| Citation: | SHI Shufeng, SHI Peng, ZHAO Yushanet al. Deorbit planning of reentry vehicles using ground track manipulation[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(10): 2141-2148. doi: 10.13700/j.bh.1001-5965.2018.0107(in Chinese)
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Aimed at the deorbit problem of reentry vehicles with constraints of reentry point location, a deorbit planning method using ground track manipulation is proposed in this paper. The deorbit trajectory design of reentry vehicles is constrained by the parameters of the real-time orbit and the aimed reentry point. First, based on the principles of orbital flight, the relationships between deorbit parameters and reentry point parameters are established with the model of impulse thrust in ellipse orbit. And the principle of thrust application for optimal deorbit is analyzed. Then, considering the influence of earth rotation and finite thrust, the necessary condition of direct deorbit is proposed. The strategy for determining deorbit location is developed with the method of nonlinear programming for the deorbit problem with latitude and longitude constraints of the reentry point. And the deorbit braking parameters conforming to the fuel optimal requirement are determined as a result. Finally, in the general case that the initial orbit does not satisfy the necessary condition of direct deorbit, the ground track manipulation method is proposed in terms of impulse thrust to satisfy the ground track constraints.
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