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Xu, Bin; Huang, Xiyuan; Wang, Danwei; Sun, Fuchun

Dynamic surface control of constrained hypersonic flight models with parameter estimation and actuator compensation. (English) Zbl 1286.93058

Asian J. Control 16, No. 1, 162-174 (2014).
Summary: In this paper, the robust adaptive controller is investigated for the longitudinal dynamics of a generic hypersonic flight vehicle. The proposed methodology addresses the issue of controller design and stability analysis with respect to parametric model uncertainty and input saturations for the control-oriented model. The velocity and attitude subsystems are transformed into linearly parameterized form. Based on the parameter projection estimation, a dynamic inverse control is proposed via the back-stepping scheme. In order to avoid the problem of “explosion of complexity”, by introducing a first-order filtering of the synthetic input at each step, the dynamic surface control is designed. The closed-loop system achieves uniform ultimately bounded stability. The compensation design is employed when input saturations occur. Simulation results show that the proposed approach achieves good tracking performance.

Cited in 36 Documents

MSC:

93B35 Sensitivity (robustness)
93C40 Adaptive control/observation systems
93E10 Estimation and detection in stochastic control theory
93E15 Stochastic stability in control theory
93A30 Mathematical modelling of systems (MSC2010)

Keywords:

hypersonic flight vehicle; linearly parameterized form; dynamic surface control; input saturation
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\textit{B. Xu} et al., Asian J. Control 16, No. 1, 162--174 (2014; Zbl 1286.93058)
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