CONTROL OF AN ACTIVE SUSPENSION SYSTEM FOR A WORK VEHICLE BASED UPON A PARAMETER OF ANOTHER VEHICLE SYSTEM

Abstract: An active suspension system (26) for a work vehicle (2) disclosed herein. The system (26) includes at least one active vibration isolator (28, 30, 32) mounted between the chassis (4) and cab (6) of the vehicle (2). The isolator (28, 30, 32) moves the cab (6) relative to the chassis (4) in response to a control signal generated by a control circuit. The control circuit communicates to a second vehicle system (258-264) via a communication interface. The communicated data includes a parameter of the second vehicle system (38, 39) related to a force applied to the vehicle (2) during operation of the second vehicle system (38, 39). The control signal is generated at least partly in response to the parameter so as to minimize the vibration on the cab (6) caused by operation of the second vehicle system (38, 39). Cab movement may be disabled when ground speed of the vehicle is below a predetermined speed threshold or when an operator presence sensor detects that the operation is not present.

Description: CONTROL OF AN ACTIVE SUSPENSION SYSTEM FOR A WORK VEHICLE BASED UPON A PARAMETER OF ANOTHER VEHICLE SYSTEM FIELD OF THE INVENTION The present invention relates generally to the field of active suspension systems. More particularly, the invention relates to an active suspension system for a work vehicle which includes at least one active vibration isolator, wherein a control circuit communicates between the isolator and another vehicle system and generates control signals for the isolator which depend at least partly upon a parameter of the another vehicle system. BACKGROUND OF THE INVENTION The ride quality and operator comfort of a work vehicle is adversely affected by vibrations or movement transmitted from the frame or chassis of the vehicle to the operator's cab. As the work vehicle travels across a surface, movement of the chassis induces the operator's cab to pitch, roll and bounce. Movement of the cab can be particularly severe in agricultural and construction equipment vehicles (e.g., tractors, combines, backhoes, cranes, dozers, trenchers, skid-steer loaders, etc.) because such vehicles typically operate on off-road surfaces or fields having a high level of bumpiness. Operator comfort may also be adversely affected by the operation of various systems on a work vehicle. In particular, operation of various work vehicle systems can cause forces to be applied to the chassis of the vehicle which, in turn, are transmitted to the cab. Examples of these forces include the following: draft forces exerted on the hitch of an agricultural tractor by an implement (e.g., a plow) which can cause the cab to pitch; normal forces applied to a work vehicle as the vehicle turns in response to a steering device which can cause the cab to roll; clutch forces generated when a work vehicle clutch (e.g., a main drive clutch; four-wheel drive clutch) is engaged or disengaged which can cause the cab to pitch; gear shift forces generated when a transmission of a work vehicle is shifted which can cause the cab to pitch; braking forces generated as brakes of a work vehicle are operated which can cause the cab to pitch; acceleration forces generated when a speed actuator changes the speed of a work vehicle which can cause the cab to pitch; etc. The movement of the cab caused by surface bumps and the operation of vehicle systems cause both qualitative and quantitative problems. An operator of such a vehicle experiences increased levels of discomfort and fatigue caused by the vibrations. Productivity is decreased when an operator is forced to rest or shorten the work day, or is unable to efficiently control the work vehicle. The operator is also less likely to be satisfied with a work vehicle which provides poor ride quality. Under certain conditions, the frequency and magnitude of cab movement may force the operator to decrease driving speed, further decreasing productivity. To improve ride quality and operator comfort, work vehicles have been equipped with passive, semi-active or active suspension systems to isolate the operator from vibrations caused by surface bumps . Such systems include vibration isolators mounted between the chassis and cab or seat. Passive systems use passive vibration isolators (e.g., rubber isolators, springs with friction or viscous dampers) to damp vibrations with different isolators used to damp different frequencies. Rubber isolators may be used, for example, to damp high frequency vibrations and air bags used to damp low frequency vibrations. However, performance of passive systems is limited due to design compromises needed to achieve good control at resonance frequencies and good isolation at high frequencies . Semi-active systems achieve control and isolation between the chassis and the cab -by controlling a damper to selectively remove energy from the system in response to movement of the cab sensed by sensors. Active systems use sensors to sense cab movement and a controller to generate control signals for an actuator which applies a force to the cab to cancel vibrations transmitted to the cab by the chassis. The power needed to apply the force is supplied by an external source (e.g., hydraulic pump) . As the above paragraphs imply, it is desirable that a suspension system attenuate both low and high frequency vibrations between the chassis and cab. Attenuation of high frequency vibrations can decrease acoustic noise in the cab, decrease fatigue and decrease vibration-induced mechanical faults. Attenuation of low frequency (e.g., less than 20 Hz) vibrations can decrease operator fatigue and improve vehicle operability. The attenuation of low frequency vibrations is particularly important because the resonant frequencies of the human body are typically below 20 Hz. For example, the human abdomen resonates at frequencies between 4-8 Hz, the head and eyes resonate at frequencies around 10 Hz, and the torso at 1-2 Hz. The actual frequency may vary with the particular individual. One active suspension system for a work vehicle includes a hydraulic actuator mounted at a single point between the rear of the cab and the vehicle frame . The front of the cab is pivotally mounted to the frame. The actuator is controlled to move the cab relative to the frame in response to sensed acceleration signals. The system includes a single air bag used to level the cab. This system, however, only affects cab pitch since the actuator can only pivot the cab about the single point . Further, the control signals applied to the actuator do not depend on parameters of other vehicle systems which are indicative of forces applied to the vehicle due to operation of those systems. Thus, the system does not specifically react to the forces caused by other systems. Another active suspension system for a work vehicle includes one active vibration isolator mounted between the vehicle chassis and the rear of the cab, and two active isolators mounted between the chassis and the front of the cab. Each isolator includes a hydraulic actuator mounted between the chassis and the cab, and an air bag to support the weight of the cab. The actuator is controlled to move the cab relative to the chassis in response to sensed acceleration signals. Each isolator is individually controlled by an electronic controller replicated for each isolator. Thus, the control signals applied to the actuators are not coordinated with each other to provide coordinated control of the isolators. Further, as with the other system, the control signals applied to the actuator do not depend on parameters of other vehicle systems indicative of forces applied to the vehicle due to operation of those systems. SUMMARY OF THE INVENTION Accordingly, the present invention provides an improved active suspension system for a work vehicle. The improved suspension system includes a control circuit which communicates via a communication interface to other vehicle systems which are the source of vibrations. The system includes an active vibration isolator responsive to control signals generated at least partly in response to parameters of the other systems which relate to forces applied to the vehicle during operation of those systems. The system can react to draft forces generated by a plow, normal forces which occur during steering, clutch forces generated as a clutch engages and disengages, gear shift forces generated by a transmission, braking forces due to braking and acceleration forces due to speed changes. One embodiment of the invention relates to an active suspension system for a work vehicle. The work vehicle includes a chassis, an operator'-s cab and another vehicle system having a parameter related to a force applied to the work vehicle . The suspension system includes an active vibration isolator located between the cab and the chassis and responsive to a control signal to control movement of the cab relative to the chassis, a communication interface coupled to the another vehicle system, and a control circuit configured to receive the parameter of the another vehicle system from the communication interface, to generate the control signal at least partly in response to the parameter, and to apply the control signal to the vibration isolator to attenuate movement of the cab due to the force. Such a system can also be mounted between the cab and operator's seat, or between the wheels and the chassis. Another embodiment of the invention relates to a work vehicle including a chassis, an operator's cab, an active suspension system including at least one active vibration isolator mounted between the cab and chassis and responsive to a control signal to control movement of the cab relative to the chassis, another vehicle system having a parameter related to a force applied to the work vehicle, and a communication interface coupled between the suspension system and the another vehicle system. The system further includes a control circuit configured to receive