A Sliding Mode Guidance Law for Impact Time Control with Field of View Constraint

doi:10.3969/j.issn.1000-1093.2019.04.013

Abstract

Abstract: To improve the robustness and engineering adaptability of the impact time control guidance law, a nonsingular impact time control guidance law with seeker's field of view constraint is designed using sliding mode technique based on the geometrical relation of projectile interception. The stability and convergence of the proposed guidance law are proved by Lyapunov theory. The theoretically analyzed and simulated results show that, when the impact time error is zero, the proposed guidance law can evolve into a pure proportional navigation guidance law, and the required terminal acceleration of the proposed guidance law is fairly smooth, converging to zero during interception. The proposed guidance law can be used to effectively control the impact time for stationary target interception and multi-missile cooperative attack. Key

Key words: missile, impacttimecontrol, field-of-viewangleconstraint, slidingmodecontrol, proportionalnavigationlaw

CLC Number:

TJ765.3⁺1

CHEN Shengfu, CHANG Sijiang, WU Fang. A Sliding Mode Guidance Law for Impact Time Control with Field of View Constraint[J]. Acta Armamentarii, 2019, 40(4): 777-787.

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第40卷
第4期2019 年4月兵工学报ACTA
ARMAMENTARIIVol.40No.4Apr.2019

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