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机构地区:[1]哈尔滨工业大学航天工程系,哈尔滨150001
出 处:《航天控制》2011年第4期55-60,93,共7页Aerospace Control
摘 要:针对预警卫星系统所具有的建模不确定性与干扰不确定性,为了实现凝视相机对战术弹道导弹的快速、高精度自动跟踪指向控制,设计了具有鲁棒稳定性的星体姿态与相机跟踪指向的复合控制系统。先利用拉格朗日法建立了预警卫星系统的动力学模型,在研究凝视相机对战术弹道导弹跟踪规律的基础上,运用H∞回路成形理论设计了星体姿态和相机跟踪指向的复合控制器,并利用μ分析方法研究了控制器的鲁棒稳定性。数学仿真表明,所设计的H∞回路成形控制器不仅具有鲁棒稳定性,而且控制精度、控制效率都高。Aiming at resolving the modeling uncertainty and disturbance uncertainty with the early warn ing satellite system, a compound control system combining with a camera tracking and pointing system that involves the satellite attitude of robust stability is designed to realize a quick and highly accurate automatic tracking and pointing control of the staring camera of tactical ballistic missiles. Firstly, a dynamics model is established by employing the Lagrange method. Then a compound controller with the combined functions of satellite attitude and camera tracking and pointing is designed in light of the theory of H ~ loop shaping, which is based on the research of the rule of the staring camera tracking the tactical ballistic missiles. Mean- while the robust stability of the controller is researched by using the method of μ analysis. The mathematical simulation demonstrates that the designed H∞ loop shaping controller is not only of robust stability, but also is of high control accuracy and efficiency.
分 类 号:TP273.3[自动化与计算机技术—检测技术与自动化装置]
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