In addition to the launch phase optimization, the trajectory optimization of the Reusable Launch Vehicle (RLV) includes the optimization of the booster landing phase. Due to the coupling relationship between the launch trajectory and the landing trajectory, it is difficult to solve a multi-phase trajectory optimization problem of RLV. To overcome the above challenge, this paper proposes a Phase-rendezvous Approach (PRA) which reconstructs the original multi-phase optimization problem to obtain the optimal solution and takes the VTVL multi-phase trajectory optimization problem as an example to carry out optimization calculations. The calculation results show that PRA successfully solves multi-phase trajectory optimization problem of RLV.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    A Phase-Rendezvous Approach for Multi-phase Trajectory Optimization of Reusable Launch Vehicle


    Weitere Titelangaben:

    Lect. Notes Electrical Eng.


    Beteiligte:
    Yan, Liang (Herausgeber:in) / Duan, Haibin (Herausgeber:in) / Yu, Xiang (Herausgeber:in) / Gao, Yan (Autor:in) / Shao, Zhijiang (Autor:in) / Song, Zhengyu (Autor:in)


    Erscheinungsdatum :

    30.10.2021


    Format / Umfang :

    17 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    A Phase-Rendezvous Approach for Multi-phase Trajectory Optimization of Reusable Launch Vehicle

    Gao, Yan / Shao, Zhijiang / Song, Zhengyu | British Library Conference Proceedings | 2022


    Trajectory Optimization for the Vertical Landing Phase of Reusable Launch Vehicles Via Convex Approach

    Li, Yuan / Shi, Linan / Chen, Ping et al. | British Library Conference Proceedings | 2022