中国航天（英文版）2021，Vol.22Issue(1)：20-27,8.DOI:10.3969/j.issn.1671-0940.2021.01.003
Launch Vehicle Reconfigurable Guidance Method Based on Online Trajectory Optimization
Launch Vehicle Reconfigurable Guidance Method Based on Online Trajectory Optimization
XU Guoqiang1
作者信息
- 1. Beijing Aerospace Automatic Institute,Beijing 100854
- 折叠
摘要
关键词
trajectory optimization/multiple shooting method/optimal control/NLP/launch vehicle safetyKey words
trajectory optimization/multiple shooting method/optimal control/NLP/launch vehicle safety引用本文复制引用
XU Guoqiang..Launch Vehicle Reconfigurable Guidance Method Based on Online Trajectory Optimization[J].中国航天（英文版）,2021,22(1):20-27,8.
