中国航天（英文版）2020，Vol.21Issue(3)：5-12,8.DOI:10.3969/j.issn.1671-0940.2020.03.001
Trajectory Design of Launch Vehicle with the Argument of Perigee Constraint for Highly Eccentric Orbit Mission
Trajectory Design of Launch Vehicle with the Argument of Perigee Constraint for Highly Eccentric Orbit Mission
FENG Jihang 1ZHANG Weidong 2WANG Ying 1LIU Chang 1SHEN Zili1
作者信息
- 1. Shanghai Institute of Aerospace System Engineering, Shanghai 201109
- 2. Shanghai Academy of Spaceflight Technology, Shanghai 201109
- 折叠
摘要
关键词
launch vehicle/highly eccentric orbit/constrain of argument of perigee/trajectory designKey words
launch vehicle/highly eccentric orbit/constrain of argument of perigee/trajectory design引用本文复制引用
FENG Jihang,ZHANG Weidong,WANG Ying,LIU Chang,SHEN Zili..Trajectory Design of Launch Vehicle with the Argument of Perigee Constraint for Highly Eccentric Orbit Mission[J].中国航天（英文版）,2020,21(3):5-12,8.
