Abstract
Nine Degrees of Freedom Motion Simulator (9-DOF-MS) is the key equipment for calibration of Camera-type Rendezvous & Docking Sensor (CRDS) in spacecraft space rendezvous & docking Guidance Navigation and Control (GNC) sub-system, and it must be high with relative position precision. For meeting 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 designed fulfils the precision requirements.
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Acknowledgements
This research was funded by the Natural Science Foundation of Hebei Province of China, grant number E2019202132; the Science and Technology Research Project of Colleges and Universities of Hebei Province, grant number BJ2019049; the Science and Technology on Space Intelligent Control Laboratory, grant number 6142208200101; the Innovation Foundation Project of CAST, grant number CAST-2021-01-11; the Tianjin Key Laboratory of Micro-Low Gravity Environment Simulation Technology Open Subjects: WDZL-2020-01; and the 2021 Postgraduate Innovation Funding Project of Hebei Province of China, grant number CXZZSS2021028.
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Li, B. et al. (2023). Analysis and Decompose of Nine Degrees of Freedom Motion Simulator Relative Positional Precision. In: Zhang, H., Feng, G., Wang, H., Gu, F., Sinha, J.K. (eds) Proceedings of IncoME-VI and TEPEN 2021. Mechanisms and Machine Science, vol 117. Springer, Cham. https://doi.org/10.1007/978-3-030-99075-6_64
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DOI: https://doi.org/10.1007/978-3-030-99075-6_64
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