执行机构
控制理论(社会学)
控制工程
计算机科学
控制(管理)
控制系统
飞行操纵面
工程类
航空航天工程
人工智能
空气动力学
电气工程
出处
期刊:Journal of Guidance Control and Dynamics
[American Institute of Aeronautics and Astronautics]
日期:2000-07-01
卷期号:23 (4): 709-718
被引量:75
摘要
Theexplicitdee nitionsof actuatorredundancies areintroduced. Adesign schemeis then presented to synthesize reliable control against actuator failures for dynamic systems possessing actuator redundancies. The properly designed controller is able to guarantee the stability and to maintain the steady-state tracking performance in the event of actuator failures. The design method is based on a robust regional eigenvalue assignment technique with the help of a precompensator. The effectiveness of the proposed method has been verie ed using an example of the aircraft bank angle control problem.
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