the parameter of the another vehicle system, to generate the control signal at least partly in response to the parameter, and to apply the control signal to the active vibration isolator to attenuate movement of the cab due to the force . Another embodiment of the invention relates to an active suspension system for a work vehicle. The work vehicle includes a chassis, an operator's cab disposed above the chassis, and a second vehicle system having a parameter related to ground speed of the work vehicle. The active suspension system includes at least one active vibration isolator mounted at a location between the cab and the chassis and responsive to a control signal to control movement of the cab relative to the chassis, a communication interface coupled to the second vehicle system, and a control circuit configured to receive the parameter of the second vehicle system from the communication interface, to generate the control signal applied to the isolator to attenuate movement of the cab when the ground speed is above a predetermined speed threshold, and to disable cab movement when the ground speed is below the threshold. BRIEF DESCRIPTION OF THE DRAWINGS The invention will become more fully understood from the following detailed description, taken in conjunction with the accompanying drawings, wherein like reference numerals refer to like parts, in which: FIG. 1 shows a work vehicle (e.g., an agricultural tractor) equipped with an active cab suspension system which includes two front and one rear active vibration isolators located between the vehicle's cab and chassis; FIG. 2 is a schematic rear view of the work vehicle shown in FIG. 1; FIG. 3 is a view from the side of the work vehicle of one of the front active vibration isolators which includes electrical interfaces to an accelerometer, a displacement sensor, a load sensor, a pressure sensor and a hydraulic actuator, a hydraulic interface to the actuator, and a pneumatic interface to an air spring; FIG. 4 is an exploded view of the accelerometer mounting assembly shown assembled in FIG. 3; FIG. 5 is a cross-sectional view of the coupling between the accelerometer and the actuator's piston; FIG. 6 is a view from the rear of the work vehicle of the rear active vibration isolator which includes two springs to support the weight at the rear suspension point ; FIG. 7 is a mechanical schematic of the active vibration isolator shown in FIG. 3; FIG. 8 is a schematic diagram of the active cab suspension system in FIG. 1 including connections between the electrical, hydraulic and pneumatic interfaces of the active vibration isolators and a controller, pressurized hydraulic fluid source and pressurized air source ; FIG. 9 is a schematic block diagram of the active suspension controller of FIG. 8 which includes a data bus interface for communicating with other vehicle systems; FIG. 10 is a process flow control diagram for the hydraulic actuator of each active vibration isolator; FIG. 11 is a schematic block diagram representing interconnections across a vehicle data bus between the active suspension controller and other vehicle systems; FIG. 12 is a block diagram of the positioning control system in FIG. 11 which includes a GPS receiver, memory card interface, and positioning control circuit; FIG. 13 is a table representing a predetermined geo- referenced map including spatially-variable data indicative of altitudes and bumpiness levels; FIG. 14 represents a predetermined geo-referenced map of a road and a field which includes bumpiness level data; and -FIG. 15 shows a work vehicle equipped with another embodiment of an active cab suspension system including an active isolator located between a side of the cab and a vertical support member (eg., engine compartment wall) , DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Referring to FIGs. 1 and 2, a work vehicle 2 (e.g., an agricultural tractor) includes a frame or chassis 4, an operator's cab 6 supported above chassis 4, a seat or dual seats 8 within cab 6, and a propulsion system 10 to propel vehicle 2 along a ground surface 12 in a forward direction 14. Propulsion system 10 includes an engine 16 secured to chassis 4, a transmission (not shown) coupled to engine 16, two driven or non-driven front wheels 18 steered by a steering wheel 20, and two rear wheels 22 driven by engine 16 via the transmission. Brake pedals 24 located in cab 6 operate left and right service brakes (not shown) to provide braking. Cab 6 is supported above chassis 4 by an active cab suspension system (ACS) 26 including two front active vibration isolators 28 and 30 located on opposite sides of cab 6 and a rear isolator 32 centrally located at the rear of cab 6 between wheels 22. The three-point suspension system provides stable control of movement responsive to pitch, roll and bounce. In some work vehicle applications, ACS 26 includes a forward-looking sensor 34 mounted to vehicle 2 to detect the bumpiness level on surface 12 forward of vehicle 2. Sensor 34 may include a radar to detect bumpiness based on the time needed for electromagnetic signals to travel from sensor 34 to surface 12 and be reflected back. However, sensor 34 could also include a vision-based or proximity sensor (e.g., a micropower impulse radar (MIR) device) . Sensor 34 is mounted to vehicle 2 at a location oriented toward surface 12. For example, sensor 34 may be mounted on the hood of vehicle 2 (34a) , or mounted below vehicle 2 to detect bumpiness forward of rear wheels 22 (34b) , or mounted forward of front wheels 18 (34c) . The sensed signals represent general levels of bumpiness (e.g., a smooth or rough surface) and are used to adjust performance parameters of isolators 28-32. In some work vehicle applications, ACS 26 includes a leveling sensor 36 mounted to cab 6 to generate signals indicative of the degree to which the attitude of cab 6 is level relative to horizontal. Leveling sensor 36 may include a gyroscope or electronic level signal generator, and sensor 36 may be mounted at the center of gravity of cab 6. The signal from sensor 36 can be used to control the attitude of cab 6 and to maintain a level attitude. ACS 26 may further include a movement sensor 37 (e.g., a three-axis accelerometer) mounted adjacent to an operator's torso or head (e.g., supported by a headrest of seat 8) to accurately sense the movement felt by the operator. The signal from sensor 37 is used as a primary or secondary control input to more accurately control the movement of cab 6 and its affect on the operator. ACS 26 may also include several accelerometers mounted to cab 6. These signals are combined to form a control input. Components of other vehicle systems within cab 6 may include a steering angle sensor 38 coupled to wheel 20 to generate a signal representing steering angle, and brake detecting circuits 39 coupled to brake pedals 24 to detect application of the service brakes. Circuits 39 can also be coupled directly to the brakes. The signals generated by sensor 38 and circuits 39 are supplemental control inputs used by ACS 26 to counteract movement of cab 6 due to forces applied to chassis 4 when turning or braking, or are used as preparatory signals (e.g., to bias the hydraulic fluid supply toward the particular isolator which will require the fluid) . As explained below, ACS 26 attenuates transmission of vibrations between chassis 4 and cab 6 caused by the interaction of wheels 18 and 22 with surface 12, or due to forces applied to vehicle 2 during operation of other vehicle systems such as the steering, transmission and braking systems. Each isolator 28-32 can be controlled separately, or coordinated with each other to improve vibration isolation and to provide additional functions. Coordinated control of isolators 28-32 can provide improved response to pitch, roll and bounce forces applied to cab 6. Performance parameters of ACS 26 are adjustable in response to estimated conditions ahead of vehicle 2, or to changes in load. The gain, and thus the frequency response, of ACS 26 is set to maximize the vibration isolation of ACS 26 without exceeding the mechanical limits (i.e., actuator stroke) of the system. The gain can further be tuned manually to account for differences among the frequency response of individual operators . Although a tractor is shown in FIGs. 1 and 2, ACS 26 may be used with other agricultural work vehicles such as combines or cotton-pickers or with construction vehicles such as backhoes, cranes, dozers, trenchers, skid-steer loaders, etc. These vehicles may be equipped with either wheeled or tracked propulsion systems. Other arrangements of ACS 26 can be used in these vehicles such as a three-point active suspension system including one front and two rear isolators or a four-point system with two front and two rear isolators. Further, one or more active vibration isolators 28-32 can be mounted between cab 6 and seat 8 in an active seat suspension system. Referring to FIG. 3, front active vibration isolator 28, which is substantially the same as front isolator 30, includes lower and upper mounts 40 and 42, respectively, which are attached to chassis 4 and cab 6, respectively, by welding, screws, bolts or other fasteners. A spring 44 including an air bag is connected between mounts 40 and 42 to support the static weight of cab 6. Spring 44 includes an enclosure 46 comprising a cylindrical outer casing 48 attached (e.g., welded) to lower mount 40 and a cylindrical inner casing 50 attached to upper mount 42 and extending into outer casing 48. The air bag (not visible) is secured within enclosure 46. The air bag is inflated with pressurized air through a supply tube 52 and a pneumatic fitting 54 to a pressure sufficient to support the static weight of cab 6 so as to off-load the weight from other components of isolator 28. In some work vehicle applications, the air pressure in springs 44 is set at a constant level to support the static weight of cab 6, and the pressure is not adjusted to account for changes in load of cab 6 on isolators 28- 