›› 2017, Vol. 43 ›› Issue (5): 49-54.doi: 10.3969/j.issn.1674-1579.2017.05.008

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Relative Position Precision Analysis and Decomposition of 9 Degree of Freedom Motion Simulator

 LI  Bo, WU  Fen-Zhi, WANG  Yun-Feng, HE  Hua-Dong, FU  Tong-Ling, XU  Bo   

  1. (1.Tianjin Key Laboratory of Microgravity Environment Simulation Technology, Tianjin 300458, China; 2.Tianjin Institute of Aerospace Mechanical and Electrical Equipment, Tianjin 300458, China; 3.Beijing Institute of Control Engineering, Beijing 100094, China)
  • Received:2017-05-06 Online:2017-10-20 Published:2018-01-03

Abstract: Abstract:9 degree of freedom motion simulator (9DOFMS) is the key equipment for calibration of cameratype rendezvous & docking sensor (CRDS) in spacecraft rendezvous and docking guidance navigation and control (GNC) subsystem, and it must be with high relative position precision. To meet this demand, the components of errors impacting this system’s integral indexes are analyzed systemically in this paper. At first, the relationship and interactions among the components of system errors are analyzed. Then the error model is built. By decomposing and redistributing the systematic precision index, 9DOFMS design fulfills the precision requirements.

Key words: Keywords:9 degree of freedom;motion simulator;relative position precision;error analysis, index decomposition

CLC Number: 

  • 中图分类号: V416.8