Reaction jet and aerodynamics compound control missile autopilot design based on adaptive fuzzy sliding mode control

Zhenhui Wu; Chaoyang Dong

doi:10.1117/12.718045

30 October 2006 Reaction jet and aerodynamics compound control missile autopilot design based on adaptive fuzzy sliding mode control

Zhenhui Wu, Chaoyang Dong

Author Affiliations +

Proceedings Volume 6358, Sixth International Symposium on Instrumentation and Control Technology: Sensors, Automatic Measurement, Control, and Computer Simulation; 635839 (2006) https://doi.org/10.1117/12.718045
Event: Sixth International Symposium on Instrumentation and Control Technology, 2006, Beijing, China

Abstract

Because of nonlinearity and strong coupling of reaction-jet and aerodynamics compound control missile, a missile autopilot design method based on adaptive fuzzy sliding mode control (AFSMC) is proposed in this paper. The universal approximation ability of adaptive fuzzy system is used to approximate the nonlinear function in missile dynamics equation during the flight of high angle of attack. And because the sliding mode control is robustness to external disturbance strongly, the sliding mode surface of the error system is constructed to overcome the influence of approximation error and external disturbance so that the actual overload can track the maneuvering command with high precision. Simulation results show that the missile autopilot designed in this paper not only can track large overload command with higher precision than traditional method, but also is robust to model uncertainty and external disturbance strongly.

Citation Download Citation

Zhenhui Wu and Chaoyang Dong "Reaction jet and aerodynamics compound control missile autopilot design based on adaptive fuzzy sliding mode control", Proc. SPIE 6358, Sixth International Symposium on Instrumentation and Control Technology: Sensors, Automatic Measurement, Control, and Computer Simulation, 635839 (30 October 2006); https://doi.org/10.1117/12.718045

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