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Yu Song, Xinyuan Miao, Lin Cheng, Shengping Gong, The feasibility criterion of fuel-optimal planetary landing using neural networks, Aerospace Science and Technology, Volume 116, 2021, 106860, ISSN 1270-9638, https://doi.org/10.1016/j.ast.2021.106860.

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论文类型:基础研究

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上一条: Di Wu, Lin Cheng, Fanghua Jiang, Junfeng Li, Rapid generation of low-thrust many-revolution earth-center trajectories based on analytical state-based control, Acta Astronautica, Volume 187, 2021, Pages 338-347, ISSN 0094-5765, https://doi.org/10.1016/j.actaastro.2021.05.017.

下一条: Lin CHENG, Peng SHI, Shengping GONG, Zhenbo WANG, Real-time trajectory optimization for powered planetary landings based on analytical shooting equations, Chinese Journal of Aeronautics, 2021,ISSN 1000-9361, https://doi.org/10.1016/j.cja.2021.07.024.

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