基于自适应模糊滑模退步控制的直接力/气动力复合控制导弹自动驾驶仪设计

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2007, Vol. 28 ›› Issue (增): 141-145.

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Reaction jet and Aerodynamics Compound Control Missile Autopilot Design Based on Adaptive Fuzzy Sliding Mode Control via Backstepping

CHEN Yu,DONG Chao-yang,WANG Qing,ZHANG Ming-lian

School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics

Received:2006-11-06 Revised:2007-02-02 Online:2007-08-10 Published:2007-08-10
Contact: CHEN Yu

Abstract

Abstract:

Aim at nonlinearity and strong couple of reactionjet and aerodynamics compound control missile, a missile autopilot design method based on adaptive fuzzy sliding mode control (AFSMC) via backstepping is proposed.

Key words: reaction , jet , and , aerodynamics , compound , control, , missile , autopilot, , adaptive , fuzzy , control, , sliding , mode , control, , backstepping , design , method

CLC Number:

TJ765.2

CHEN Yu;DONG Chao-yang;WANG Qing;ZHANG Ming-lian. Reaction jet and Aerodynamics Compound Control Missile Autopilot Design Based on Adaptive Fuzzy Sliding Mode Control via Backstepping[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2007, 28(增): 141-145.

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Reaction jet and Aerodynamics Compound Control Missile Autopilot Design Based on Adaptive Fuzzy Sliding Mode Control via Backstepping

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