| Citation: | BEN Liyan, YAN Lingling, XIE Xianghua, et al. Design of Moon-to-Earth transfer orbit with direct atmospheric reentry[J]. Journal of Beijing University of Aeronautics and Astronautics, 2020, 46(2): 287-293. doi: 10.13700/j.bh.1001-5965.2019.0194(in Chinese)
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A new solution algorithm for the design of Moon-to-Earth transfer orbit which leaves from the Moon parking orbit with direct atmospheric reentry and single impulse is presented in this paper. The algorithm is divided into two steps, designing the initial solution and searching the exact solution. First, according to the constraint conditions, the high-precision initial solution is generated by simple iteration using pseudostate theory. Then, the real orbit and state transition matrix are calculated by numerical integration in the real dynamic model, and the exact solution is found by the differential correction method. Because the initial solution with high accuracy is used, the difficulty of finding the solution for the design of Moon-to-Earth transfer orbit is greatly reduced. Numerical simulations indicate that the algorithm is of high efficiency and good robustness.
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