| Citation: | LIAN Kefei, DONG Yunfeng. Adaptive cooperative control for electromagnetic spacecraft formation flight position tracking[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(10): 2154-2162. doi: 10.13700/j.bh.1001-5965.2016.0809(in Chinese)
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Aimed at the relative position cooperative control problem of electromagnetic spacecraft formation flight, an adaptive cooperative controller was designed based on the consensus theory. Firstly, primary principles and accurate nonlinear dynamics equation of the relative motion of electromagnetic spacecraft formation were discussed. The relative motion dynamics model was then amended considering the uncertainties of the electromagnetic distant field calculation model. Secondly, nonlinear adaptive cooperative control laws for formation station tracking were designed under the condition of electromagnetic model uncertainty and communication delay among spacecraft. Solutions of magnetic moment allocation by utilizing optimization method were developed according to the difference of the maximum magnetic moments that electromagnetic spacecraft can produce. Finally, simulation shows that the adaptive cooperative controller is effective, and compared with artificial potential function method, the ability of maintaining the instantaneous stability of formation shape is improved by 4.9 times. The allocation method of magnetic moments has also achieved reasonable results.
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