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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    Title :

    Reentry Trajectory Planning of Hypersonic Gliding Vehicle Based on IFDS Algorithm


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Liu, Lianqing (editor) / Niu, Yifeng (editor) / Fu, Wenxing (editor) / Qu, Yi (editor) / Zhang, Ke (author) / Wang, Mengyang (author) / Zhang, Zhaohua (author) / Zhang, Dong (author)

    Conference:

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



    Publication date :

    2025-04-09


    Size :

    9 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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