32. In such applications, a pneumatic system is charged with pressurized air supplied to spring 44 through tube 52. The pressure of the air supplied to spring 44 is set or regulated at or slightly below the pressure needed to raise cab 6. Solenoid-controlled valves turn on the flow of air to isolators 28-32. Such systems may be pressurized off-line so the vehicle does not require an on-board air compressor. Alternatively, air pressure in such pneumatic systems may be maintained by an on-board air compressor to replace air lost to leaks. This type of system does not actively control air pressure, and does not respond to changes in the weight of cab 6. However, in other work vehicle applications, ACS 26 actively controls the air pressure within springs 44. As described below, such systems include air control valves to selectively supply and relieve pressurized air from a source (e.g., a compressor and/or high pressure air tank) to springs 44 in response to control signals generated based on, for example, load forces exerted on springs 44 by cab 6. The compressed air source provides the ability to actively control pressure during operation of vehicle 2. To improve accuracy in controlling pressure, the pressure in springs 44 may be monitored using a pressure sensor 56 mounted to upper mount 42 and configured to generate closed-loop pressure feedback signals on conductors 58. Isolator 28 includes a rollover restraint system 60 to prevent cab 6 from detaching from chassis 4 during a rollover. Restraint system 60 includes a rollover frame 62 secured (e.g., welded) to lower mount 40 which is able to cooperate with a plate 64 secured to outer casing 48. Frame 62 includes a circular hole 66 having a diameter slightly larger than that of casing 48 but less than that of plate 64. In the event of a rollover causing casing 48 to separate from lower mount 40, casing 48 can slide upward within hole 66 until plate 64 makes contact with frame 62. Thus, movement of cab 6 caused by a rollover is restrained and cab 6 does not detach from chassis 4. Connected adjacent to spring 44 between mounts 40 and 42 is a linear hydraulic actuator 68. Actuator 68 includes a cylinder 70 and a piston or rod 72 moveable therein to move cab 6 relative to chassis 4. A valve assembly 74 coupled to cylinder 70 selectively supplies and relieves pressurized hydraulic fluid between a pair of tubes 76 and 78 and cylinder 70 in response to valve control signals received on conductors 80. Thus, piston 72 moves in either direction along the axis of cylinder 70 in response to the control signals. Preferably, the control signals are pulse-width modulated (PWM) control signals and valve assembly 74 is a four-way, three- position electrically-controlled solenoid valve. Referring to FIGs. 3-5, a threaded free end 82 of piston 72 extends through upper mount 42 and is coupled to a movement sensor 84 via a mounting assembly 86 which provides high-frequency isolation of sensor 84 from mount 42. In upward order, assembly 86 includes an internally- threaded rod nut 88 for receiving end 82, a potentiometer target bracket 90 having an aperture 92, a lower hardened washer 94 having an aperture 96, an elastomeric vibration isolator 97 having lower and upper isolator portions 98 and 100 located on opposite sides of upper mount 42 and having apertures 102 and 104, an upper hardened washer 106 having an aperture 108, and a bolt/sleeve 110 having a threaded bore 112 to securely receive free end 82 of piston 72. Isolator portions 98 and 100 include inner annular portions 114 and 116, respectively, which pass through an aperture 118 in mount 42. The components of assembly 86 are coaxially aligned such that piston 72 passes through nut 88, apertures 92, 96, 102, 118, 104 and 108 and bore 112. Thus, elastomeric vibration isolator 97 physically separates upper mount 42 from piston 72 to provide high-frequency isolation. Bolt/sleeve 110 includes a tapped hole 120 coaxial to piston 72 to receive a threaded post 122 of movement sensor 84, thereby securely mounting sensor 84 to piston 72. Sensor 84 generates an electrical signal on conductors 124 which represents movement of piston 72 in a direction along the axis of piston 72 at a point P (e.g., at washer 94) lying between actuator 68 and elastomeric isolator 97. Thus, isolator 97 provides high-frequency isolation between upper mount 42 and movement sensor 84. Sensor 84 preferably includes an accelerometer. During operation, valve control signals generated in response to the signals from sensor 84 are applied to actuator 68 to move cab 6 to counteract the movement of chassis 4. Post 122 can alternatively be secured directly to a bore in end 82 of piston 72. Potentiometer target bracket 90 includes first and second flat portions 126 and 128 and a rising portion 130 extending from portion 126 to 128. A displacement sensor 132 (e.g., potentiometer; inductive sensor) is adjustably secured by bolts 134 to a track 136 running along valve assembly 74. Sensor 132 generates electrical signals on conductors 138 representing the distance that actuator shaft 140 extends from casing 142. This distance is indicative of the displacement between mounts 40 and 42. The displacement signal from sensor 132 is used to bias piston 72 to a centered steady-state position so as to prevent migration to either end of cylinder 70 over time, and to control the height of cab 6 above chassis 4. Vibration isolator 28 may also include a load sensor 144 which generates electrical signals on conductors 146 representing load forces exerted by cab 6 on chassis 4. The load forces can be used to adjust air pressure within spring 44 to account for changes in weight of cab 6. For example, changes in the weight of an operator, or changes due to having two people in cab 6, can be accommodated. To accommodate translational movement between chassis 4 and cab 6, a spherical bearing assembly 148 is provided between cylinder 68 and lower mount 40. Assembly 148 includes a bearing eye 150 which extends down from cylinder 68 and encompasses a spherical bearing 152. Eye 150 fits into a slot within a bearing block 154 mounted to lower mount 40, and is held in place by a crosspin 156 inserted through an aperture in block 154 and bearing 152. Assembly 148 allows relative movement of cylinder 68 about the axis of bearing 152. Although FIG. 3 shows actuator 68 adjacent to spring 44, actuator 68 and spring 44 may be coaxially located as shown in U.S. Pat. No. 5,603,387, herein incorporated by reference in its entirety. Referring to FIG. 6, rear isolator 32 is similar to front isolator 28 except that rear isolator 32 includes a second spring 44 to off-load the higher static weight of cab 6 on rear isolator 32. Off-loading may be necessary to avoid exceeding the weight capacity of a single air bag. However, a second spring may not be needed if ACS 26 includes four active isolators, or if the cab weight does not exceed the capacity of a single air bag. Other differences between rear isolator 32 and front isolator 28 include the shapes of potentiometer target bracket 90 and of upper mount 42 (which both extend between springs 44) , and the coupling of elastomeric vibration isolator 97 to bracket 90 instead of to upper mount 42. Sensor 132 is mounted on or within cylinder 70 such that sensor 132 and cylinder 70 are co-linear. Referring to FIG. 7, each vibration isolator 28-32 is represented by a mechanical schematic showing spring 44 connected between cab 6 and chassis 4, actuator 68 connected between chassis 4 and point P (e.g., at washer 94) , and elastomeric vibration isolator 97 in series with actuator 68 between point P and cab 6. Actuator 68 provides low frequency (e.g., below 20 Hz) isolation between chassis 4 and point P. Isolator 97 provides high frequency (e.g., above 20 Hz) isolation between point P and cab 6. Thus, cab 6 is isolated from chassis 4 for both high and low frequency movement or vibrations. Each individual active vibration isolator 28-32 has characteristics defined by the mass M of cab 6 supported by the isolator, the stiffness K s of spring 44, the input velocity V c of actuator 68, and stiffness K and damping coefficient R of isolator 97. Stiffness K s of spring 44 affects only the power consumption of actuator 68 and does not affect idealized isolation. The quantity being actively controlled is input velocity V c of actuator 68. Referring to FIG. 8, ACS 26 includes front isolators 28 and 30, rear isolator 32, an active suspension system controller (ASC) 200, a source of pressurized hydraulic fluid 202, a pressurized air source 204, an air control valve- 206 for each isolator 28-32, and a vehicle data bus 208. ASC 200 is connected by electrical conductors to movement sensor 84, displacement sensor 132, load sensor 144, air pressure sensor 56, valve assembly 74, and air control valve 206 of each isolator 28-32, and to bump sensor 34, leveling sensor 36, and movement sensor 37. ASC 200 receives signals from each sensor and generates output signals in response thereto which are applied to valves 74 and 206. ASC 200 further communicates to and from other vehicle systems via bus 208. Preferably, bus 208 conforms to the SAE J-1939 standard for vehicle data busses entitled "Recommended Practice for a Serial Control and Communications Vehicle Network" . Pressurized hydraulic fluid source 202 includes an engine-driven pump 210 to supply pressurized hydraulic fluid to isolators 28-32 via tubes 76 under the control of valve assemblies 74. Valve assemblies 74 also control release of fluid from isolators 28-32. Released fluid is returned to a reservoir 212 of source 202 via tubes 78. When pressure in springs 44 is actively controlled, each air control valve 206 includes an apply valve 214 which receives a flow of pressurized air from source 204 (e.g., a compressor) and selectively applies the flow to spring 44 of each isolator 28-32 in response to control signals generated by ASC 200. Each valve 206 includes a release valve 216 to selectively release air from the air bag to a