• DocumentCode
    724442
  • Title

    Trajectories optimization of hypersonic vehicle based on a hybrid optimization algorithm of PSO and SQP

  • Author

    Linshuang Feng ; Lei Liu ; Yongji Wang

  • Author_Institution
    Nat. Key Lab. of Sci. & Technol. on Multispectral Inf. Process., Huazhong Univ. of Sci. & Technol., Wuhan, China
  • fYear
    2015
  • fDate
    23-25 May 2015
  • Firstpage
    4518
  • Lastpage
    4522
  • Abstract
    We discuss the trajectory optimization problems in the climb segment of the hypersonic vehicle in this paper. First of all, we analyze the hypersonic vehicle model. The strength of the PSO algorithm (Particle Swarm Optimization, PSO) is its strong global optimization ability, but its local optimization ability is relatively weak. The SQP algorithm (Sequential Quadratic Programming, SQP) is quite the opposite, and it has high requirements of the initial trajectory. So we propose a hybrid optimization algorithm of PSO and SQP which combine the advantages of PSO and SQP, while improving the quality of the optimal trajectory.
  • Keywords
    aircraft control; optimal control; particle swarm optimisation; quadratic programming; trajectory optimisation (aerospace); PSO algorithm; SQP algorithm; climb segment; global optimization; hybrid optimization algorithm; hypersonic vehicle model; local optimization; optimal trajectory; particle swarm optimization; sequential quadratic programming; trajectory optimization problem; Electronic mail; Particle swarm optimization; Quadratic programming; Vehicles; Hybrid optimization; Hypersonic aircraft; PSO; SQP; Trajectory optimization;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control and Decision Conference (CCDC), 2015 27th Chinese
  • Conference_Location
    Qingdao
  • Print_ISBN
    978-1-4799-7016-2
  • Type

    conf

  • DOI
    10.1109/CCDC.2015.7162721
  • Filename
    7162721