多约束多输入拦截器姿轨一体化复合控制

doi:10.12305/j.issn.1001-506X.2023.03.22

Abstract

Abstract:

An attitude and trajectory integrated compound control method with high precision and low energy consumption is proposed for the near space kinetic interceptor. Firstly, based on the kinematics and dynamics of interceptor, characteristics of actuators and the structure of full strapdown seeker, the guidance and control system model of the full strapdown attitude and trajectory compound control interceptor is established. Secondly, the mapping function including the body line-of-sight is designed using the arctangent function. Aiming at the attitude and trajectory coupling problem, combined with the high order sliding mode control, the integrated attitude and trajectory compound control law is designed to achieve multiple tasks while satisfying the body line-of-sight constraint and the impact angle constraint. Finally, the stability of the system controlled by the proposed control law is proved based on Lyapunov stability theory, and the superiority of the integrated design, the effectiveness of the mapping function's constraint and the robustness of the proposed control law are verified by simulation results.

Key words: kinetic interceptor, compound control, attitude and trajectory coupling, sliding mode variable structure control, integrated guidance and control, state constraint

CLC Number:

Qian PENG, Jianguo GUO, Zongyi GUO, Guoqing WANG. Multi-constraint multi-input interceptor integrated attitude and trajectory compound control[J]. Systems Engineering and Electronics, 2023, 45(3): 806-813.

Figures/Tables 11

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控制器	脱靶量/m	拦截时间/s	交会角/(°)
IGC-SMC	0.000 2	10.13	-0.001 7
BC-SMC	0.011 4	10.17	-0.000 1

控制器	姿控发动机冲量	轨控发动机冲量
IGC-SMC	9.718	89.18
BC-SMC	10.840	107.50

控制器	脱靶量/(×10^－4 m)	交会角/(°)
EDO-CSMC	5.83	-0.001 6
CSMC	0.43	-0.006 3
EDO-SMC	2.25	-0.001 7
SMC	6.82	-0.145 3

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Multi-constraint multi-input interceptor integrated attitude and trajectory compound control

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