vent 218 in response to the air control signals. The pressure within each air bag increases up to the maximum pressure of source 204 when the apply valve 214 is open, and decreases when release valve 216 is open. The air control signals may include PWM signals. Referring to FIG. 9, ASC 200 includes a signal conditioning/multiplexer circuit 220 to receive signals from sensors 84, 132, 144 and 56 of each isolator 28-32 and from sensors 34, 36 and 37. - ASC 200 further includes an active suspension control circuit (ASCC) 222 coupled to circuit 220, a memory circuit 224 accessible to ASCC 222, an interface circuit 226 to generate control signals (e.g., PWM signals) to valve assembly 74 and air control valve 206 associated with each isolator 28-32, and a data bus interface circuit 228 configured to communicate with other vehicle systems across bus 208. Circuit 220 includes signal conditioning hardware (e.g., filters), multiplexers and A/D interface circuits. ASCC 222 includes a digital processor (e.g., a 16-bit microprocessor) which may include software conditioning such as digital filtering or averaging. Memory circuit 224 includes nonvolatile memory (ROM, EEPROM or FLASH) for storing programs and volatile memory (RAM) for storing variables. Dedicated, specific purpose equipment or hard-wired logic circuitry can also be used. PWM interface circuit 226 generates PWM control signals based upon digital words written to circuit 226 by ASCC 222. Interface circuit 228 formats input and output bus messages which conform to the J-1939 standard protocol. ASC 200 includes an operator interface circuit to receive command signals from operator-actuatable command devices and control operation of ACS 26. The interface includes a signal conditioning/multiplexer circuit 230 (which may be the same as circuit 220) which receives signals from command devices 232-238. Devices 232-238 include any or all of: a cab rate command device 232 (e.g., potentiometer) to set a rate at which cab 6 moves during power-up/power-down; a cab height command device 234 (e.g., potentiometer) to set a steady-state height of cab 6 above chassis 4; a cab lower command device 236 (e.g., switch) to command cab 6 to a minimum height; and a tuning device 238 (e.g., potentiometer) to tune the gain, and thus the frequency response, of ACS 26. Referring to FIG. 10, ASC 200 generates the valve control signals applied to actuator 68 via conductors 80 for each active vibration isolator 28-32. The control signals may be generated individually for each isolator 28-32 using the process shown in FIG. 10. The inputs to the process are displacement signal D (FIG. 7) sensed by sensor 132, and acceleration signal A (FIG. 7) sensed by sensor 84. A first network 240 having the shown transfer characteristics removes a DC component of signal A caused by the acceleration of gravity and integrates signal A to generate a signal representing absolute velocity at point P (FIG. 7) . A second network 242 provides dynamics to isolate lower vibration frequencies (e.g., below 20 Hz) with desired stability and performance characteristics. Second network 242 can be tuned to the resonant frequency of chassis 4, or to a frequency selected by the operator. A summing circuit 244 sums the output from network 242 with signal D to produce a combined signal representing both the velocity of chassis 4 to be counteracted and the displacement of piston 72. Signal D causes piston 72 to return to a centered steady-state position to prevent the migration of piston 72 to either end of cylinder 70 over time. A gain circuit 246 amplifies the summed signal and applies the amplified signal to PWM interface circuit 226 to generate the valve control signals applied to hydraulic valve 74. Valve 74 responds by selectively supplying and relieving hydraulic fluid to each actuator 68 to cause each piston 72 to move cab 6 relative to chassis 4. Thus, the transmissibility of each isolator 28-32 is defined by the equation: V Q /V J = 1/(1+G) * ((R/M)s + K/M) / (s 2 + (K/M) s + K/M) wherein G is the gain (e.g., 100) of circuit 246 relating input velocity V c of actuator 68 with the velocity at point P, V 0 is the velocity of cab 6 (FIG. 7) , V τ is the velocity of chassis 4 (FIG. 7) , R and K are the damping coefficient and stiffness of elastomeric isolator 97, and M is the mass of cab 6 being supported. The gain G of circuit 246 may be adjusted manually by an input device such as a potentiometer (not shown) , or automatically as described below. Stiffness K s of spring 44 does not affect transmissibility because spring 44 only off-loads the static weight of cab 6 to reduce power consumption. In work vehicle applications wherein air pressure within air springs 44 is actively controlled, ASC 200 generates the control signals applied to the air control valve 206 of each isolator 28-32 to selectively supply and relieve pressurized air to the air bags. The control signals control the air pressure within springs 44 in response to load signals generated by load sensors 144. The pressure within springs 44 is controlled to support the static weight of cab 6 on each isolator 28-32. Thus, changes in weight of cab 6 at each support position are accommodated by changes in pressure within each spring 44. Closed-loop pressure control can be provided using pressure signals from sensors 56 as feedback signals. The control process shown in FIG. 10 and the active control of pressure within springs 44 can be modified to adjust performance parameters of ACS 26. The adjustable parameters include, for example, the gain and frequency response of isolators 28-32, and the gain at which the displacement signal from sensor 132 biases piston 72 to the steady-state position to prevent migration of piston 72 to either end of cylinder 70 over time. The gain of isolators 28-32 is adjusted by changing gain G of circuit 246, or the gain of network 240 or 242 (e.g., gain G . The frequency response is adjusted by modifying the transfer function of network 242. The gain at which piston 72 is biased is adjusted by changing the impact of signal D in the control process of FIG. 10. For example, the impact is changed by adjusting the weight of signal D in the combined signal output by summing circuit 244. As discussed above, the pressure within springs 44 is also an adjustable parameter which can be actively controlled. The primary control inputs for ACS 26 include the acceleration signal A and displacement signal D. The system is set to provide maximum gain without exceeding the stroke of actuators 68. However, the gain may then be adjusted based on secondary or supplemental control inputs such as estimated conditions or signals from other vehicle systems. One supplemental input used to adjust the performance parameters of ACS 26 is the estimated condition of surface 12 forward of vehicle 2. Adaptive or predictive control algorithms respond to the estimated condition to improve performance. For example, the performance parameters may be adjusted based upon the estimated bumpiness of surface 12 ahead of vehicle 2. Bumpiness may be estimated by processing (e.g., taking a root-mean-square of) the signals from bump sensor 34. Alternatively, the bumpiness level can be estimated from the previous level of movement sensed by movement sensor 84 based upon the assumption that surface 12 forward of vehicle 2 will have a similar bumpiness level as surface 12 behind vehicle 2. The bumpiness level can also be estimated based upon the assumptions that vehicle 2 travels quickly on roads and slowly in fields, and that roads are smooth while fields are bumpy. The level is estimated by comparing ground speed of vehicle 2 to a predetermined threshold lo t to o cπ o LΠ LΠ $. CQ 0 0 P to 0 Hi rt cr rt CQ rr μ- cr en LQ CQ μ- to 0 μ- Pi H tr rt CQ CQ μ- μ- O P 0 00 Tl ti tr P tr P tr P Φ φ tr P P ω o Hi P rt Φ φ P O 3 TJ rt cQ P rt 1 Φ Φ Pi CQ φ ti φ co rt <i φ μ- ti o rt <! Hi 3 0 Φ r P rr ^ CO ti Λ rt Φ Hi P ft 0 φ P Hi P ti Φ Φ Φ TJ P 0 Φ P ti Tl to P P ft Hi Pi cr ti Φ P 0 π Φ P t μ- rt φ μ j O rt t > rt φ CQ ti Ω P φ Ω 3 H φ Ω Ω rt 0 CO CO P ^ 21 Φ P ti tr P CQ tr 0 μ- O 0 tJ 0 Φ Φ 3 ti 0 r 0 LQ Φ TJ Pi tr P Φ 0 ^ -, Ω ti < P n ti Ω Ω P Λ TJ rt φ ! Φ Hi ti rt Ω φ to 0 rr rt Φ Ω D P tr cr Φ pi Q 0 μ- α ^ tr C H CQ tr i Φ φ 0 H 0 ti cn P Φ tr P Φ CQ LQ P J μ- P ft Φ to P Φ Φ to P CQ LQ cr φ to 3 O . CO Φ ft tr 3 LQ 0 TJ LQ LQ φ TJ o CQ ii P CO P P rt φ rr Pi C μ- 3 φ 3 rt cr TJ rt P tr φ o μ- φ P rt O μ- CQ ft o μ- 3 P P tr P <-τ o < tr 3 P cr μ- tr μ- P Hi P P CQ μ- ; Q Tl Z P TJ rt Ω P P tr M rr <; P Φ P CO P P Φ φ Ω P ft Ω LQ TJ P 3 rr μ- ≤ P μ- ti O ft Φ Hi 0 Φ J φ 3 Φ μ> ti ft CQ 0 tl φ P 0 α P ti CQ tr co tr ti P P £ φ φ 3 <i Φ CO ft TJ CD o 0 Ω P P CO P rt φ 3 Φ rt Φ ft rt Φ tr P P ft LQ CO rr φ Φ CO μ- CQ rr rt P ti rt rt μ- CQ P Φ CO 0 ^ 0 P O μ- CQ P P tr P rr 0 P P 3 0 O Tl ft μ- Ω iQ φ co ft TJ 0 P rt £ CO Ω Φ I-' cr μ- ti Φ rr Ω μ- Hi TJ Φ TJ T μ- 0 *< 0 P r 0 rt 0 CQ tr tr tr 0 Φ P Hi 0 3 0 CO Φ p; Ω P P P • P P 3 3 cr P tr Ω ^J P Φ μ- μ- μ- £ "< P r 0 P P CQ P CQ <! 0 μ- μ- Pi ω rr μ- 1 P φ P CQ Ω to ti Ω Hi LQ CQ 0 Ω Ω P Hi rt rt P φ . 