later to do certain work to prevent external energy from getting in the next step. In a MDOF system, an arrangement that only satisfies equation (5) may not be enough, another amount of energy, the modal energy transfer, should be taken into consideration. It can be seen from the above that functional switches may be selected from energy dissipation devices, like that shown in FIG. 4A, and either mass coupling devices like that shown in FIG. 21, or stiffness modifying devices, like that shown in FIG. 22. Such devices either increase the dynamic impedance of the structure to reduce the input of energy to the structure caused by the application of external energy, or decrease the energy transferred from other modes of the structure, or both, whereby the conservative energy of the structure is minimized. A four-way switch system is shown in FIGS. 26 - 28, which system can be operated in two modes to allow the switches act in both X and Y directions. In FIG. 27, 131 is an oil reservoir; 132 is a mounting housing; 133 is a brake housing; 134 is a turning disk; 135 is a sliding channel; 136 is a slider; 137 is a right plunger; 138 is a right cylinder; 139 is a right oil chamber; 140 is a left plunger; and 141 is a left oil chamber. In FIG. 26, 142 is a bearing of upper cover 143; 144 is a sliding bearing; 145 is a bearing of sliding channel 135; 146.1 is a left pipe; 146.2 is a right pipe; and 147 is a control valve. In FIG. 28, 148 is an electromagnetic brake; 149 is an electromagnet for brake; and 150 is an electromagnet for control valve 147. When a voltage is applied to the electromagnet 149, the brake 148 prevents the disk 134 from turning. Therefore, no relative turning movement between the two ends of the bearing device occurs. When no voltage is applied, the brake does not act, the disk can turn freely due to external torque. When the electromagnet 150 receives the voltage, it pushes to close the control valve 147. Thus, no oil can pass through pipes 146 and valve 147. Therefore, neither plunger 137 nor plunger 140 can move. The position of the slider 136 is fixed. When no voltage is applied, the slider 136 can be moved by external force but receive certain resistance from the control valve 147. Namely, when the valve is opened with larger orifice, less resistance will occur; when the valve is slightly opened with small orifice, heavy resistance will appear. As described above, the brake-disk works as a turning switch. When it is allowed to turn freely, zero torsion stiffness is achieved. When no turning movement is allowed, heavy torsion stiffness will apply. The value of the stiffness is designed according to specific structures. Also, the slider works as a translational switch. When it can be moved freely, no stiffness is added to the structure. However, certain amount damping will be made by adjusting the resistance from the orifice of the control valve 147. When it is fixed, certain value of stiffness is achieved according to specific needs. The opening of the orifice of the control valve is adjusted to achieve certain resistance. The resistance is determined in this way: 1) The slider 136 must be stopped at certain position in desired duration of time (it is allowable to take shorter time duration) , otherwise the cylinder cannot be used in the next step. 2) The damping ratio of the cylinder-plunger system should be at least 70%, otherwise the energy dissipation will not be enough to drop the energy from the entire structure.

Claims: What is claimed is: 1. A method for structure parameter modification of a vibrating structure in real-time; the method being characterized by the combination of the following steps: analyzing physical parameters of the structure; mounting functional switches in the structure in selected locations determined by the analysis, each functional switches having "on" and "off- states; measuring the value of one or more of velocity, acceleration, or displacement of the structure caused by the application of external energy; and providing control means to control the functional switches in real-time in response to the measured values, the controlled functional switches being switched between states to minimize conservative energy of the structure, thereby controlling the displacement of the structure. 2. The method of claim 1 wherein the control means adds minimal energy to the functional switches during the control of the functional switches. 3. The method of claims 1 or 2 wherein the physical parameters are determined by a) determining weight, lateral stiffness, and natural frequency of the structure; and b) then determining a theoretical displacement response of the structure when subjected to a selected seismic excitation by using the figures determined by step a. 4. The method of claim 3 further characterized by the steps of: selecting a method to be employed for minimizing the actual displacement response of the structure if the theoretical displacement response from step b of claim 3 is unacceptable based its percent deviation from building code and upon its natural frequency; and calculating the appropriate modifications of stiffness, mass and damping to achieve the desired displacement response of the structure. 5. The method of any of the preceding claims wherein the functional switches are selected from energy dissipation devices, and either mass coupling devices or stiffness modifying devices, or both, the devices either increasing dynamic impedance of the structure to reduce the input of energy to the structure caused by the application of external energy, or decreasing the energy transferred from other modes of the structure, or both, whereby the conservative energy of the structure is minimized. 6. The method of any of the preceding claims wherein the functional switches are used together with prior art devices for controlling the displacement of the structure, wherein the control means includes threshold values, and wherein the functional switches of this invention are activated when the measured values exceed the threshold values to allow the prior art devices to perform first. 7. The method of controlling the displacement of a structure as set forth in any of the preceding claims wherein the functional switches are mounted in a plurality of intersecting planes, wherein measurement values of one of velocity, acceleration or displacement are taken in more than one plane, and wherein the control means is responsive to measured values in more than one plane, the control means controlling functional switches in intersecting planes. 