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The Study of the Relation Between Faulty Tolerant Bound and Control Allocation
Abstract:
Fault tolerant control can improve the safety of aircraft under control surface failures. Sometime the redundancy method losses its effectiveness when the actuator is impaired severely. Under this condition the fault tolerant method can not be used to compensate failures. The paper proposes a method to find the bound by analysis and computer by moment for fault tolerant control. And give the effect on control allocation. At last the fault tolerant bound is added to control allocation as one of limit conditions.
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4077-4081
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Online since:
January 2012
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© 2012 Trans Tech Publications Ltd. All Rights Reserved
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