0 ti Φ rt ti CO ^ P 3 Φ rt P Hi Ω tr P 0 cr ti Φ 3 ti Φ ti rt ti ft Φ ≤ H 0 rt TJ 0 ti tr P φ rt μ- P ft 0 TJ Ω 0 ft Hi tr Φ •» ft Ω ft tr P Hi P μ- 0 • Pi Ω P rt tr P Pi 3 Hi M μ- P P Φ <! μ- w 0 rt μ- ft ti ≤ P Hi Tl CQ Φ rt tr φ rt TJ μ- to P cr CO Ω Φ ≤ μ- P P O Ω Ω Φ φ 0 CQ 0 Φ ti Φ Φ ti μ- μ- μ- rt Ω Φ CO μ- Φ TJ tr LQ P rt 0 tr Tl P 3 O P CQ μ- O H Cfl μ > ti Φ ω o P co μ- tr Q en μ- LQ 0 • μ- tr rt ti P P φ Ω < CQ CQ < tr P to Φ ω P Φ H P CQ LQ P CQ φ 0 Ω rr P P tr rr cr ft o μ- μ- Hi ft Φ P P CO 3 Ω O ft P P to μ- Φ < rt ti ti ft P Φ μ- ft Q Hi μ- P ti ft TI CO P P P P μ j rr O Φ Ω P O φ φ P P μ- Hi P φ μ- ω ω O φ ti X μ- P Φ Φ CO P μ- rt 0 < P P Ω μ- P P rt LQ Ω rt Φ P 0 μ- 1 μ- rr cα ti 0 tr 0 o P P rt • P rt rt P ft Ω Φ o P P μ- ti Φ ft 3 CQ < φ 3 tr Φ rt ti Φ P Φ ≤ Ω rt 0 Ω μ- iQ l_l. ti 3 H μ- Φ φ P 0 rr μ- < P to μ- 0 P Φ CQ ti H- ti <; ti tr Ω < P Φ •6 CO CO P P ft ft ri Φ ft φ 3 *> LQ T) Tl ft <! rt 0 Φ CO H μ- 0 Φ ft CQ P μ- 3 rt P μ- Φ ft φ en tr cr 3 TJ ti φ 0 3 Φ μ- CQ tr Φ P φ rr CQ ti t O 3 rr 1 CO ft CO ^ 0 Φ CQ Hi φ Φ en P < rt <! Φ φ μ- 03 0 P co μ- CQ TJ rt 3 rt CO cr <! μ- CQ Ω rt O CO o to 03 CO Φ ti μ- μ- ft Ω 1 rt ^ rt <; rr tr P cr > ϋ P P P φ φ φ ti < tr Ω Hi O ft 0 tr Ω ti P LO tr ti Φ P P P ^ ^ CO o Ω 3 ft 3 ft P μ- Φ 0 μ- Ω en P ti φ 3 μ- to Φ cr 0 rt Ω P π - tr TJ l_l. Φ rt cr tr ft rt 0 μ- P rt 0 - P P ft ti φ ? ^ Φ Φ ft μ- φ μ- P P rt φ μ- CO μ- ϋ ω P ft tr ti rr to P φ rt 3 Φ 3 rt φ CQ to . rr P CQ rt 0 P α Ω Φ ti 0 ti Φ tr μ- ) P Φ P ti μ- cr TJ φ *. TJ 0 o tr φ rt 0 CO Φ Φ P 0 0 0 03 P Λ CO ^ μ- P rt P 0 P 0 φ H o P CO μ- 0 P cr cr Φ Hi CQ P μ- <; J ≤ P • < P rt ft Ω 0 cr 3 CQ rt P P a rt O P Hi Ω P φ Ω l rr Ω ti P rt Φ P CQ Φ H Tl μ- H 1 rt ii 0 LQ rt 3 to φ 0 0 0 0 μ j μ- <! μ- > <; μ- 1 Φ . Φ H ^ rt Ω Φ O P ≤ Tl Ω P TJ 0 O ti P ti 0 Ω <: 3 φ CQ μ- μ- P Φ μ- P <! P H μ- Φ μ- Φ rt tr P μ- S; pi r ti ft CO H O Φ μ- ti 0 cr rt P Ω CQ CQ rt 0 P Φ TJ CQ CQ CQ < tr pi rt P P μ- Φ ft P N • ; > < ft tr Φ Tl 0 P CQ 0 Φ Φ rt Φ φ CO 0 Φ ft 3 CO rr to μ- rt φ P μ- P ft 0 Φ CQ P to CQ H O O ti CQ P TJ o 03 P ti ft ft rr rr Ω P CQ P tr Ω CQ 03 P - ^Ω μ- ω Q rt 0 1 P 0 0 O tr P tQ O Z ft Φ P rt 1 rt P CQ en Φ μ- P P LO rr μ j Φ ti Φ H rt Φ •* tr P Ω tr LO tr μ- -o > μ- oo 0 P P^ to Φ CO tr Φ ft Φ rt Tl P φ to φ Hi to CO P . 1 LQ ft φ P O cr o LO LO to to H LΠ o LΠ o LΠ o LΠ rt CQ P * Ω Ω ti rt P rr Ω to P Ξ Hi < P ft rr T 0 rt rt P μ- 3 *. r Ω Hi Ω 0 O O μ- CQ 0 P P Φ P tr 0 μ- P μ- μ> Φ Ω μ- μ- 0 TJ 0 Φ Hi P P ^ tr 0 0 tr rt μ- CQ μ- 0 tr μ- CQ ft Φ P 3 φ ΓT P tr rt Hi 3 CO φ CQ rr ft X φ P t cr P tr LQ <l P P ti CQ rr rr μ- < tr μ- μ- P Hi μ- μ- ti ti rt Φ Φ μ- Oi ci ¬ φ CQ Φ P P P LQ ft en φ CQ Tl P ti φ ft Ω P φ P rr P P ω ti TJ 3 P CO ti Φ P CQ ti P μ- 1 μ- CQ 0 rr 0 P P s: rr ti LQ μ- rt μ- — Φ C rr 0 X φ μ- H H < O O P P P Ξ rt P ti tr rt φ 0 φ 0 μ- ω - Ω P 3 P CQ P Hi CQ rt CQ P Φ • φ P rt Ω P Φ μ- Ω μ- 0 ti P P P ^ P φ 0 ft Tl rr CQ 3 μ- 0 CO P rt P ft ti rt ω ii TJ P Ω tr Ω P LQ CT 3 φ ft μ- μ- φ P Tl rt - P CQ CO μ- P cr P μ- Φ ti tr tr Φ ^ Ω φ ft • Ω tr TJ P 0 CQ Ω 3 Ω TJ 0 -J M φ P 0 ft ft LQ CQ 0 P ft O CQ TJ P Φ rt ≤ rt φ Φ 0 P O TJ 3 φ> Λ LQ CQ en rt 0 Φ P TJ tr Pi Ω Ω ti P li 0 tr Φ P O S P - Hi P 0 Φ P P tr ≤ P O rr P tr P rt μ- P w CQ <; rr Ω ≤ P φ O rt ft ti μ- rt i rr tr rt Φ P Pi P Φ rt tr C ti P rr P μ- en Pi μ- 0 Pi CO μ- μ- tr ft Ω ft φ Ξ O μ- tr CO 0 ti P ω CO 3 μ- P O φ Ω rt P P ti LQ P P P 0 Ω μ- ft 0 μ- CQ φ rt α φ rr en Ω μ- rt CQ tr μ- P < Q rt ft 1 tr CQ rt ti 0 P P ti Φ N Tl P P μ- P O P rt Ω μ- O P Φ ti NJ rt μ- ti cr P rt X Φ H Ω P P > 3 TJ rt Ω n μ- 3 Ω i P rt μ- 0 0 P P P ft rt 0 rt ft P o rt CO μ- rt o TJ O Ω φ co P CQ 0 μ- 0 Ω μ- Ω P ti P O P Ω LQ μ- en Φ < Φ Ω 3 μ- rt rt < P CQ rt ^ 0 P 3 rr . — . μ 0 μ- ti Hi rt P P Φ P Ω Φ 3 P Φ μ- TJ Φ μ- ΓT ti 0 CQ TJ LQ TI P Φ P rt φ Φ μ- P TJ P P Ω Ω tr 0 3 P P Oi 0 3 Φ tr CO Ξ P ti rt ~ P Pi • Φ rr μ- ti Φ Ω P P 0 rt rt 0 rt μ- 3 φ P ft $, φ ft Φ tr μ- φ Hi ti rt LQ P ti P rt μ- P ft rt ≤ μ- P P Ω Φ 3 P ft ^ > < μ- Φ P ω ft μ- CQ en 3 P 0 Φ O • Ω 0 Φ ti P tr Φ O Φ P rt rt P μ- 1 P P rt N H rt rt φ P Ω φ CO P ti ft H - tr μ- P P TJ ti li tQ tr ti rt φ Ω P CQ Ω CQ P O ti tr ft . rt ft N rt Ω rt en Φ φ 0 0 tr ft CQ μ- 0 rt rt P ti TJ μ- 0 φ rt en μ- ti CQ P Φ rt tr P en P rt ti P CO μ- LQ P P μ- TJ P Φ ii P P 0 ft P O CD rt Φ μ- rt ti Φ φ μ- ft oo TJ tr CQ TJ TJ LQ P CO rt O - rr P 0 Q li P H TI μ- Ω CO CO LQ μ- O ft μ- co φ φ o 0 TJ μ- P P P rt Φ P Φ Ω cr φ tr H Hi tr 0 TJ P 0 ti P O P Ω Hi en CQ H P P > tr T) Tl φ 0 Hi rt μ- Ω Φ P P P TJ t_l_ rt Hi P ft P 00 μ- rt φ CQ P tr Hi CO 0 φ 0 Hi 0 <1 φ Ω tr Φ Ω P O Tl P ft μ- rt rr Ω 0 CQ r Φ P n Hi μ- 3 ≤ φ s: ti μ- ti 0 Φ μ-> P rt ω CQ O CQ Ω Φ CQ μ- tr P P P CO P μ- P Q CO φ Φ P ft φ P ti rr μ- O P μ- ≤ rt O P TJ TJ O Φ ti rt μ- P Tl 0 LQ Ω to Ω 0 ^ ti rr ti P φ P rt ti Φ <! Ω LQ Ω rt Φ P Ω 0 P Φ μ- 3 CO T ti tr rt o P ft Ω ri P P ti φ P μ- rt μ- ti CQ rt tr 3 P CQ ft 0 t P rt μ- o tr P ft r P 0 TJ Φ 0 Ω μ- Φ P Ω P O P ti φ Ω μ- Ω P Ω μ- r- 1 0 r CO O • <; TJ 3 ti CQ rr Q ft Tl CQ P P ft TJ O μ- ti Φ 0 CO 0 CQ Hi r Φ Φ ≤ P TJ en 0 n £ φ P φ μ- φ ^ - ^ rr CO O TJ CQ 3 Hi TJ 0 ti P 0 ft <! tr CO Φ ti P rt Ω rt CO μ- Φ P O CQ Φ 0 — - ≤ O O φ ti 0 P CQ φ μ- . ti to tr P μ- Q P ti rt Ω rr rt φ • ti • P ti φ 0 P μ- P P ^ rr 3 Φ Φ r Hi P to o 0 Φ P 3 P 0 Pi Φ 0 P LQ r H Pi s rr CQ Ω μ- tr 0 0 φ 0 H 03 o Hi CQ μ- li rt rt ti tr P P Ω . Ω TJ Φ • rt P CQ 0 Φ P Φ μ- P P ι-3 ti μ- 0 Φ P μ- μ- 0 ω tr - o t-3 0 ft O 3 P rt CO <! rt 3 tr 3 P LO Ω < Tl CQ LQ N 3 en ^ -j P tr CQ ti o Ω P Φ r < CQ 0 P rt P φ co cQ t 0 Φ Φ Φ μ- Φ en to P cr rr φ μ- cr > Hi P rt P Φ P ^ 0 μ- μ- P 0 tr ti ι_l. P ft P P 03 CQ Ω P ti P rt ^ rt to P 0 rr ft Tl TJ <! rt P cr TI rt ti μ- P Φ P Q rt μ- rr ti rt μ- 0 μ- 03 < ti CQ < 0 P φ P rt P 0 O ft Ω rt ti ft tr Φ ft rt P Φ P O CO TJ Φ cr Q φ £ TJ Hi CO ft P μ- ≤ μ- O ? ^ Hi ti P tr rt P P rt P P J O UJ tr Φ cr μ- Φ TJ φ Φ μ- CO φ Ω P φ ϋ μ- ti ft o φ Φ Ω rt ω O ti ≤ to μ- to Φ rt Ω H φ -J P n rt ti 0 P . P P li li μ- ii tr 0 μ- 0 μ- Φ Ω CQ 03 rt tr O μ- ft £> tr μ- 1 P rt t LQ rt P r cr P Φ ti P 0 Φ ^ P ti μ- Φ £ P ft φ cr ^ P to μ- P rt Φ . Φ P rt O 0 P CQ Tl P Φ Q 1 CQ φ Φ U) Φ φ rt 0 ft i P LQ o P TJ li CQ > P CQ μ-" tr en Ω CQ CO £ P to Φ P ti ≤ Ω P o 0 P μ- Φ o P 03 tr • TJ to - • P Ω O P ?r ft ft Ω 3 P • tr position to its steady-state position at a predetermined rate. The rate can be fixed, or can be manually set by cab rate command device 232. To insure availability of sufficient hydraulic power to each isolator 28-32, ASC 200 delays extending pistons 72 until a sufficient time has passed following power-up. Alternatively, ASC 200 can monitor the displacement of each isolator 28-32 and set the command signals to extend pistons 72 no faster than the movement of the slowest isolator 28-32. Thus, no isolator is raised faster than another isolator which may lag due to insufficient hydraulic power. Closed-loop displacement control is also performed during power-down. In one embodiment, ASC 200 includes control logic which prevents cab 6 from being actively moved relative to chassis 4 when vehicle 2 is not moving (i.e., ground velocity less than a predetermined speed threshold) or when an operator-presence sensor indicates the operator is not present. For example, ASC 200 does not raise cab 6 to its steady-state height until vehicle speed exceeds a threshold. Gating the valve control signals with movement of vehicle 2 prevents the unexpected movement of cab 6 when a person outside cab 6 is nearby. Vehicle speed can be sensed using sensor 338 (FIG. 12) . Another benefit of coordinating the displacements is the ability to control the attitude of cab 6, either with respect to the horizontal (i.e., horizon) or with respect to chassis 4. For example, to maintain a level attitude of cab 6 with respect to chassis 4, displacement signals from each sensor 132 can be combined (e.g., averaged) and the combined signal used as the steady-state displacement control parameter (e.g., D in FIG. 10) . Further, if work vehicle 2 is equipped with leveling sensor 36, the steady-state displacement control parameter can depend on the signal from sensor 36 to maintain a level attitude of cab 6 with respect to the horizontal. For example, if a sensed signal indicates that the front of cab 6 is LO LO to to μ> LΠ o LΠ o LΠ o LΠ 0 Φ m en Ξ lfc» > 3 CO ft < φ tr 3 to Φ O ζ O Ω Ω 3 to P ti Tl 3 •-3 P LO LO rt H X 0 03 Φ .ϋ CQ μ- μ- Φ P pi P P oo X Hi H- < μ j 0 μ- u> Φ 0 Oi tr NJ O μ- P μ- rt LQ rr Ω < 1 TJ rr Φ φ 3 P φ» ω rt P ^ ft Φ l_J. CQ M Φ P iQ Ω tr Φ P tr Φ u> Hi tr ti Pi 3 μ- • 0 Oi rt Φ P ft Ω rt rt TJ <! ti tr P Φ P ti φ to P 0 tr ti P 3 μ- μ- Ω CQ Φ P μ- 0 Φ Φ rt P CQ φ H 3 CQ μ- ft tr μ- i Φ H i i P C cr H P O rt tr rt Ω P P ti φ ti Ω P CQ P μ- CQ μ- 0 3 P Ω P tr P P ft 3 >τ| Φ tr CQ P O P 3 ti CQ P - - P 0 cr li o P tr 0 Hi *, Pi Φ Φ Ω Φ LQ Ω C Φ P Φ Φ cr tQ tr Hi Φ μ- tr P CQ φ ■ ^ Hi Φ ► ft tr — φ ft H P rt O Ω LQ P P Φ ft Φ Ω rt μ j tr TJ 0 α ~ P Φ <! tr < • Φ Φ rt CQ tr Hi O Φ rr CQ O tr tr φ Ω P φ o TJ 3 rt ti φ cr P Φ o P H <j < tr l_J. rt Φ P CO CQ Φ μ- £ 0 Pi Φ P Ω rt Φ TJ Hi O Φ ti Φ tr rt rt μ j φ μ- Φ Φ P Φ rr rt ft P P ti P r cr rt tr μ- P 0 ti P - 0 ≤ tr < Λ Ω ti CQ P P tr ti r Ω Ω s- LQ rr 0 μ- Oi Φ Φ ≤ ti ti rt P < Φ φ φ P Φ - ft ft cr φ O O P rt ti P ti φ O en < cr ti ft o P to cr ft Φ Φ ti μ- μ- Φ ^ μ- μ j P O Φ ti Φ CQ rt 3 φ 0 ti 3 Φ 00 TJ Φ ι_ι. - P o ti to P rt ft 1 O rt P ft 3 P o 0 < rt rt ?r φ X 1 P P rt 0 φ U) tr CQ μ- rt rt tr tr I- 1 CQ 0 μ- μ j < P *< Φ 0 0 rt Pi co ti P CQ rr Ω O P ft en ii Φ 3 rt rt ti tr φ Φ φ Φ < P Φ < φ 3 to P P ft tr P rt Φ P P ^ O φ <! ft ft P ≤ Φ Ω Ω P φ ti TJ 3 ft Φ φ tr Ω ti Hi ^ ~, CO tr P rt ? CO 3 φ tr Φ Ω P 0 rt O μ- tr 3 φ Φ ft O O O Hi TJ Φ P Φ rt Φ P rt P μ j P φ Φ μ- P Ω P tr 0 r μ- <^ Φ P rr CO TJ en O h o 0 μ- P O rt φ ft P o μ- LQ tr tr rt φ ti Ω P - ^ φ μ- ft φ i H P LQ μ j tr 0 ft P φ rt ft ft Hi LQ tr ti ft Ω μ^ ti ti P ti P ft CQ <! CQ tr Φ TI Hi μ- ft tr μ- tr rt en μ- O P μ- 0 φ P P tr P ti Hi P μ- μ- Φ Φ Φ rt *< μ- ti tt ^ 5 > φ rt CQ 0 rt CQ μ- P P Φ < Φ <! cr μ- 0 ft P LQ tr X LQ O Tl P 1 tr tr TJ cr 0 £ 0 μ j ti Pi rt P CQ φ P P ti P P μ- P rt 0 P tr < μ- ft CQ Φ P Φ μ j t_l. O Hi μ- μ* φ r ti TJ ti P Φ LQ 3 Ω rt P Ω 3 0 Hi CO rt μ- CQ Φ rt P rt P φ Hi rt P ft TJ Φ 0 TJ Hi P ft P P tr Φ j Tl μ- ft rt P rt ft Ω Ω Ω tr rr ti μ j 0 U3 ι_ι. φ Hi O P P CQ Φ P Ω P 0 φ O O rt Ω H- μ- Φ rt rr P 0 rt Φ Ω μ- ti μ- P CQ 0 TJ Ω CO rt φ P P CQ Hi P Hi φ P rr CO 3 CO tr cr 3 ti 0 CO O < Ω P CQ • ti Φ φ to tr 3 to - tr <J tr P TJ φ Φ μ- CQ P Pi P φ LQ rt ti μ- Φ P P Ω Ω μ- ^j Ω ft ft P .—, en P to 1_1. P rt rt P Φ Φ P TJ ω ^ rt rt Ω en P P cr to P μ- en Φ P rt Φ o μ- oo P ti ti < μ- Ω rt ft H P rt P P O O rt cr tr ii cr co Ω • TJ 3 3 1 O Φ O Φ 0 tr tr tr Ω μ- ti ^ rt P P Ω P ω TJ μ- O Φ 0 LQ φ P P LO rt CO P φ ΓT P tr O P • rt μ j Tl ft P P tr CΛ rt P en o Hi 3 Hi H *<: μ- 1 to ≤ CQ μ- O CO P 3 Φ to P Φ rt P Φ μ- Ω P Φ ^ P CQ μ- 0 to ^ co μ- ^ μ- Φ P O CO Ω μ- μ- P O tr P Ω rt Ω P Hi rt Ω TI CQ P rt Hi O 0 P rt CQ O rr rci P O ti 0 cr iQ tr P ti Φ μ- P rt ti rt 0 tr 0 0 TJ tr CΛ ft μ j tr rr 0 Hi Φ O P cr Φ P Φ tr 0 rt Φ 3 cr O 0 ti P ≤ TJ μ- P tr P μ- Φ tr μ- 1 ti H rt φ tr P rt < μ- tr φ rt 0 P 0 P Φ r 0 P μ- P φ rr < φ P <! ω Φ Φ CQ 0 μ j Φ CO P P μ- CΛ Hi rt μ j 0 LQ ti tr ti ti ti 0 μ- CO rt Φ Φ P- Ω P Φ Hi 0 Ω 0 rt μ- rr P • ω ti Φ P rt φ Φ Ω H ft P Tl O tr O X 0 Φ $. 