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Non-Static error tracking control for near space airship loading platform
[摘要] A control scheme based on internal model with non-static error is presented against the uncertainty of the near space airship loading platform system. The uncertainty in the tracking table is represented as interval variations in stability and control derivatives. By formulating the tracking problem of the uncertainty system as a robust state feedback stabilization problem of an augmented system, sufficient condition for the existence of robust tracking controller is derived in the form of linear matrix inequality (LMI). Finally, simulation results show that the new method not only has better anti-jamming performance, but also improves the dynamic performance of the high-order systems.
[发布日期]  [发布机构] National University of Defense Technology, Changsha; 410000, China^1;China Satellite Maritime Tracking and Control Department, Jiangyin; 214431, China^2
[效力级别] 材料科学 [学科分类] 
[关键词] Anti jamming performance;Dynamic performance;High order systems;Internal modeling;Robust state feedback;Robust tracking controller;Stability and control;Uncertainty system [时效性] 
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