Application of Model-Free Control to the Operation of Post-Capture Combined Spacecraft

• Published in: Aerospace Vol. 10; no. 1; p. 90
• Main Authors: Song, Ting, Zheng, Zixuan, Guo, Yufei, Yuan, Jianping
• Format: Journal Article
• Language: English
• Published: Basel MDPI AG 01.01.2023
• Subjects: attitude and orbital operation; Attitudes; Control algorithms; Control methods; data mapping model; Design; Equations of motion; ground-based test; Mapping; model-free control; Modelling; Optimization; Orbital mechanics; Parameter estimation; Parameter identification; Robots; space debris; Space robots; Spacecraft; Spacecraft recovery; Test systems
• ISSN: 2226-4310; 2226-4310
• DOI: 10.3390/aerospace10010090

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.