0 Ω 3 CQ Q ti μ- — Ω rt P CQ 0 P 3 P ti μ- Hi P rt 0 P ft Φ 3 tr P Tl μ- Φ CQ • 0 ft o rr Ω Tl Ω P t P Φ ti Ω 3 ti ti rr tr 0 •i 3 P rr μ- rr ft ω O P O Tl P P P tr " ti 0 rr 03 P to μ- Tl P ft tr Φ ≤ Φ P CQ μ- co φ tr μ- μ- ti μ j Φ Φ to Ω φ μ- O 1 TJ 3 00 φ co j P μ- Φ ft P CO O r ft P ft ft P rr} ti P rt CQ P ti 0 UI ^ P Φ 1 O φ O P P ti ft μ- P O rt φ φ μ- rt P P rt 3 P CQ TJ LQ ft t 1 ti rr LO t - 3 P P rt CQ • P rr ^ ≤ co O ti rt 0 TJ Pi rt ti O μ- • P Φ to • P μ- rt 0 ft O P P P 0 ti rt 0 - rt rr P μ- P 3 ti rt P cα φ Φ Φ» -j H > ^ μ j CQ tr ti μ- O r P tP> P Φ CO rr O ω CQ ft P <! to P Φ CQ CQ P φ Co Hi 0 ti μ- cQ φ> rt rt O H ti μ- μ- Ω • rt to ti ** 0 P CO Ω • Φ Φ O rt CO O Ω P O 00 ti ft ti Hi P Φ P ti 1 U) to to LΠ o LΠ o LΠ LΠ μ- rt o Ω P μ- 3 P Hi rt 0 . — . CQ z tr H Hi 0 ^ Hi r CQ tr P^ φ Z S rt r 0 0 Z φ 0 P tr — P ti CQ 0 rt 0 tr Hi z rr μ- Φ tr ti Hi 0 0 tr μ- •<; P X μ- μ- tr tr ti Hi Φ < P P φ cr Φ 0 rr < ti φ tr Φ Φ 0 ti ti Φ LQ Φ rt μ j rt Φ φ μ- φ ft Ω φ TJ Ω Φ μ- Φ -> CQ P to 3 P CO ti μ j tr μ- O LQ P Ω P 0 en P P 3 0 φ CQ P Ω TJ φ P rt O φ P rt P φ rt P 0 Z Z cα P tr Hi P cr Ω ft n φ z Φ Ω tr cr rr μ- O X 0 j P 0 n P P φ φ ti rr Oi 0 li CQ μ- ,— Ω 0 tr P φ μ- P tr LQ Φ ti μ- O P P rt CO CQ tr Ti 0 rt μ- μ- 3 Hi CQ ti P 0 CQ ft O ti P rr ti o CO Z ti rt ω 3 P μ- P P 0 LQ iQ 0 P O CQ Ω rt H 0 Φ 3 P CO 1 φ μ- 0 P ft 0 J 0 TJ TJ cr rt P P Z P tr tr <^ Ω Hi P Φ φ P μ- 1 rt 3 ft LQ 0 ) ft CO P ft μ- H 0 P 0 LQ Ω LQ Φ 0 r rt μ- Φ rr 3 P Φ 0 P Φ O P ri O Φ co CO φ P P Φ CQ tr Φ ti P CJ. P Ω μ- Ω Z Φ rt ti ft Φ CO Hi φ ft rt P CO (t P •* Φ 0 ft P O LQ P CQ CO LQ H P P P tr 0 3 P 0 Hi 0 P Z ii TJ CO 0 ft ft P φ o P rr Φ CO P P to cr tQ P Φ ti μ- rt rt μ- Ω Φ P rt Ω tr μ- TJ P ti Co μ- ft rt P LQ μ- 0 ti rt Tl TJ - P 0 O P Φ 0 P P ti ft O P Φ cr 0 i Hi P φ ft Φ P 3 TJ TJ en P cr P φ ft tr Z P H P P P li Φ t TJ Hi ti Ω tr Φ 0 0 Α ti Φ < ft to ft Ω rt tr cr Hi CO rt rt 00 > rt 0 o 3 Hi μ- H" O Φ P ti ii o φ 0 Ω Φ oo cr tr tr en φ 0 t φ rt Φ μ- 1 CO 0 P ti μ- 0 P 0 P rt rt rt ti CQ P 0 ft tr CQ 1 0 • <; P Φ P ^ ti 03 tr ft rt P LO o rt Ω P ti P P Ω •• Φ Φ P P μ- μ- μ- LO P P Hi Ω 1 μ- φ tr o Pi rt Φ Φ Ω rt ft rt 0 P- ft Φ ti μ- CQ CQ Ω LQ to ft LQ ti ti <! CQ Φ LO P Ω φ rt to tr Φ o Φ ti rt X ft CQ rt rt -> P TJ μ- φ Φ 0 Φ Φ t Ω 3 0 CO tr pi o Φ P P ft Hi ti ti tr σ tr P H 0 P ti φ P μ- 0 CO CQ 3 tr P 0 0 φ ti φ φ P o 3 0 P o P Φ φ ^ ^ 3 φ P μ- P Z rt P μ- CQ Hi Z li P ti 0 Ω 0 rt P ti Ω Ω TJ CQ P rt cr to CO Φ t μ- ft P Ω Φ P ti CQ Φ Ξ ti 3 P o P o Ω rt rt P P P CQ rt P 0 ti μ- P μ- Hi ft rt CQ Φ P Ω φ Φ M Pi ft P LQ rr Φ z Φ •» μ- P Φ 0 rt rt μ- Q P 1 tr < Hi φ tr Ω ϋ rt μ- CQ o ► <; Hi P P φ rt ti p. - O ti O Φ CQ φ Φ 0 P CQ φ Φ Z P CO rt φ LQ J o Hi μ- μ- μ j Ω μ- Φ tr P P 0 Hi CO rt ft P P rt ti Ω <; tr rt Φ 3 ^ tr φ o P O LQ CQ tr LQ X Φ P Tl ) z z P 3 Φ 0 μ- 0 Z rt Φ φ ft li φ rt Ω rr ti P O tr Φ ft ti z P tr z t P o ti Hi 0 P P Φ μ- P μ- Φ P Φ CO rt J rr Ω H 0 μ- rt ti Ω Φ P z Φ tr 03 3 < P ti LQ P μ- P 0 CO μ- O rt < μ- 0 ti Φ P P P co rt tr P CQ ti P P φ 1 Ω O μ- rt (t ft LQ Q Ω <! 0 P P CO Φ ! P μ- ft rt ft 0 0 Φ P Ω CQ ft li rr LO P P P φ Z Z rt tr μ- Φ ft P Φ P r Ω μ- 0 Hi ft P ft P ft < tr to cr LQ LQ ft 0 tr tr CQ rt rt rt tr P Φ rt 0 ] ft P 0 0 H Hi P tQ P ti μ- Φ φ Φ φ μ j tr ^ μ- rt TJ co Hi μ- tr ω CO rt ti P CO o r Ω 0 Φ P Φ ω μ- tr ti ft z μ- — - tr 3 P o 0 φ Ω 0 φ Hi P TJ Φ ti ti O P P ft ft 0 CQ μ- φ φ CO ^ P rt Tl Hi μ- ^ P μ- I— 1 ω ϋ rt Φ O to Ω ti cr 0 μ- O Ω < TJ μ- 0 P <J 0 φ CO ω φ ft Hi 0 < - μ- 0 LΠ CO Hi oo Φ Φ Φ ti P P Φ φ LQ f ή CQ P Φ ft Ω φ • φ P φ P o Tl 1 - to en P Hi ft P φ tr P tr P ) μ- φ φ tr Pi p. P P o t P rr p. tr rt LQ ti o 0 μ- U) 03 Ω Hi en Φ 0 ft μ- rr rt ti P ti μ- μ j P cr O — rt tr μ- tr CO Φ P CQ to P 1 P tr Φ 00 Oi ti o to Ω CQ - O co CQ CQ Ω ti φ μ- μ] μ j φ Hi Ω φ Pi J P. 0 P LO ti Ω Ω ti j ti rt 0 • μ- en ft rt CO 0 • <: O *» ti O CQ P ft to Φ μ- rt Z tr ft μ- φ 0 rt CQ ri φ 0 P 0 rr P ti Φ ^ P P CQ - CQ μ- μ- Φ μ- ω P tr CQ P LQ 0 CQ CO P cr μ- Ω 0 μ- P rt rt μ- ft P 0 <! μ j CO Ω P to Φ to rt ^ -, <! P μ- ) rt pi ti Φ to Pi Z CQ P. 0 0 P μ- CO Ω μ j φ TJ ti Ω 0 ft 00 tr M 2 φ 0 LQ ti μ- CO ft 0 0 CO H LQ co P Ω P ti Φ H P μ- p- ti 1 Φ »P> 0 Hi Tl Φ P Φ φ J P μ- P μ j P CQ rt 3 0 rt Z Ω μ- P Φ co φ Φ LO Φ> rr 0 o Φ P P <; j O ft ti ti co Hi μ- 1 P rt P ti 3 3 0 φ 0 P CO P 0 ) μ j to rt Φ Ω ti ti Ω Φ P Φ Φ o P. rt 0 z to μ- μ- 3 ti μ- P LQ Φ ω CO CO P O 3 μ- Ω P tr CQ P ,-. ft P CQ 0 ti O φ 03 *- cr P 0 LQ CO CO φ CO rt rr cr ft P rt rt φ rt • rt Φ . TJ CO rr P Ω rt ti Φ μ- I P P LQ ft t tr P φ. • CQ μ- 0 μ- P P ^ tr ^ μ- o P P Φ tr P LQ LO 0 rt P oo rt 3 ^ 0 TJ < CQ P 0 0 iQ P ii P CQ Φ LO Ω tr to z H- rt rt 1 • φ P TJ φ φ Φ σ rt μ- Hi P . Φ Φ P to tr rt . P P tr Φ LO P φ ft Φ Q ~ P • LQ Φ ft to ft "• ω LO to to μ» LΠ o LΠ o LΠ LΠ Ω rt Ω CO P Ω P 0 0 O CQ CQ μ- Ω Ω P CQ cr Φ Ω ft μ- μ- rt Z CQ CO Oi ft •ri 0 0 tr 0 μ- 0 P rt rt ^ μ- P P 0 P ) ^ P < tr μ- μ- co co tr P P φ P tr O P P Φ 3 Q TJ P tr tr CQ LQ TJ T P tr J CQ CQ Φ Oi co CQ 0 0 Φ CQ 3 Ω φ ϋ CQ CO 3 P 0 CQ P φ φ ft P TJ P rt rt - P P rt rt 3 O rt 0 Φ P P co 0 ti ti ti Φ P rt ti en μ- Φ LQ ti ti P Oi ti CQ Φ P rt P Φ tr P μ- H 3 3 to μ Φ O φ 3 > S Z φ μ- μ] μ- rt rt φ rt ft ft tr μ- X Φ Φ Ω ft CO rt Φ ti <! < φ CO 3 CQ μ- 1 ft CO π tr tr CQ tr tr tr 0 0 μ j μ- Φ ti Oi 0 μ- Φ μ- φ to l-h Φ μ- P CO Φ Φ P P P li ti P P 3 P z 3 ft ti 0 μ- CQ P tr LΠ φ ϋ P iQ 0 Φ 0 tr P P μ- rt to rt rt M P rr Oi TJ TJ rr tr 3 Φ φ P P rt μ- o ti φ rt P Hi ti P to P Φ φ to CO μ- — ft tr μ- ii rt φ P <; Tl μ- TJ tr Ω ti 3 P P rt < en z < ft 00 <! φ ti Φ φ μ- ti P μ- ti P P Ω P CO μ- P μ- 1 μ- O P μ- o Φ Z rt cr 1 φ ft rt CO ^ rt φ ft Ω Φ LQ rt 0 O Φ tr P μ- CO CQ ti P Ω t tr Φ tr ^ LO 0 μ- tr μ j TJ CQ P Φ CO P 0 LQ P μ- O CQ Φ LQ 0 r μ- μ- φ o to P Ω CQ Φ 0 ti P μ- ft rt ft O Φ Ω ft CQ to Ω Z P Hi P 3 Ω LQ Ω P ft 0 rt P Φ ti Hi Φ tr Φ P 0 Φ 0 o O CQ rt rt T) ti P Ω tr TJ 3 <! tr rt O ft P P ti rt ft CQ Φ Φ <! to rt P <! oo P 0 tr P 0 rt tr Φ Oi P φ Φ rt 0 0 ti CO rt μ- 0 CQ rt O ^ μ- LO μ- r μ- φ • rt <! Φ rt 3 0 μ- ti P tr rt ti Hi Φ μ- ti cr ft CQ P μ- tr Hi Ω to P ti Ω ti φ r} CQ ti Hi P P μ- μ- t 0 P ft 0 LQ μ- P P μ- ti P φ P Φ 1 CQ 0 Φ Ω o tr H TI CQ CO o LQ 3 Ω o Hi μ- ti rt P r rt cQ Φ Ω ti CQ to CQ 0 < μ- Ω ti Hi P H Φ P μ- P Ω tr P P Φ P Hi Hi P φ LO P φ Ω • μ- 0 Ω to Ω P rt rt φ co Ω P Φ φ rt μ- 1 P μ- ti ti tr 3 00 0 O to rt tr CO 3 ti tr 00 Φ TJ Φ Φ P 0 rt • P • μ- o P 0 o ti P Ω ^ LΠ H μ- "< φ H P 1 CQ T ti ω to 0 tr P μ- O rt P CO P P σ> Φ • ; P P O Φ> 0 Ω CO H ti > 0 CO CO P ft P LQ P O ft ti rt rt P ti ft rt ft t ^ n rr to μ- μ- μ- CΛ LQ φ t-3 Hi Φ Q ft P Φ μ- Φ rt Φ φ CO tr O φ ti μ- ra P P tr rt Φ Hi ti P μ- O Φ * 0 3 O CQ 3 Φ P Ω Φ P ft Φ Oi P 0 rt Φ φ 0 P 0 0 ti CQ Hi P tr Q Z P ^ Ω CO Λ P 0 t ti O P μ j φ CQ ti ti tr ti Ω ti 3 O CO > < 0 μ- CO t ti ω o P P en rt rt Oi rt Λ Φ Ω φ P P rt tr Ω μ- Ω φ ti LΠ Φ rt P μ- μ- φ rt ^ < φ rt O rt tr P O Φ rt μ- tr Φ μ- CQ P P ft Ω tr Φ 0 en Ω φ rt P TJ X ϋ φ X Φ Φ Φ μ- Tl P P Φ ti Φ μ- CQ 0 rt r o Φ ft Hi φ 3 ii TJ φ O P tr Tl P < ft TJ φ Ω P μ- ft ω . — . o 0 tr P rt μ- O Ω Φ 3 P μ- P Φ tr TJ ft Ω 3 ii Ω CO 0 3 P li en ^ rt rt 0 < to O ft •tj ft Ω P P tr rt P φ O 0 cr O P φ P rt CQ ti 0 O Φ Φ LΠ 3 μ- μ- ft μ- 0 CQ ft CQ 3 P Ω P P 3 P P ft 0 μ- O Ω tr ti to CO 3 Z P P rt Φ P φ Ω P 3 LQ O O rt 3 rt CQ o ti to co Φ P > μ- φ Ω "< P μ- ti J tr Φ Hi ii φ o P 03 <! rt z Z ti 0 P φ CO Ω Ω o Ω CO P <t ^ P Φ CO ft Φ O μ- μ- Hi ft μ- rt ft O ft ti CQ UJ 1 rt Φ CQ Φ π φ 3 0 (t μ- tr rt ^ tr ti rt rt P P CQ ti (-• Φ t UJ μ- ^ ft Φ μ- 3 P φ Ω CQ P CQ cr ^ to Ω tr tr Ω rr 0 O P to to ft to o μ- CQ to <; Oi TJ 3 P > Φ • Ω ft φ • Φ Φ Φ TJ CO μ- 00 oo μ- rr P rt μ- o to φ P rt CO tr Ω φ P CQ 0 P α P 0 μ- LQ 1 Z 1 co μ- Φ cQ Φ P o . ft Φ t μ- n μ- Φ 3 o Tl rt O rt CQ P LQ P ω tr UJ CQ ft 3 TJ ft LΠ O Ω CQ z TJ 2 z tr <! ti P 0 μ- P P to φ t ft ω rt μ- 0 O o P to φ ti O tr Φ Φ Ω ti LQ rt P P φ μ- ft Φ to tr P > Q μ- rt o Φ ti P 0 < μ- ti P ^ 3 Ω CO P tr σ Ω Ω P 0 P LΠ φ μ- LQ 0 μ- Z o P t TJ Φ Ω μ- O P P φ CO o P <! P ti Ω z CQ to ^ rt rt P P μ- Ω rt φ n ti 3 tr <! Ω <! ti to Hi CQ φ P Φ ti P . o P H tr μ- P P Ω rr P 0 μ- o μ- Φ Φ μ- 1 μ- P 00 CQ Hi φ tr P φ z ti ti Ω 0 0 ti tr P P O P P P Z tr φ P rt 1 o rt ft μ- cr CQ P P 3 P P CO 3 P ft rt P rt rt rt μ- μ- LQ Φ U) rt ti tr Ω Φ φ CO ti LO ti CQ μ- ^ ti ft φ ti ii Φ Ω ft • to 0 P P i Φ ft en Φ vo tr P φ Φ P z O 0 O μ< P ^ Φ rt TJ φ • ft • CO ^ LQ P CO CO Ω μ- Hi φ rt P o rt P rt tr rt cr P Ω P to tr φ tr Control system 250 includes other vehicle systems having parameters related to forces applied to vehicle 10. For example, control system 250 may include a tool height control system 258, a steering control system 260, a four-wheel drive/differential lock (4WD/DL) control system 262, and a transmission and speed control system 264. Each system 258-264 includes input devices 266 to generate command signals and output interfaces 268 to control output actuators. Vehicle 2 may be equipped with any or all of these systems (e.g., a tractor equipped with tool height control system 258 may not have an armrest control console coupled to bus 208) . Vehicle 2 may also include other vehicle systems having parameters related to forces applied to vehicle 2. Communication of parameters related to forces applied to vehicle 2 across bus 208 gives ASC 200 access to such parameters without the need for separate sensors dedicated to ACS 26. In one embodiment, tool height control system 258 is installed on a tractor equipped with a hitch assembly to raise and lower a tool (e.g., implement or plow) . Input devices 266 include draft force and position command devices used by control system 258 to generate control signals applied to an actuator to raise and lower