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非线性变结构制导律
引用本文:佘文学,周凤岐,周军.非线性变结构制导律[J].宇航学报,2003,24(6):638-641.
作者姓名:佘文学  周凤岐  周军
作者单位:西北工业大学航天学院,西安,710072
摘    要:为使导弹制导系统具有良好的鲁棒性能和适应性能,本文基于Lyapunov稳定性理论,利用滑模控制来设计导弹的末端导引规律。考虑结构摄动和目标机动加速度的界未知情况下,提出了一种基于零化视线法向速度的具有强鲁棒性的末端导引规律,这种制导律在保证系统闭环稳定的前提下能够在线对结构摄动和目标机动加速度的界进行估计。仿真验证说明所提出的方法是有效的。

关 键 词:非线性系统  鲁棒控制  自适应  制导律
文章编号:1000-1328(2003)06-0638-04
修稿时间:2003年1月14日

Nonlinear variable structure guidance law
SHE Wen-xue,ZHOU Feng-qi,ZHOU Jun.Nonlinear variable structure guidance law[J].Journal of Astronautics,2003,24(6):638-641.
Authors:SHE Wen-xue  ZHOU Feng-qi  ZHOU Jun
Abstract:In this paper,the design of robust controller for a class of uncertain nonlinear systems is considered,and the adaptive variable structure robust controller is presented with uncertainly unknown boundary of structure perturbation and disturbance.It can estimate the uncertain boundary of structure perturbation and disturbance on the premise that the stabilization of close-loop system is guaranteed.The method is applied to the design of anti-ballistic missile strongly robust endgame guidance law based on zeroing normal speed of LOS.The algorithm is very simple and never needs the boundary of the acceleration of target, so it is more convenient for comprehension and practical implementation.The simulating results show that the algorithm is very effective.
Keywords:Nonlinear system  Robust control  Adaptability  Guidance law
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