Abstract
The parameter identification method for inertial parameters of the base and link on a free-flying space robot is studied according to the angular momentum conservation equation. Firstly, the base and joints of the links are respectively excited with the cubic polynomial trajectory, and then their dynamic parameters are identified using the nonlinear least square algorithm, so that the results of the simulation are effectively proven by the method.
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Acknowledgment
This work is supported by the project of defense preresearch (2009SY4104002, 2010SY4106007) and 863(2008AA1088).
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Jianjun, S., Xiaoping, D., Chao, W., Qiao, W., Xin, L., Yu, J. (2012). Mass Characteristic Parameter Identification for a Space Robot Based on Angular Momentum Conservation. In: Chen, R. (eds) 2011 International Conference in Electrics, Communication and Automatic Control Proceedings. Springer, New York, NY. https://doi.org/10.1007/978-1-4419-8849-2_43
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DOI: https://doi.org/10.1007/978-1-4419-8849-2_43
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