基于积分滑模控制的导引律设计
Guidance Law Design Based on Integral Sliding Mode Control
综述文章：本文研究了导弹拦截机动目标的末端制导问题。基于积分滑模控制理论,提出了一种新型导引律的设计方法。将目标机动视为有界的外部扰动,设计了一种非线性积分滑模导引律,此导引律使得视线角速度和视线角具有有限时间收敛特性。仿真结果验证了所提方法的有效性。
Reviews: The terminal guidance problem for missile intercepting maneuvering targets is developed. Based on integral sliding mode (ISM) control method, a novel guidance law is designed. Regarding the target acceleration as unknown bounded disturbance, a nonlinear ISM guidance law is introduced. The obtained guidance law guarantees the line-of-sight (LOS) angular rate and LOS angle a finite-time convergence characteristics. Simulation comparison results demonstrate the effectiveness of the presented method.
罗生、张振兴、李世华
军用火箭、导弹技术军事技术航空航天技术
导弹导引律积分滑模控制有限时间控制
Missileguidance lawintegral sliding mode controlfinite-time control
罗生,张振兴,李世华.基于积分滑模控制的导引律设计[EB/OL].(2012-12-18)[2025-08-16].http://www.paper.edu.cn/releasepaper/content/201212-429.点此复制
评论