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• W4316804900 abstract "A model-free control method is applied to the attitude and orbital operation of the post-capture combined spacecraft, which consists of a space robot and debris. The main contribution of this paper lies in the following three aspects. Firstly, the discrete dynamic linearization method of the motion equation for a post-capture combined spacecraft is proposed, and then, the standardized expression form of multiple input and multiple output system for the attitude and orbital dynamics motions of post-capture combined spacecraft are presented. Secondly, the data mapping model of the post-capture combined spacecraft is defined, and based on this, an initial value online optimization method for the data mapping model is provided, which is key for the convergence of model-free control. Finally, a test system based on the ground-based three-axis spacecraft simulator is built to simulate the attitude and orbital operation of post-capture combined spacecraft, and the experimental system is implemented to verify the validation of the model-free control method proposed in this paper. The results show that the model-free control has a good control effect on the attitude and orbit of the post-capture combined spacecraft, even if the configuration of the spacecraft is time-varying." @default.
• W4316804900 created "2023-01-17" @default.
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• W4316804900 date "2023-01-16" @default.
• W4316804900 modified "2023-09-30" @default.
• W4316804900 title "Application of Model-Free Control to the Operation of Post-Capture Combined Spacecraft" @default.
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• W4316804900 doi "https://doi.org/10.3390/aerospace10010090" @default.
• W4316804900 hasPublicationYear "2023" @default.
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