A mathematical model of air vehicle gliding trajectory was established and attack angle was regarded as control variable. Adaptive simulated annealing algorithm was adopted to optimize the 101 nodes of attack angle. By optimizing the control law of attack angle of gliding trajectory, the maximum range of air vehicle is increased significantly, which increases 107%.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Research on Parameter Optimization Method of an Air Vehicle Gliding Trajectory



    Published in:

    Advanced Materials Research ; 945-949 ; 662-665


    Publication date :

    2014-06-06


    Size :

    4 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




    Trajectory Optimization for Hypersonic Gliding Vehicle Using Lossless Convexification

    Shi, Zhenghao / Li, Xiaosong / Zhang, Lei et al. | Springer Verlag | 2025


    Trajectory optimization for hypersonic gliding vehicle considering stochastic disturbance

    Haifeng, G. / Changqiang, H. / Dali, D. et al. | British Library Online Contents | 2014


    Direct Method for Gliding Trajectory Optimization Problem

    Chen, Wanchun / Zhou, Hao / Yu, Wenbin et al. | Springer Verlag | 2020


    Multi-objective optimization of reentry trajectory for Hypersonic Gliding Vehicle

    Ding, Dali / Guo, Haifeng / Huang, Liqiong et al. | IEEE | 2016


    Trajectory Optimization of a Subsonic Unpowered Gliding Vehicle Using Control Vector Parameterization

    Ahmad Mahmood / Fazal ur Rehman / Aamer Iqbal Bhatti | DOAJ | 2022

    Free access