the tool. Sensors provide draft force and position feedback signals. The command signals generated by input devices 266 are indicative of draft forces which will be applied to the tractor, and the feedback signals are indicative of draft forces currently being applied to the tractor. Thus, the command signals and feedback signals are both related to draft forces applied to the tractor. A hitch assembly control system for a tractor having the above components is described in U.S. Pat. No. 5,421,416. In another embodiment, tool height control system 258 is installed on a combine equipped with a positioning assembly which raises and lowers a header. A header control system for a combine is described in U.S. Pat. No. 5,455,769. The '416 and '769 patents are commonly assigned and herein incorporated by reference. Steering control system 260 includes a steering input device 266 (e.g., steering wheel 20) coupled to a sensor (e.g., sensor 38) which generates steering angle command signals indicating the degree of turning. A feedback sensor can be used to measure actual turning. The sensed signals are indicative of the normal forces applied to vehicle 10 due to turning since steering angle is a measure of turning radius, and normal force equals velocity squared divided by radius . Velocity is sensed by a ground speed sensor such as sensor 338. A steering control system is disclosed in U.S. Pat. No. 5,194,851, commonly assigned and herein incorporated by reference. An exemplary 4WD/DL control system 262 is described in U.S. Pat. No. 5,505,267, commonly assigned and herein incorporated by reference. Control system 262 includes 4WD/DL input devices 266 and output interfaces 268, and has parameters indicative of command and output signals for a 4WD clutch and DL lock related to forces applied to vehicle 2 as 4WD is engaged and disengaged and DL is locked and unlocked. The '267 patent further discloses brake detecting circuits (e.g., circuits 39) coupled to the brakes (e.g., brakes 24) of a vehicle to generate signals representing the state of the brakes and, thus, whether braking forces are being applied to vehicle 2. An exemplary transmission/speed control system 264 is described in U.S. Pat. No. 5,233,525, also commonly assigned and incorporated herein by reference. Control system 264 includes gear shift and speed input devices 266 and output interfaces 268. Control system 264 has parameters indicative of commanded and output gear shift signals of a transmission, and commanded and output speed actuator settings. These parameters are related to the forces applied to vehicle 2 as the transmission upshifts and downshifts and vehicle 2 accelerates and decelerates. ASC 200 has access via bus 208 to parameters of the other systems shown in FIG. 11 related to forces applied to vehicle 2 during operation of those systems. ASC 200 uses the parameters as supplemental control inputs when generating control signals for isolators 28-32 to attenuate movement of cab 6 due to such forces . For example, if a parameter indicates that a pitch or normal force is about to be applied to vehicle 2 control signals applied to isolators 28-32 will prevent the operator from being thrown backwards or sideways. The gain parameter can also be adjusted when such forces are predicted. Further, the attitude of cab 6 can be changed to improve ride quality in response to such forces (e.g., by tilting cab 6 into a turn, or tilting cab 6 in the fore-and-aft direction in response to a pitch force) . In addition, the force parameters from other vehicle systems can be used by ACS 26 as preparatory signals. For example, ACS 26 could bias the oil supply to the isolator 28-32 which will require the most oil flow when the force actually impacts cab 6. Adaptive or predictive control algorithms can use the parameters to predict movement of cab 6 caused by the forces. Fuzzy logic control algorithms may also be used to generate control signals in response to the force parameters to provide improved ride quality. Empirical testing may be used to determine the control algorithms . Referring to FIG. 12, positioning control system 258 includes a positioning control circuit (PCC) 300 for receiving, processing and communicating site-specific data. PCC 300 is coupled to an interface circuit 302 for communicating across bus 208. PCC 300 also communicates with external systems such as a computer 304 via a memory card 306 which transfers geo-referenced maps including spatially-variable map data indicative of fields, roads and the bumpiness thereof. Card 306 can be a Type II PCMCIA card made by Centennial Technologies, Inc. PCC 300 includes a digital processor and memory. However, dedicated, specific purpose equipment or hard-wired logic circuitry can also be used. PCC 300 communicates with an operator through a user interface 308 via a bus 310 (e.g., RS-232/485 interface). Interface 308 can include, for example, a graphical user interface 312 providing cursor control (e.g., a mouse, joystick or four-way switch) , assignable switches 314 (e.g., push buttons) configurable by PCC 300, a keyboard 316 and a voice interface 318. PCC 300 generates display signals applied to a reconfigurable display 320 (e.g., CRT, flat screen active-matrix LCD) via a bus 322. Display 320 can display, inter alia, the configuration of switches 314. User interface 308 and display 320 are located in cab 14 for easy operator access. PCC 300 may communicate with a printer 324 via an interface 326 (e.g., an RS-232 link). PCC 300 also communicates with a location signal generation circuit 328 which generates location signals representing the positions of vehicle 2. Circuit 328 includes a global positioning system (GPS) receiver 330 with an associated antenna 332, and a differential GPS (DGPS) receiver 334 with an associated antenna 336. A single antenna may be used in place of antennas 332 and 336. GPS receiver 330 may be made by Trimble Navigation Ltd. of California, and DGPS receiver 334 may be made by Satloc, Inc. of Arizona. GPS receiver 330 determines longitude and latitude coordinates (and altitude) of the vehicle from signals transmitted by the GPS satellite network. Accuracy of the position data is improved by applying correction signals received by DGPS receiver 334. In one embodiment, PCC 300 interfaces with the SATLOC L-Band Integrated TerraStar DGPS System via an RS- 485 link. PCC 300 receives signals representing the ground speed of vehicle 2 from ground speed sensor 338 via interface 340 (e.g., a frequency interface). Ground speed sensor 338 preferably includes a radar device mounted to the body of vehicle 2. However, sensor 338 may also include a magnetic pickup sensor configured to sense the speed of the vehicle's wheels or transmission. Referring to FIG. 13, bumpiness level data used to adjust the performance parameters of ACS 26 may also be determined using vehicle position as an index to geo- referenced maps of surface 12. For example, PCC 300 is provided with predetermined geo-referenced maps or data layers 350 stored on memory card 306. Map 350 is represented by a table wherein rows represent field locations and columns represent the longitude and latitude coordinates, altitude and the bumpiness level for each location. In one embodiment, bumpiness levels are represented using discrete numbers (e.g., level 1 = a relatively smooth surface, level 2 = a medium surface, level 3 = relatively bumpy surface) . Other levels may also be defined and real numbers may be used. For example, data point no. 3 indicates that the altitude is 801.0 feet and the surface is relatively smooth at the location defined by latitude and longitude coordinates - 88.7290720 and 39.0710740, respectively. Map 350 is preferably implemented using a geographical information systems (GIS) database stored as a DOS file on card 306. Referring to FIG. 14, a predetermined geo-referenced map 350 of a road 352 and a field 354 which includes bumpiness level data is represented graphically. Road 352 is labeled bumpiness level 1 since it is relatively smooth. One area of field 354 is labeled level 2 since it has medium bumpiness, while a second area 358 of field 354 (i.e., area within the polygon) is labeled as level 3 since it is relatively bumpy. The bumpiness level data stored in map 350 may have been generating during a previous pass of vehicle 2 by storing the signals that were generated by movement sensors 84 (using appropriate filtering) . Alternatively, scouting data may have been entered into map 350 using computer 304, or map 350 may distinguish only between smooth areas (e.g., paved roads) and bumpy areas (e.g., fields) in which case bumpiness level data is not needed if it is assumed that roads are smooth and fields are bumpy. When the vehicle and implement are at positions shown by markers 360 and 362, the vehicle is on road 352 and the expected course of travel shown by arrows 364 indicates that the vehicle is expected to turn into field 354. The current bumpiness level is level 1, and a bumpiness level of 2 is expected after the turn. Similarly, when the vehicle and implement are located at positions shown by markers 366 and 368, the vehicle is in the smoother area of field 354 (level 2) and is about to enter the bumpy area (level 3) . PCC 300 can use the current position of the vehicle and geo-referenced map 350 to estimate the bumpiness level that the vehicle will encounter and to adjust the performance parameters of ACS 26 to accommodate changes in the level of bumpiness. Referring to FIG. 15, vehicle 2 is equipped with another embodiment of an active suspension system which includes an active vibration isolator 400 mounted between a side 402 of cab 6 and a support member 404 extending from chassis 4. Active or passive isolators or supports 406 between cab 6 and chassis 4 allow the cab to move in response to actuations of isolator 400. Isolator 400 may be the same as isolator 28. Since isolator 400 no longer supports the static weight of cab 6, however, spring 44 may be eliminated or have a reduced weight