Trajectory optimization for hypersonic gliding vehicle considering stochastic disturbance

被引:0
作者
Guo, Haifeng [1 ]
Huang, Changqiang [1 ]
Ding, Dali [1 ]
Xiao, Hong [1 ]
机构
[1] Aeronautics and Astronautics Engineering College, Air force Engineering University, Xi'an
来源
Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics | 2014年 / 40卷 / 09期
关键词
Disturbance; Generalized polynomial chaos; Gliding; Hypersonic; Reentry; Stochastic; Trajectory optimization;
D O I
10.13700/j.bh.1001-5965.2013.0755
中图分类号
学科分类号
摘要
To solve the problem of the reentry trajectory optimization for the hypersonic gliding vehicle with stochastic disturbance, the numerical method of trajectory optimization based on the generalized polynomial chaos was put forward. The sampling space was formed by the sampling of stochastic variable using generalized polynomial chaos. The space of the observations came into being after putting every sampling value into solving the problem of the deterministic trajectory optimization iteratively. The expected value, variance and covariance were computed and the outputs were approximated. The simulation of maximizing the downrange angle of the reentry trajectory optimization for the hypersonic gliding vehicle with stochastic disturbance was carried out based on this method. The results of the simulation indicate that the method could solve the problem of trajectory optimization with stochastic disturbance, and the computational efficiency was improved greatly contrasted with the Monte Carlo method.
引用
收藏
页码:1281 / 1290
页数:9
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