Mixed H2/H∞ Linear Parameter Varying State Feedback Control for Bank-to-Turn Missile Autopilot Design
This paper presents a mixed H2/H∞ linear parameter varying state feedback control approach for a bankto-turn missile autopilot design. A mixed H2/H∞ linear parameter varying state feedback control is proposed firstly. In a polytopic domain, linear matrix inequality conditions that depend only on the vertices of polytope are presented to make sure that the prescribed H2 attenuation level, H∞ attenuation level and the stability of the closed-loop system are guaranteed. Then the pole placement method is combined into the proposed controller design to meet some time response characteristics of the closed-loop system. Therefore, the solution of the gain scheduled controller is obtained. There are no structural constraints on the plant and the presented approach can obtain less conservative results than some previous results. Furthermore, the approach is applied to a bank-to-turn missile pitch-axis autopilot design over full flight envelope, the capability and effectiveness of the proposed approach is demonstrated by the results.
mixed H2/H∞ state feedback control linear parameter varying systems bank-to-turn missile autopilot design
Li Hui Guan Chengqi Zhou Danjie Li Fengyi Zha Xu
Beijing Electro-Mechanical Institute, Beijing 100074, China
国际会议
长春
英文
240-246
2010-08-24（万方平台首次上网日期，不代表论文的发表时间）