Adaptive sliding-mode guidance of a homing missile

被引：0
|
作者：
Zhou, Di [1 ,2 ,3 ]
Mu, Chundi [1 ]
Xu, Wenli [1 ,4 ]
机构：
[1] Tsinghua University, 100084 Beijing, China
[2] Harbin Institute of Technology, Harbin, China
[3] Automation Department, Tsinghua University, Beijing, China
[4] University of Colorado, Boulder, CO, United States
来源：
Journal of Guidance, Control, and Dynamics | / 22卷 / 04期
关键词：
Adaptive control systems - Computer simulation - Control system synthesis - Linear control systems - Nonlinear control systems - Robustness (control systems) - Time varying control systems;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Sliding-mode control is applied to design robust homing missile guidance law. The sufficient and necessary condition for the sliding-mode motion of a linear time-varying system not to be affected by disturbances and the sufficient condition for that motion not to be affected by parameter perturbations are given. An adaptive reaching law of sliding mode for a linear time-varying system is then presented and used to derive an adaptive sliding-mode guidance law. Theoretical analysis and simulation results show that the adaptive sliding-mode guidance law is robust against disturbances and parameter perturbations. Furthermore, the presented guidance law is simple to implement in practice.
引用
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页码：589 / 594
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