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航天器多普勒测速平均误差的分析与修正
引用本文:王宏,李海涛,董光亮.航天器多普勒测速平均误差的分析与修正[J].飞行器测控学报,2007,26(1):42-46.
作者姓名:王宏  李海涛  董光亮
作者单位:北京跟踪与通信技术研究所,北京100094
摘    要:对航天器多普勒测速平均误差进行了分析,详细推导了圆轨道和椭圆轨道时该误差的计算公式,计算了不同采样周期和轨道高度时的误差大小。经过分析指出,该项误差对于高轨航天器影响较小,对于低轨航天器可以通过缩短采样周期或利用3个点或多个点的连续测量数据进行修正。

关 键 词:多普勒测速  误差分析与修正  卫星轨道  积分时间
收稿时间:2006-08-31
修稿时间:2006-09-26

Analysis and Calibration of Average Error in Doppler Range Rate Measurement for Spacecraft
WANG Hong, LI Hai-tao, DONG Guang-liang.Analysis and Calibration of Average Error in Doppler Range Rate Measurement for Spacecraft[J].Journal of Spacecraft TT&C Technology,2007,26(1):42-46.
Authors:WANG Hong  LI Hai-tao  DONG Guang-liang
Institution:Beijing Institute of Tracking and Telecommunications Technology, Beijing 100094
Abstract:This paper discusses the average error in Doppler range rate measurement for spacecraft and derives in detail formulas for computation of such errors for circular and elliptic orbits. The magnitude of errors for different sampling periods and orbit altitudes is computed. Based on detailed analysis, the paper points out that the error has less impact on spacecraft in high altitude orbits. As for spacecraft in low altitude orbits, the error can be corrected by reducing sampling periods or with continuous measurement data for three or more points.
Keywords:Range Rate Measurement by Doppler  Error Analysis and Calibration  Satellite Orbit  Integration Time
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