Reentry Trajectory Optimization for a Hypersonic Vehicle Based on an Improved Adaptive Fireworks Algorithm

被引:11
|
作者
Wei, Xing [1 ]
Liu, Lei [1 ]
Wang, Yongji [1 ]
Yang, Ye [2 ]
机构
[1] HUST, Sch Automat, Natl Key Lab Sci & Technol Multispectral Informat, Wuhan 430074, Hubei, Peoples R China
[2] Beijing Aerosp Automat Control Inst, Beijing 100854, Peoples R China
关键词
GLOBAL OPTIMIZATION;
D O I
10.1155/2018/8793908
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Generation of optimal reentry trajectory for a hypersonic vehicle (HV) satisfying both boundary conditions and path constraints is a challenging task. As a relatively new swarm intelligent algorithm, an adaptive fireworks algorithm (AFWA) has exhibited promising performance on some optimization problems. However, with respect to the optimal reentry trajectory generation under constraints, the AFWA may fall into local optimum, since the individuals including fireworks and sparks are not well informed by the whole swarm. In this paper, we propose an improved AFWA to generate the optimal reentry trajectory under constraints. First, via the Chebyshev polynomial interpolation, the trajectory optimization problem with infinite dimensions is transformed to a nonlinear programming problem (NLP) with finite dimension, and the scope of angle of attack (AOA) is obtained by path constraints to reduce the difficulty of the optimization. To solve the problem, an improved AFWA with a new mutation strategy is developed, where the fireworks can learn from more individuals by the new mutation operator. This strategy significantly enhances the interactions between the fireworks and sparks and thus increases the diversity of population and improves the global search capability. Besides, a constraint-handling technique based on an adaptive penalty function and distance measure is developed to deal with multiple constraints. The numerical simulations of two reentry scenarios for HV demonstrate the validity and effectiveness of the proposed improved AFWA optimization method, when compared with other optimization methods.
引用
收藏
页数:17
相关论文
共 50 条
  • [21] Reentry trajectory optimization for hypersonic vehicle satisfying complex constraints
    Jiang Zhao
    Rui Zhou
    Chinese Journal of Aeronautics , 2013, (06) : 1544 - 1553
  • [22] Reentry trajectory rapid optimization for hypersonic telescopic deformable vehicle
    Yue C.
    Tang S.
    Guo J.
    Wang X.
    Zhang H.
    Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics, 2021, 43 (08): : 2232 - 2243
  • [23] Trajectory optimization for cooperative reentry of multiple hypersonic glide vehicle
    Jiang P.
    Guo D.
    Han L.
    Li Q.
    Ren Z.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2020, 41
  • [24] An Effective TLBO-Based Memetic Algorithm for Hypersonic Reentry Trajectory Optimization
    Qu, Xinghua
    Li, Huifeng
    Zhang, Ran
    Liu, Bo
    2016 IEEE CONGRESS ON EVOLUTIONARY COMPUTATION (CEC), 2016, : 3178 - 3185
  • [25] Reentry Trajectory Optimization of Powered Hypersonic Vehicle for Improving Range based on Discontinuous Ignition
    Lin, Jun
    He, Yingzi
    Wang, Zhi
    Zhao, Jiang
    2020 CHINESE AUTOMATION CONGRESS (CAC 2020), 2020, : 4445 - 4450
  • [26] Multi-objective Optimization of Reentry Trajectory for Hypersonic Gliding Vehicle
    Ding Dali
    Guo Haifeng
    Huang Liqiong
    Wang Yuan
    2016 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC), 2016, : 1436 - 1443
  • [27] Reentry Trajectory Optimization for Hypersonic Glide Vehicle with Flexible Initial Conditions
    Dong, Chunyun
    Cai, Yuanli
    JOURNAL OF AEROSPACE ENGINEERING, 2017, 30 (05)
  • [28] Hypersonic reentry trajectory optimization by using improved sparrow search algorithm and control parametrization method
    Hui, Xu
    Guangbin, Cai
    Shengxiu, Zhang
    Xiaogang, Yang
    Mingzhe, Hou
    ADVANCES IN SPACE RESEARCH, 2022, 69 (06) : 2512 - 2524
  • [29] Fast Optimization of Glide Vehicle Reentry Trajectory Based on Genetic Algorithm
    Jia Jun
    Dong Ruixing
    Yuan Xuejun
    Wang Chuangwei
    FOURTH SEMINAR ON NOVEL OPTOELECTRONIC DETECTION TECHNOLOGY AND APPLICATION, 2018, 10697
  • [30] Ascent Trajectory Optimization for Hypersonic Vehicle Based on Improved Chicken Swarm Optimization
    Fu, Wenzhe
    Wang, Bo
    Li, Xu
    Liu, Lei
    Wang, Yongji
    IEEE ACCESS, 2019, 7 : 151836 - 151850