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Direct Adaptive Control of Systems with Actuator Failures: State of the Art and Continuing ChallengesIn this paper, the problem of controlling systems with failures and faults is introduced, and an overview of recent work on direct adaptive control for compensation of uncertain actuator failures is presented. Actuator failures may be characterized by some unknown system inputs being stuck at some unknown (fixed or varying) values at unknown time instants, that cannot be influenced by the control signals. The key task of adaptive compensation is to design the control signals in such a manner that the remaining actuators can automatically and seamlessly take over for the failed ones, and achieve desired stability and asymptotic tracking. A certain degree of redundancy is necessary to accomplish failure compensation. The objective of adaptive control design is to effectively use the available actuation redundancy to handle failures without the knowledge of the failure patterns, parameters, and time of occurrence. This is a challenging problem because failures introduce large uncertainties in the dynamic structure of the system, in addition to parametric uncertainties and unknown disturbances. The paper addresses some theoretical issues in adaptive actuator failure compensation: actuator failure modeling, redundant actuation requirements, plant-model matching, error system dynamics, adaptation laws, and stability, tracking, and performance analysis. Adaptive control designs can be shown to effectively handle uncertain actuator failures without explicit failure detection. Some open technical challenges and research problems in this important research area are discussed.
Document ID
20080033124
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Tao, Gang
(Virginia Univ. Charlottesville, VA, United States)
Joshi, Suresh M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
August 18, 2008
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: AIAA Guidance, Navigation and Control Conference and Exhibit
Location: Honolulu, HI
Country: United States
Start Date: August 18, 2008
End Date: August 21, 2008
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NSF ECS0601475
WBS: WBS 457280
CONTRACT_GRANT: NNX08AB99A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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