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激光星间链路终端指向误差标定中的误差分离研究
引用本文:程竟爽,林益明,何善宝,王海红,国爱燕.激光星间链路终端指向误差标定中的误差分离研究[J].宇航学报,2019,40(1):85-93.
作者姓名:程竟爽  林益明  何善宝  王海红  国爱燕
作者单位:1. 北京空间飞行器总体设计部,北京 100094;2. 中国空间技术研究院,北京 100094
摘    要:针对激光星间链路终端指向误差在轨标定中航天器姿态测量误差影响标定结果的问题,本文提出了基于多链路测量的航天器姿态测量误差分离方法。该方法利用了导航星座中同一航天器同时建立多条链路的特点,获取不同方向的LCT指向误差测量数据。通过同时估计航天器姿态测量误差与LCT自身指向误差参数,实现了航天器姿态测量误差与LCT自身指向误差的分离。仿真结果表明:航天器姿态测量误差对LCT指向误差标定结果有显著影响,利用本方法进行误差分离后,LCT指向误差标定结果最大偏差由分离前的64.9 μrad下降到误差分离(6条链路)后的21.1 μrad,有效降低了航天器姿态测量误差对LCT指向误差标定结果的影响。该方法的有效性取决于链路条数和链路拓扑构型。

关 键 词:激光星间链路终端  指向误差  在轨标定  误差分离  
收稿时间:2018-03-05

Research on Error Separation in In Orbit Calibration of Laser Communications Terminal Pointing Error
CHENG Jing shuang,LIN Yi ming,HE Shan bao,WANG Hai hong,GUO Ai yan.Research on Error Separation in In Orbit Calibration of Laser Communications Terminal Pointing Error[J].Journal of Astronautics,2019,40(1):85-93.
Authors:CHENG Jing shuang  LIN Yi ming  HE Shan bao  WANG Hai hong  GUO Ai yan
Affiliation:1. Beijing Institute of Spacecraft System Engineering, Beijing 100094, China; 2.China Academy of Space Technology, Beijing 100094, China
Abstract: The in-orbit calibration accuracy of the LCT pointing error is corrupted by the spacecraft’s attitude measurement errors. A method using measurements from multiple inter-satellite links to the separation of the spacecraft’s attitude measurement errors is proposed. The measurement data of the LCT pointing errors are acquired from multiple directions corresponding to the inter-satellite links established in navigation constellation. The spacecraft’s attitude measurement errors and LCT pointing error parameters are estimated simultaneously utilizing those measurements. The simulation results show that the calibration accuracy of the LCT pointing error is severely affected by the spacecraft’s attitude measurement errors. While applying parameters estimation with this method, the maximal error of the resulting estimated pointing error parameters is reduced from 64.9 μrad to 21.1 μrad (with 6 links), demonstrating the validity of this error separation method. It also shows the accuracy of this method is dominated by the number and the topology of the inter-satellite links observed.
Keywords:Laser communications terminal  Pointing error  In-orbit calibration  Error separation  
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