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INS地面自对准的鲁棒性分析
引用本文:陈文华,任俊.INS地面自对准的鲁棒性分析[J].南京航空航天大学学报,1997,29(1):20-25.
作者姓名:陈文华  任俊
作者单位:[1]南京航空航天大学自动控制系 [2]湖北宜昌测试技术研究所
摘    要:讨论了惯性导航系统(INS)地面自对的鲁棒性能问题。文中指出当采用两个水平方向加速度计作为测量时,INS的地面自对准稳态性能与设计滤波民采用的噪声方差无关。但由于自对准的时间限制,实际自对准性能鲁棒性,即滤波器的稳态性能,可以通过鲁棒设计得进。利用对策论原理,文中给出了最优鲁棒INS自对准设计方案。

关 键 词:惯性导航  自对准  鲁棒性

Robustness Analysis of INS Ground Alignment
Chen Wenhua.Robustness Analysis of INS Ground Alignment[J].Journal of Nanjing University of Aeronautics & Astronautics,1997,29(1):20-25.
Authors:Chen Wenhua
Abstract:Discusses the performance robustness of an Inertial Navigation System (INS)ground alignment. It points out that the steady state performance of the INS ground alignrnent is not affected by the choice of the noise covariances in the design of Kalman filters when two level accelerations are used in the measurement. However because of the limitation of the alignment time in reality, the alignment performance robustness of the ground alignment can be enhanced by robust design. The optimal robust INS ground alignment scheme is presented using game theory.
Keywords:inertial navigation  alignment  robustness  Kalman filter  noise uncertainties
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