Chenhao Zuo1, Hongqian Zhao1, Xiaokui Yue1, Honghua Dai1,*
The International Conference on Computational & Experimental Engineering and Sciences, Vol.27, No.1, pp. 1-1, 2023, DOI:10.32604/icces.2023.09494
Abstract Dramatically increase of the amount of the failed satellites is posing a serious threat to the normal orbiting
satellites. To avoid potential collisions, it is important to remove the failed satellites, and the first step is to
detumble these uncontrolled targets. This study proposes an efficient calculation method for the failed
satellite de-tumbling system. The plasma plume generated by Hall effect thruster on chaser is used as noncontact de-tumbling medium, which reduces fuel consumption and collision risk [1]. The plasma plume is
composed of a variety of particles with strong disorder, so it is difficult to calculate the plume de-tumbling… More >
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