8. An apparatus for modifying a structure to control its displacement when subjected to the application of external energy due to external forces such as an earthquake or wind, the structure including a frame supported upon a base, said apparatus comprising: sensor means connected to the frame to sense displacement of the frame; functional switch means coupled to the frame; and control means for operating the functional switch means in response to signals received from the sensor means when the sensor means senses displacement of the frame, the functional switches when operated by the control means either minimizing energy of the structure, or preventing transfer of energy to the structure, or both, to thereby minimize the conservative energy of the structure whereby displacement of the structure is minimized. 9. The apparatus as set forth in claim 8 wherein the sensor means includes: a first sensing means for determining position; a second sensing means for determining velocity; a third sensing means for determining acceleration; a fourth sensing means for determining strain; and a fifth sensing means for determining force. 10. The apparatus as set forth in either claim 8 or 9 wherein the functional switch means includes at least one functional switch mounted in a x-z plane of the structure, and at least one functional switch mounted in a y-z plane of the structure, the functional switches being capable of minimizing or preventing transfer of energy from one of said planes to the other of said planes. 11. The apparatus as set forth in any of claims 8 - 10 wherein the functional switch means includes a plurality of functional switches, each functional switch capable of being set to act as a rigid member, to act as a movable unit, or to act as a damper. 12. The apparatus as set forth in claim 11 wherein each functional switch is mechanical. 13. The apparatus as set forth in claim 11 wherein each functional switch is hydraulic. 14. The apparatus as set forth in claim 13 wherein each hydraulic functional switch includes an oil chamber; and an orifice capable of being opened and closed to allow fluid to flow through. 15. The apparatus as set forth in any of claims 11 - 14 wherein each functional switch includes a regulator. 16. The apparatus as set forth in claim 15 wherein the regulator includes an electro-mechanical controller. 17. The apparatus as set forth in claim 15 wherein the regulator includes a mechanical controller. 18. The apparatus as set forth in any of claims 11 - 17 wherein the functional switch means are coupled to the frame by links, wherein the sensor means includes a data acquisition and decision making unit, the data acquisition and decision making unit being connected to the regulator. 19. A method of real-time structure parameter modification (RSM) to control the displacement of a structure comprising the following steps: mounting functional switches in a structure, each functional switch being capable of controlling the displacement of the structure when energy is applied to the structure, and each functional switch capable of being switched between "on" and "off" states; measuring the velocity of the structure adjacent each functional switch, which velocity is caused by the application of external energy to the structure; establishing an initial local structural control signal for each functional switch in response to the measured velocity of the structure adjacent the associated functional switch; and providing control means for causing the functional switch to act upon the control signal in the absence of any override signal in such a manner that the functional switch will control displacement of the structure. 20. The method of controlling the displacement of a structure as set forth in claim 19 wherein, when the velocity approaches zero, the local structural control signal is initiated which, when acted upon, will change the state of the functional switch. 21. The method of controlling the displacement of a structure as set forth in either claim 19 or 20 wherein the functional switches are mounted in a plurality of intersecting planes, a wherein the velocity is measured in more than one plane. 22. The method of controlling the displacement of a structure as set forth in one of claims 19, 20 or 21 wherein a force measurement is taken for each functional switch, and a comparison is made to see if the measured force exceeds a threshold force, and either initiating an override signal if the force exceeds the threshold level to prevent the associated functional switch from acting upon the initial local structural control signal until after a prescribed time delay, or not initiating an override signal if the force does not exceed the threshold level. 23. The method of controlling the displacement of a structure as set forth in claim 22 wherein measurements are taken at a number of strategic locations of acceleration and structural displacement, wherein the conservative energy of the structure is calculated using the measured values of velocity, acceleration and structural displacement, wherein the status of all functional switches is determined in real-time, and wherein optimal commands are issued to the functional switches to change their state according to a velocity displacement theory. 24. The method of controlling the displacement of a structure as set forth in claim 22 wherein measurements are taken at a number of strategic locations of acceleration and structural displacement, wherein the conservative energy of the structure is calculated using the measured values of velocity, acceleration and structural displacement, wherein the status of all functional switches is determined in real-time, and wherein optimal commands are issued to the functional switches to change their state according to the principle of minimization of conservative energy. 25. The method of controlling the displacement of a structure as set forth in claim 24 wherein a determination is made to establish a fail-safe setting for all functional switches to insure the stability of the structure to the extent possible without RSM, wherein the measurements of displacement, velocity and acceleration values are compared to certain maximum preset levels, and if the measurements are found to exceed the maximum allowable values, override signals are sent to cause all functional switches to be in the fail-safe setting. 26. An apparatus for real-time structure parameter modification (RSM) whereby the displacement of a structure may be controlled; the apparatus comprising: a plurality of functional switches (36) mounted in a structure, each functional switch being capable of controlling the displacement of the structure when energy is applied to the structure, and each functional switch capable of being switched between "on" and "off" states; a velocity transducer (64) mounted in the structure adjacent each functional switch (36) for measuring the velocity of the structure adjacent each functional switch, which velocity is caused by the application of external energy to the structure, each velocity transducer initiating a signal in response to measured velocity; control means (67) which establishes an initial local structural control signal for each functional switch in response to the associated velocity signal; and means (57) for causing the functional switch to act upon the control signal in the absence of any override signal in such a manner that the functional switch will control displacement of the structure. 