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安装误差和动不平衡对旋转导弹惯性器件输出的影响及补偿
引用本文:高庆丰,夏群力,方蜀州,陈罗婧. 安装误差和动不平衡对旋转导弹惯性器件输出的影响及补偿[J]. 北京理工大学学报, 2010, 30(7): 765-770
作者姓名:高庆丰  夏群力  方蜀州  陈罗婧
作者单位:北京理工大学,宇航学院,北京,100081;航天东方红卫星有限公司,北京,100094
摘    要:为了提高旋转导弹惯性器件的测量精度.建立了弹体坐标系和动平衡坐标系并给出其转换关系;给出了陀螺仪坐标系、加速度计坐标系分别与弹体坐标系之间的转换关系.推导了安装误差和弹体动不平衡引起的陀螺仪和加速度计的测量误差模型,并进行了仿真.结果表明,利用直接补偿和高通滤波补偿方法实现了对陀螺仪和加速度计测量结果的补偿,仿真结果验证了补偿方法的可行性.

关 键 词:旋转导弹  动不平衡  安装误差  惯性器件

Influence of Installation Error and Dynamic Imbalance on the Output of Inertia Devices in Rolling Missiles and Its Compensation
GAO Qing-feng,XIA Qun-li,FANG Shu-zhou,CHEN Luo-jing. Influence of Installation Error and Dynamic Imbalance on the Output of Inertia Devices in Rolling Missiles and Its Compensation[J]. Journal of Beijing Institute of Technology(Natural Science Edition), 2010, 30(7): 765-770
Authors:GAO Qing-feng  XIA Qun-li  FANG Shu-zhou  CHEN Luo-jing
Affiliation:GAO Qing-feng1,XIA Qun-li1,FANG Shu-zhou1,CHEN Luo-jing2(1.School of Aerospace,Beijing Institute of Technology,Beijing 100081,China,2.DFH Satellite Company Ltd,Beijing 100094,China)
Abstract:To improve the measurement precision of inertia devices in rolling missile,the missile body coordinate and dynamic balance coordinate system were established,and the transform between them was derived.The transformations among gyro coordinate,accelerometer coordinate and missile body coordinate system were also given in this paper.The models for the measurement error of gyros and accelerometers,which are caused by installation error and body dynamic imbalance,were deduced.Simulation results show the necessi...
Keywords:rolling missiles  dynamic imbalance  installation error  inertia devices  
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