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用GPS评定IMU(惯性测量装置)误差
引用本文:孙梅.用GPS评定IMU(惯性测量装置)误差[J].航天控制,1995(1).
作者姓名:孙梅
作者单位:北京航天自动控制研究所
摘    要:在导弹飞行试验时,基于GPS的弹道基准系统可替代常规雷达。由于GPS弹道基准的精度高,所以可用来评定导弹惯性测量装置的性能。在两发现役的和平保卫者导弹发射前配置了GPS转发器和三波段天线。根据GPS测量的矩离、矩离增量数据,用卡尔曼滤波方法评定各个IMU误差,结果证明GPS优于雷达。

关 键 词:全球定位系统,惯性测量装置,误差,卡尔曼滤波

The Use of GPS for Evaluating Inertial Measurement Unit Errors
Sun Met.The Use of GPS for Evaluating Inertial Measurement Unit Errors[J].Aerospace Control,1995(1).
Authors:Sun Met
Institution:Beijing Aerospace Automatic Control Institute 100854
Abstract:A trajectory refenence system based on the Global Positioning System(GPS)can be used instead of conventional radars during missile flight tests.The high quality of the GPS-based trajectory reference makes it useful for evaluating the performance of the missile's Inertial Measurement Units(IMUs).Such a system was installed and flight tested on two recently launched ballistic missiles.The GPS hardware configuration used on these flight is described.A kalman filter approach The ability of the GPS-based system to identify IMU errors is compared to that of radar;GPS is found to provide superior estimates of the IMU errors.
Keywords:Global positioning system  Inertial measur ement unit Error Kalman filtering  
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