Robust Failure Compensation for a Morphing Aircraft Model Using a Probabilistic Approach

We present a probabilistic robust control design for a morphing aircraft model subject to uncertain actuator failure. The morphing aircraft model has multiple distributed arrays of shape-change devices that are used to generate moments for stabilization and low-rate maneuvering, augmenting conventio...

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Veröffentlicht in:	IEEE transactions on control systems technology Jg. 15; H. 2; S. 324 - 331
Hauptverfasser:	Ataei-Esfahani, Armin, Wang, Qian
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	New York, NY IEEE 01.03.2007 Institute of Electrical and Electronics Engineers The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Schlagworte:	Actuator failure Actuators Aerospace control Aircraft propulsion Applied sciences Arrays Computer science; control theory; systems Control system synthesis Control systems Control theory. Systems Devices Exact sciences and technology Failure Failure compensation Fracture mechanics (crack, fatigue, damage...) Fundamental areas of phenomenology (including applications) Ice Morphing aircraft Physics Probabilistic methods probabilistic robust control Probability theory quadratic stability Robust control Robustness Shape control shape-change device arrays Solid mechanics stochastic gradient algorithms Structural and continuum mechanics Studies Uncertainty Vehicles Stabilization dynamic control Control synthesis Modeling Uncertain system Apparatus failure Metamorphosis Transducer network Actuator Multimodel control Parametric excitation Failure compensation shape-change device arrays Probabilistic approach morphing aircraft Rupture Morphism Control surface quadratic stability Robust control Engineering design probabilistic robust control Reliability Aircraft stochastic gradient algorithms
ISSN:	1063-6536, 1558-0865
Online-Zugang:	Volltext
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