Lyapunov-Based Exponential Tracking Control of a Hypersonic Aircraft with Aerothermoelastic Effects

被引:126
|
作者
Wilcox, Z. D. [1 ]
MacKunis, W. [1 ]
Bhat, S. [1 ]
Lind, R. [1 ]
Dixon, W. E. [1 ]
机构
[1] Univ Florida, Dept Mech & Aerosp Engn, Gainesville, FL 32611 USA
关键词
ASYMPTOTIC TRACKING; ADAPTIVE-CONTROL; FEEDBACK-CONTROL; SYSTEMS; MODEL;
D O I
10.2514/1.46785
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Hypersonic flight conditions produce temperature variations that can alter both the structural dynamics and flight dynamics. These aerothermoelastic effects are modeled by a nonlinear, temperature-dependent, parameter-varying state-space representation. The model includes an uncertain parameter-varying state matrix, an uncertain parameter-varying nonsquare (column-deficient) input matrix, and a nonlinear additive bounded disturbance. A Lyapunov-based continuous robust controller is developed that yields exponential tracking of a reference model, despite the presence of bounded nonvanishing disturbances. Simulation results for a hypersonic aircraft are provided to demonstrate the robustness and efficacy of the proposed controller.
引用
收藏
页码:1213 / 1224
页数:12
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