| Citation: | ZHANG Ran, YIN Jianfeng, HAN Chaoet al. Spacecraft forced fly-around formation design and control[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(10): 2030-2039. doi: 10.13700/j.bh.1001-5965.2016.0768(in Chinese)
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In order to meet the requirements of spacecraft fly-around technology in on-orbit service mission, spacecraft forced fly-around formation design and control scheme was investigated. Based on the analytic solution of the C-W(Clohessy-Wiltshire) equations, bi-teardrop formation was proposed. Then multi-impulse fly-around formations were developed after single-or double-impulse formations. The formula between the initial states of following spacecraft and the shape of fly-around formation was derived, and the analytic expressions of four fly-around formations and the impulse control scheme were proposed. Simulation results verify that four designed formations could be used in spacecraft slow fly-around and fast fly-around scenarios. The total fuel consumptions and distance errors of different formations were compared. Numerical results show that bi-teardrop formation has the smallest total impulse. The theory of spacecraft forced fly-around formation design and control is improved, and the results provide reference for engineering application.
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