Claims
- 1. A method comprising the step of:
a) generating a hedge signal to avoid adaptation to at least one characteristic of an adaptive control system and/or a plant controlled by the adaptive control system.
- 2. A method as claimed in claim 1 further comprising the steps of:
b) modifying a commanded state signal with the hedge signal; and c) generating a reference model state signal based on the commanded state signal modified with the hedge signal in the step (b).
- 3. A method as claimed in claim 2 further comprising the step of:
d) generating a tracking error signal based on the reference model state signal and a plant state signal; and e) generating an adaptive control signal to adapt control response of the adaptive control system.
- 4. A method as claimed in claim 1 wherein the hedge signal is generated in the step (a) based on a difference between a first signal derived from a plant model not having the characteristic, and a second signal derived from a plant model having the characteristic.
- 5. A method as claimed in claim 4 wherein the first signal is generated based on an input control signal and a plant state signal in addition to the plant model not having the characteristic, and the second signal is generated further based on a command control signal and a plant state signal in addition to the plant model having the characteristic.
- 6. A method as claimed in claim 5 wherein the input control signal is generated based on at least one of the commanded state signal, reference model state signal, a plant state signal, and an adaptive control signal.
- 7. A method as claimed in claim 6 wherein the command control signal is generated based on the input control signal modified by a control allocation and a control characteristic imposed by the controller.
- 8. A method as claimed in claim 4 where in the second signal is generated based on an actuator state signal.
- 9. A method as claimed in claim 5 further comprising the step of:
b) generating a display based on the input control signal, an operator generating the command control signal based on the display.
- 10. A method as claimed in claim 1 wherein the plant is an aircraft and/or spacecraft.
- 11. A method as claimed in claim 1 wherein the plant is an automobile.
- 12. A method as claimed in claim 1 wherein the plan is an unmanned vehicle.
- 13. In an adaptive control system for controlling a plant, a hedge unit coupled to receive at least one control signal and a plant state signal, the hedge unit generating a hedge signal based on the control signal, the plant state signal, and a hedge model including a first model having a characteristic to which the adaptive control system is not to adapt, and a second model not having the characteristic to which the adaptive control system is not to adapt, the hedge signal used in the adaptive control system to remove the characteristic from a signal supplied to an adaptation law unit of the adaptive control system so that the adaptive control system does not adapt to the characteristic in controlling the plant.
- 14. An adaptive control system as claimed in claim 13 wherein the characteristic is a time delay between generation of the commanded state signal by the controller at a time, and receipt by the controller of the plant state signal resulting from the commanded state signal generated at the time.
- 15. An adaptive control system as claimed in claim 13 wherein the characteristic is a time delay between generation of a state by the plant and sensing of the state of the plant by the sensor to generate the plant state signal.
- 16. An adaptive control system as claimed in claim 13 wherein the characteristic pertains to a control limit of the actuator used to control the plant.
- 17. An adaptive control system as claimed in claim 13 wherein the control limit pertains to actuator end points.
- 18. An adaptive control system as claimed in claim 13 wherein the control limit pertains to actuator dynamics.
- 19. An adaptive control system as claimed in claim 13 wherein the control limit pertains to a rate limit of the actuator.
- 20. An adaptive control system as claimed in claim 13 wherein the control limit pertains to quantization effects associated with the actuator.
- 21. An adaptive control system as claimed in claim 13 wherein the plant is an aircraft and/or spacecraft.
- 22. An adaptive control system as claimed in claim 13 wherein the plant is an automobile.
- 23. An adaptive control system as claimed in claim 13 wherein the plant is an unmanned vehicle positioned remotely from an operator.
CROSS-REFERENCE TO RELATED APPLICATION
[0001] This application is a continuation under 35 U.S.C. §120 and 37 C.F.R. §1.53(b) of copending U.S. patent application Ser. No. 09/585,106, filed on May 31, 2000, which application claimed the benefit of provisional application No. 60/199,615, filed Apr. 24, 2000, which are hereby incorporated herein in their entirety by reference.
STATEMENT OF U.S. GOVERNMENT RIGHTS IN THE INVENTION
[0002] This invention was made with U.S. Government funding under Contract No. NAG8-1638 awarded by the National Aeronautics and Space Administration (NASA)—Marshall Space Flight Center and Contract No. F49620-98-1-0437 awarded by the Air Force Office of Scientific Research (AFOSR). The U.S. Government has certain rights in the invention.
Provisional Applications (1)
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Number |
Date |
Country |
|
60199615 |
Apr 2000 |
US |
Continuations (1)
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Number |
Date |
Country |
| Parent |
09585106 |
May 2000 |
US |
| Child |
10602458 |
Jun 2003 |
US |