Design of air-breathing supersonic vehicle guidance law for intercepting the high maneuvering target with impact angle constraint

Author:

Xu Zihe,Ming Chao,Bai Zhiheng,Feng Tong

Abstract

Abstract To achieve interception vehicles that can intercept high maneuvering targets with impact angle constraint, and improve the strike effectiveness of the vehicle, based on the two-dimensional planar motion model of the vehicle and the target, this article proposes a sliding mode control vehicle guidance law. The stability of the guidance law is verified through the Lyapunov function, and an extended state observer is set to check for disturbances. After simulation verification, the guidance law can intercept the target with predetermined terminal angle constraints and has good tracking performance.

Publisher

IOP Publishing

Reference9 articles.

1. Impact angle constraint guidance law using fully-actuated system approach;Chen;Aerospace Science and Technology,2023

2. Terminal impact angle control guidance law considering target observability;Li;Aerospace,2022

3. Adaptive sliding mode interception guidance for the vehicle with unknown target acceleration;Liang;Journal of Astronautics,2022

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