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三向测量技术在深空探测中的应用研究
引用本文:黄磊,王宏,樊敏.三向测量技术在深空探测中的应用研究[J].飞行器测控学报,2012(3):6-10.
作者姓名:黄磊  王宏  樊敏
作者单位:北京跟踪与通信技术研究所
摘    要:较详细地介绍了三向测量技术(包括三向测距和三向测速),阐述使用三向测量的工程背景和重要意义,给出利用三向测量数据进行实时定位的数学推导,并分别对三向测距和三向测速原始数据的误差进行了分析;最后给出在"嫦娥一号"试验轨道段采用三向测量技术得到的残差分析结果。结果表明,在未进行站间时间同步的情况下,"嫦娥一号"卫星100km×100km环月轨道段三向测距误差约200m,三向测速误差约2cm/s,利用三向测量数据可以单独进行轨道确定,验证了我国后续深空探测中应用三向测量技术的可行性。

关 键 词:三向测量  三向测距  三向测速  深空探测  误差分析

Application of Three-way Measurement in Deep Space Exploration
HUANG Lei,WANG Hong,FAN Min.Application of Three-way Measurement in Deep Space Exploration[J].Journal of Spacecraft TT&C Technology,2012(3):6-10.
Authors:HUANG Lei  WANG Hong  FAN Min
Institution:(Beijing Institute of Tracking and Telecommunications Technology,Beijing 100094)
Abstract:The engineering background and significance of three-way measurement(including three-way ranging and three-way Doppler) are introduced.The mathematical model and application scenarios for real-time trajectory determination using three-way measurements are given and the theoretical error of data is analyzed.The result of residual error analyses of Chang’E-1 three-way measurement shows that without time synchronization,three-way ranging error is approximately 200m and three-way Doppler error is approximately 2 cm/s in 100 km×100 km lunar orbit.Therefore,three-way measurement data can be used independently for orbit determination and it is feasible to use three-way measurement in future deep space missions.
Keywords:three-way measurement  three-way ranging  three-way Doppler  deep space  error analysis
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