Compound Control Strategy for Missile with Lateral Thrust and Aerodynamic Based on Zero-Effort Miss and Overload Error
GAO Zhenxin， ZHAO Wei， WANG Yichong， BI Peng， HOU Zhenqian
Shanghai Electro-mechanical Engineering Institute， Shanghai 201109，China
Abstract In order to solve the problem that conventional control strategy is difficult to effectively correct the handover error of midcourse and terminal guidance, a new control strategy is proposed in this paper. Firstly, the mathematical model of compound control system with lateral thrust and aerodynamic is established, then the common orbital control strategies of near space target interceptors are analyzed, and through simulation comparison, the orbital control strategies with the best control performance is selected. On this basis, combined with the work requirements of near space target interceptors, an orbital control strategy based on zero-effort miss and overload error is proposed. The simulation results show that the new control strategy can reduce fuel consumption over 40% on the premise of ensuring hitting precision, which is more conducive to hitting targets with larger position error.
Key words ：
near space target interceptor
compound lateral thrust and aerodynamic
orbital control
overload error
zero-effort miss
Received: 11 December 2020
Published: 15 December 2022
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2022, Vol. 5 
