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Trigonometric Regularization and Continuation Method Based Time-Optimal Control of Hypersonic Vehicles

LIN Yujie HAN Yanhua

Transactions of Nanjing University of Aeronautics and Astronautics2024，Vol.41Issue(S01)：P.52-59,8.

Transactions of Nanjing University of Aeronautics and Astronautics2024，Vol.41Issue(S01)：P.52-59,8.DOI:10.16356/j.1005-1120.2024.S.007

Trigonometric Regularization and Continuation Method Based Time-Optimal Control of Hypersonic Vehicles

LIN Yujie ¹HAN Yanhua¹

作者信息

1. College of Astronautics,Nanjing University of Aeronautics and Astronautics,Nanjing 211106,P.R.China
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摘要

关键词

hypersonic vehicle(HSV)/optimal control/trigonometric regularization method(TRM)/continuation method

分类

航空航天

引用本文复制引用

LIN Yujie,HAN Yanhua..Trigonometric Regularization and Continuation Method Based Time-Optimal Control of Hypersonic Vehicles[J].Transactions of Nanjing University of Aeronautics and Astronautics,2024,41(S01):P.52-59,8.

基金项目

supported by the Na-tional Natural Science Foundation of China(No.52272369). （No.52272369）

Transactions of Nanjing University of Aeronautics and Astronautics

OACSTPCD

ISSN：1005-1120

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