Aiming at the restriction of no-fly zone during the reentry of hypersonic glide vehicle, a reentry guidance method for avoiding no-fly zone based on IFDS algorithm is proposed . In longitudinal guidance, a predicor-corrector method is used to calculate the magnitude of bank angle. In lateral guidance, the current expected heading angle of the aircraft is calculated in a two-dimensional plane by the IFDS algorithm. Then a bank reversal logic is applied to determine the symbol of the bank angle based on the current expected heading angle. Finally, the feasibility of the algorithm to solve the no-fly zone avoidance problem is verified by a large number of simulations.


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    Titel :

    Reentry Trajectory Planning of Hypersonic Gliding Vehicle Based on IFDS Algorithm


    Weitere Titelangaben:

    Lect. Notes Electrical Eng.


    Beteiligte:
    Liu, Lianqing (Herausgeber:in) / Niu, Yifeng (Herausgeber:in) / Fu, Wenxing (Herausgeber:in) / Qu, Yi (Herausgeber:in) / Zhang, Ke (Autor:in) / Wang, Mengyang (Autor:in) / Zhang, Zhaohua (Autor:in) / Zhang, Dong (Autor:in)

    Kongress:

    International Conference on Autonomous Unmanned Systems ; 2024 ; Shenyang, China September 19, 2024 - September 21, 2024



    Erscheinungsdatum :

    09.04.2025


    Format / Umfang :

    9 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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