27. The apparatus as set forth in claim 26 wherein the functional switches and velocity transducers are mounted in a plurality of planes. 28. The apparatus as set forth in either claim 26 or 27 wherein a force measuring means (65) is provided, the force measuring means initiating a force signal in response to the application of a force for each functional switch, and wherein the control means is provided with comparison means to see if the measured force exceeds a threshold force, the control means being provided with means to initiate an override signal if the force exceeds the threshold level an override signal will be initiated to prevent the associated functional switch from acting upon the initial local structural control signal until after a prescribed time delay. 29. The apparatus as set forth in claim 28 wherein acceleration and displacement transducers (73) are mounted at a number of strategic locations in said structure, wherein a computer (74) is provided to calculate the conservative energy of the structure using the measured values of velocity, acceleration and structural displacement, wherein feedback lines are provided from all functional switches to the computer so that the status of the functional switches is determined in real-time, and wherein the computer issues optimal commands to the functional switches to change their state according to the principle of minimization of conservative energy. 30. A method for real-time structure parameter modification of a vibrating structure; the method being characterized by the combination of the following steps: providing a first pair of first and second functional switches, each switch capable of being switched between an "on" state where there is essentially no relative movement between first and second parts of the switch, and an "off" state where the first and second parts of the switch may move freely relative to each other; mounting the functional switches in a structure in such a manner that if the first functional switch of the first pair were placed under tension due to the application of external energy, and the second functional switch of the first pair would be placed under compression; measuring one or more of the velocity, acceleration, or the displacement values of the structure caused by the application of external energy; and changing the state of the functional switches between "on", and "off" states in response to the measured values, the functional switch under compression being switched "on", and the functional switch under tension being switched "off". 31. The method of claim 30 wherein the first pair of functional switches are mounted in a common plane. 32. The method of claim 31 further characterized by the steps of: providing a second pair of first and second functional switches, each switch of the second pair capable of being switched between an "on" state where there is essentially no relative movement between first and second parts of the switch, and an "off" state where the first and second parts of the switch may move freely relative to each other; mounting the second pair of functional switches in a second plane, the second plane intersecting the first plane, the second pair of functional switches being mounted in such a manner that if the first functional switch of the second pair were placed under tension due to the application of external energy, the second functional switch of the second pair would be placed under compression; changing the state of the functional switches of the second pair between "on", and "off" states in response to the measured values, the functional switch under compression being switched "on", and the functional switch under tension being switched "off". 33. The method of any of claims 30 - 32 wherein one end of the first functional switch of one of the pairs is adjacent one end of the second functional switch of the same pair. 34. The method of any of claims 30 - 33 wherein the functional switches are controlled by adaptive algorithms to keep the apparent stiffness, damping and mass unchanged but real stiffness, damping and mass of the structure modified. 35. Method of real-time structural parameter modification comprising the following steps: providing functional switches, each of which can be switched between an "on" state where there is essentially no relative movement between first and second parts of the switch, a "damping" state where movement between the first and second parts of the switch absorb energy, and an "off" state where the first and second parts of the switch may move freely relative to each other; mounting the functional switches in a structure whose physical parameters of mass, damping and stiffness can be modified by the switches; measuring the values or one or more of velocity, acceleration, or the displacement of the structure caused by application of external energy in more than one plane; and changing the state of the functional switches between "on", "off", and "damping" states in response to the measured values and corresponding adaptive control algorithms to effectively dissipate energy applied to the structure and control displacement of the structure. 36. Method of real-time structural parameter modification as set forth in claim 35 wherein functional switches are mounted in the structure in intersecting planes, and wherein the displacement of the structure is controlled in more than one plane simultaneously. 37. The method of real-time structural parameter modification as set forth in either claim 35 or 36 wherein the functional switch when controlled in response to the measured velocity, force, displacement, and acceleration and corresponding adaptive control algorithms link and un¬ link certain members and substructures to vary the mass of the structure. 38. A functional switch comprising: a cylinder assembly having opposed axially aligned first and second separated bores; first and second rods slidably disposed within the first and second bores, respectively; coupling means coupling the first and second rods together for simultaneous movement; and a fluid passageway extending between adjacent ends of the bores, the fluid passageway being provided with a valve for controlling the flow from one bore to the other.

Inventors: LEE GEORGE C, LIANG ZHONG, TONG MAI, LEE, GEORGE, C., LIANG, ZHONG, TONG, MAI
Applicants: LEE GEORGE C, LIANG ZHONG, TONG MAI, UNIV NEW YORK, LEE, GEORGE, C., LIANG, ZHONG, THE RESEARCH FOUNDATION OF STATE UNIVERSITY OF NEW, TONG, MAI
Application year: 1995
Main classification: E02D27
IPC codes: E01D19, E02D27, E02D31, E04B1, E04H9, F16F15, G05D19