Adaptive Variable Structure Guidance System Design of a Longitudinal Automatic Carrier Landing System
The design problem of guidance system of a longitudinal automatic carrier landing system is considered. The mathematic model of the landing guidance problem is created based on the analysis of the main architecture of a longitudinal automatic carrier landing system. The landing guidance system is designed via adaptive variable structure sliding mode control theory and the stability of guidance system is analyzed. The chattering problem is solved via using hyperbolic tangent. Simulation results indicate that the guidance system has the merits of response fast and tracking precisely and validate the feasibility and reasonability of this method.
Automatic Landing Adaptive Variable Structure Control Guidance Law Chattering
Zhu Qi-dan Wang Tong Zhong Xun-yu Zhou Fang
College of Automation,Harbin Engineering University,Harbin 150001,China
国际会议
2009年中国控制与决策会议(2009 Chinese Control and Decision Conference)
广西桂林
英文
4855-4859
2009-06-17（万方平台首次上网日期，不代表论文的发表时间）