固定鸭舵二维修正弹比例导引律参数优化

doi:10.7527/S1000-6893.2020.24751

Abstract

Abstract: To solve the problems of limited control force of the 2D correction mechanism with fixed canards and the overload variation required at the end of the control section by the Proportional Navigation Guidance (PNG), an overload threshold control strategy based on the PNG is proposed. The control forces and moments of the correction mechanism are analyzed. With the objective function of the minimum distance between the projectile and target, the longitudinal and transverse planar guidance coefficients and overload thresholds are selected as the design variables, and a parameter optimization model is established based on the PNG. The model is then optimized by the Differential Evolution (DE) algorithm. Finally, the control strategy proposed is compared with the traditional PNG in terms of flight stability, control efficiency, control mechanism overload, and control accuracy by external ballistic simulation, and the effectiveness of the control strategy is also verified by the Monte-Carlo method. The results show that compared with the traditional PNG, the control strategy proposed can improve the flight stability of the control section and reduce the overload at the end of the control section of the 2D ballistic correction projectile.

Key words: fixed canards, proportional navigation guidance, optimal design, differential evolution, flight stability

CLC Number:

CAO Lifei, CAO Hongsong, LIU Pengfei, LIU Hengzhu, XIAO Yanwen. Parameter optimization of proportional navigation guidance for 2D trajectory correction projectile with fixed canards[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(6): 324751-324751.

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Parameter optimization of proportional navigation guidance for 2D trajectory correction projectile with fixed canards

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