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BTT autopilot design for agile missiles with aerodynamic uncertainty
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作者 Yueyue Ma Jie Guo Shengjing Tang 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2015年第4期802-812,共11页
The approach to the synthesis of autopilot with aerody- namic uncertainty is investigated in order to achieve large maneu- verability of agile missiles. The dynamics of the agile missile with reaction-jet control syst... The approach to the synthesis of autopilot with aerody- namic uncertainty is investigated in order to achieve large maneu- verability of agile missiles. The dynamics of the agile missile with reaction-jet control system (RCS) are presented. Subsequently, the cascade control scheme based on the bank-to-turn (B-I-T) steering technique is described. To address the aerodynamic un- certainties encountered by the control system, the active distur- bance rejection control (ADRC) method is introduced in the autopi- lot design. Furthermore, a compound controller, using extended state observer (ESO) to online estimate system uncertainties and calculate derivative of command signals, is designed based on dynamic surface control (DSC). Nonlinear simulation results show the feasibility of the proposed approach and validate the robust- ness of the controller with severe unmodeled dynamics. 展开更多
关键词 agile missile AUTOPILOT high angle of attack active dis-turbance rejection control (ADRC) dynamic surface control (DSC) extended state observer (ESO).
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