基于改进人工势场法的再入制导方法

doi:10.12305/j.issn.1001-506X.2023.07.27

Abstract

Abstract:

Aiming at the reentry guidance of hypersonic vehicles with no-fly zones, a three-dimensional guidance method is proposed based on the improved artificial potential field method (APFM). In the longitudinal direction, dynamic pressure, overload, and heat flow process constraints are regarded as virtual obstacles, and terminal altitude and speed are regarded as virtual target. Then, the longitudinal artificial potential field function is improved to adapt to the trajectory design of skip reentry trajectory and quasi-equilibrium gliding trajectory. A double layer predictive-correction algorithm is designed to solve the adjustable parameters to consider the effect of no-fly zones on three-dimensional trajectory. The simulation results show that the proposed improved APFM can adapt to different types of no-fly zone shapes. It can adapt to target points with larger crossrange requirements than existing methods. The parameters are simple to adjust and easy to implement in engineering.

Key words: reentry guidance, no-fly zones, virtual obstacles, improved artificial potential field method (APFM)

CLC Number:

V448

Shenming QUAN, Songyan WANG, Tao CHAO, Ming YANG. Reentry guidance method based on improved artificial potential field method[J]. Systems Engineering and Electronics, 2023, 45(7): 2158-2169.

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References 30

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参数	起点状态	终点状态
经度	0	70
纬度	0	0
高度	120	15
速度	7 500	1 000
倾角	0	0
偏角	-90	—

方法	终端经度/(°)	终端纬度/(°)	待飞射程/km
本文方法	84.542 5	19.956 4	222.148
方法1	82.246 8	16.671 5	639.107
方法2	80.811 1	13.681 1	995.568
GPOPS	84.979 0	20.156 5	200.999

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Reentry guidance method based on improved artificial potential field method

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