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《JOURNAL OF ASTRONAUTICS》 1994-01
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A NEW AUTOPILOT DESIGN METHOD FOR BANK-TO-TURN MISSILES BASED ON THE VARIABLE STRUCTURE CONTROL THEORY

Zhou Jun; Zhou Fengqi (Northwestern Polytechnical University)Feng Wenjian; Zhen Huanmin(Guidance & Control Dept.of Aerospace Industry Ministry)  
For Bank-to-turn(BTT)missiles,all the autopilot 3-channel independence design methods having presented are single input frequency methods based on the classical control theory,which need omit all the coupling relationship among the three channels of an autopilot.A new autopilot 3-channel independence design method,which is based on the variable structure adaptive control theory,is proposed in this paper.All the coupling factors among the channels are reserved during the design coures, and the control laws gotten from the method totally depend on the maximums and minimums of plant's parameter variations,which makes no need of on-line parameter identification and improves the accuracy of the design and the robustness of the control systems. Paper using the method proposed here and considering many non-ideal factors of control actuators,rato gyros and accelerometers,a 3-channel autopilot of a BTT-90 missile is designed,and some satisfactory digital simulation results are presented.
【CateGory Index】: TJ765.2
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