capacity. Eliminating spring 44 eliminates the need for a compressed air source, reduces power used by the system, and reduces cost. To maximize response to cab pitch, isolator 400 is mounted high on side 402 of cab 6. Member 404 may be an engine compartment wall or another vertical support structure securely mounted to chassis 4. Alternatively, member 404 could be oriented along the longitudinal direction of vehicle 2 such that the system is responsive to roll. Isolators 406 may be existing cab mounts. Multiple isolators 400 may be used on side 402 of cab 6 to provide isolation in other axis' such as that provided by bottom-mounted isolators 28-32. Isolator 400 provides control in the longitudinal direction. However, active isolators can also be mounted so as to control movement of cab 6 in the six degrees of freedom. A particular application of an active suspension system for a work vehicle may use all or a subset of the sensors, actuators and other features and components disclosed above, and may include different combinations of the various alternatives. While the embodiments illustrated in the FIGURES and described above are presently preferred, it should be understood that these embodiments are offered by way of example only. For example, depending upon the application, an air-operated actuator 68 may be used in place of a hydraulic actuator. Furthermore, an application may permit use of an electric (e.g., solenoid-type) actuator. The power sources for these actuators include pressurized hydraulic fluid, pressurized air, and electricity, respectively. Also, active isolators may also be mounted to provide isolation for the six degrees of freedom of the cab. The invention is not limited to any particular embodiment, but extends to various modifications that nevertheless fall within the scope of the appended claims.

Claims: WHAT IS CLAIMED IS; 1. An active suspension system for a work vehicle, the work vehicle including a chassis, an operator's cab disposed above the chassis, and another vehicle system having a parameter related to a force applied to the work vehicle, the active suspension system comprising: at least one active vibration isolator mounted at a location between the cab and the chassis and responsive to a control signal to control movement of the cab relative to the chassis; a communication interface coupled to the another vehicle system; and a control circuit coupled to the isolator and the communication interface, the control circuit configured to receive the parameter of the another vehicle system from the communication interface, to generate the control signal at least partly in response to the parameter, and to apply the control signal to the vibration isolator to attenuate movement of the cab due to the force. 2. The active suspension system of claim 1 further including a first sensor configured to generate a first sensed signal indicative of movement of the cab caused by disturbances in the chassis, wherein the control signal primarily depends upon the first sensed signal and secondarily upon the parameter of the another vehicle system. 3. The active suspension system of claim 2 further including a second sensor configured to generate a second sensed signal indicative of displacement between the cab and the chassis, wherein the control signal further depends upon the second sensed signal . 4. The active suspension system of claim 1 wherein the work vehicle includes a tractor and the parameter is a draft force signal indicative of a draft force applied to the work vehicle by an implement. 5. The active suspension system of claim 1 wherein the parameter is a steering angle signal indicative of a normal force applied to the work vehicle. 6. The active suspension -system of claim 1 wherein the parameter is a clutch signal indicative of a clutch force applied to the work vehicle. 7. The active suspension system of claim 1 wherein the parameter is a gear shift signal indicative of a gear shift force applied to the work vehicle. 8. The active suspension system of claim 1 wherein the parameter is a brake signal indicative of a braking force applied to the work vehicle. 9. The active suspension system of claim 1 wherein the parameter is a speed actuator signal indicative of an acceleration force applied to the vehicle. 10. The active suspension system of claim 2 wherein the parameter of the another vehicle system causes a change in system gain. 11. The active suspension system of claim 1 further comprising an operator presence sensor coupled to the control circuit, wherein active movement of the cab is disabled when presence of the operator is not detected. 12. A work vehicle, comprising: a chassis; an operator's cab disposed above the chassis; an active suspension system including at least one active vibration isolator mounted between the cab and the chassis and responsive to a control signal to control movement of the cab relative to the chassis; another vehicle system having a parameter related to a force applied to the work vehicle; and a communication interface coupled between the active suspension system and the another vehicle system; wherein the active suspension system further includes a control circuit coupled to the communication interface and configured to receive the parameter of the another vehicle system, to generate the control signal at lease partly in response to the parameter, and to apply the control signal to the active vibration isolator to attenuate movement of the cab due to the force. 13. The work vehicle of claim 12 further including a first sensor configured to generate a first sensed signal indicative of movement of the cab caused by disturbances in the chassis, wherein the control signal depends primarily upon the first sensed signal and secondarily upon the parameter of the another vehicle system. 14. The work vehicle of claim 12 wherein the work vehicle is a tractor, the another vehicle system includes a height control system coupled to an implement, and the parameter is a draft force signal indicative of a draft force applied to the work vehicle by the implement. 15. The work vehicle of claim 12 wherein the another vehicle system is selected from the group consisting of a steering control system, a clutch control system, a transmission control system, a brake control system and a speed control system, and the parameter is indicative of a force applied to the vehicle by the selected another vehicle system. 16. An active suspension system for a work vehicle, the work vehicle including a chassis, an operator's seat supported by the chassis, and a second vehicle system having a parameter related to a force applied to the work vehicle, the active suspension system comprising: at least one active vibration isolator mounted at a location between the seat and the chassis and responsive to a control signal to control movement of the seat relative to the chassis; a communication interface coupled to the second vehicle system; and a control circuit coupled to the communication interface and the vibration isolator, the control circuit configured to receive the parameter of the second vehicle system from the communication interface, and to generate the control signal applied to the vibration isolator at least partly in response to the parameter, wherein movement of the seat due to the force is attenuated. 17. The active suspension system of claim 16 further including a first sensor configured to generate a first sensed signal indicative of movement of the seat caused by disturbances in the chassis, the control signal depending primarily upon the first sensed signal and secondarily upon the parameter of the second vehicle system. 18. The active suspension system of claim 17 further including a second sensor configured to generate a second sensed signal indicative of displacement between the seat and the chassis, the control signal further depending upon the second sensed signal. 19. The work vehicle of claim 16 wherein the second vehicle system includes a clutch and the parameter is a clutch signal indicative of a clutch force applied to the vehicle, and movement of the cab due to the clutch force is attenuated. 20. The work vehicle of claim 16 wherein the second vehicle system includes a transmission and the parameter is a gear shift signal indicative of a gear shift force applied to the vehicle, and movement of the cab due to the gear shift force is attenuated. 21. The work vehicle of claim 16 wherein the second vehicle system includes a brake and the parameter is a brake signal indicative of a braking force applied to the vehicle, and movement of the cab due to the braking force is attenuated. 22. The work vehicle of claim 16 wherein the second vehicle system includes a speed actuator and the parameter is a speed actuator signal indicative of an acceleration force applied to the vehicle, and movement of the cab due to the acceleration force is attenuated. 23. An active suspension system for a work vehicle, the work vehicle including a chassis, an operator's cab disposed above the chassis, and a second vehicle system having a parameter related to ground speed of the work vehicle, the active suspension system comprising: at least one active vibration isolator mounted at a location between the cab and the chassis and responsive to a control signal to control movement of the cab relative to the chassis; a communication interface coupled to the second vehicle system; and a control circuit coupled to the communication interface and the active vibration isolator, the control circuit configured to receive the parameter of the second vehicle system from the communication interface, to generate the control signal applied to the isolator to attenuate movement of the cab when the ground speed is above a predetermined speed threshold, and to disable cab movement when the ground speed is below the threshold.

Inventors: SCHUBERT WILLIAM L, SCHUBERT, WILLIAM, L.
Applicants: CASE CORP, CASE CORPORATION
Application year: 1998
Main classification: B62D24
IPC codes: B62D33, F16F15