| Citation: | LIAO Xiang, ZHENG Jing, XU Yongsheng, et al. Precise references orbit design of miniSAR satellite[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(12): 2442-2449. doi: 10.13700/j.bh.1001-5965.2021.0141(in Chinese)
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In order to meet the requirements of the mini synthetic aperture radar (miniSAR) satellite interferometry mission for the space baseline, a set of precision reference orbit design algorithms was established by analyzing the features of the satellite reference orbit. The algorithm takes a group of orbit determination data after the successful orbit insertion of the miniSAR satellite and the estimation elements of reference orbit obtained by analyzing the reference orbit features as inputs. The Eckstein-Hechler mean elements model and nested iterative correction method are used to design and output the reference orbit within the mission duration. Numerical simulation shows that the spatial regression accuracy of the reference trajectory formed by the algorithm is better than 0.01 m, which can be applied to real engineering application.
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