Robust failure compensation for a morphing aircraft model using a probabilistic approach

被引:22
作者
Ataei-Esfahani, Armin [1 ]
Wang, Qian [1 ]
机构
[1] Penn State Univ, Mech & Nucl Engn Dept, University Pk, PA 16802 USA
基金
美国国家科学基金会;
关键词
failure compensation; morphing aircraft; probabilistic robust control; quadratic stability; shape-change device arrays; stochastic gradient algorithms;
D O I
10.1109/TCST.2006.883188
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
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 conventional control surfaces. Each actuator operates at either on or off state; failure of each actuator could cause uncertainty in the applied control input. We characterize the morphing aircraft's actuation failure in a probabilistic way. In particular, each shape-change device within an actuator array is assumed to have certain probability to fail While devices from different arrays may have different failure probabilities. Consequently, we model the uncertain actuator failure as a random parametric uncertainty in the input matrix of the morphing aircraft model. A probabilistic robust explicit-model-following controller is then designed to stabilize the closed-loop system and to satisfy tracking performance subject to uncertain actuator failure. Simulation results are presented and evaluated for the application of this probabilistic robust failure compensation design to lateral dynamics of an Innovative Control, Effector morphing aircraft model.
引用
收藏
页码:324 / 331
页数:8
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