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Orbital capability evaluation and trajectory reconstruction for launch vehicle with thrust decline
更新时间:2025-05-26
    • Orbital capability evaluation and trajectory reconstruction for launch vehicle with thrust decline

    • In the field of aerospace, experts have proposed a method for evaluating the orbit insertion capability and trajectory reconstruction of launch vehicles during thrust reduction based on local collocation method and neural network, providing a solution to improve the success rate of launch missions.
    • Journal of Jilin University(Engineering and Technology Edition)   Vol. 53, Issue 8, Pages: 2245-2253(2023)
    • 作者机构:

      1.南京航空航天大学 航天学院,南京 211106

      2.北京航天自动控制研究所,北京 100854

    • DOI:10.13229/j.cnki.jdxbgxb.20211120    

      CLC: V488.23
    • Received:28 October 2021

      Published:01 August 2023

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  • LI Shuang,LIN Zi-rui,YE Song,et al.Orbital capability evaluation and trajectory reconstruction for launch vehicle with thrust decline[J].Journal of Jilin University(Engineering and Technology Edition),2023,53(08):2245-2253. DOI: 10.13229/j.cnki.jdxbgxb.20211120.

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