Trajectory Design of Launch Vehicle with the Argument of Perigee Constraint for Highly Eccentric Orbit Mission

AEROSPACE CHINA

中国航天科技集团有限公司主管

中国航天系统科学与工程研究院主办

ISSN 1671-0940

CN 11-4673/V

English 中文版

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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 , ZHANG Weidong , WANG Ying , LIU Chang , SHEN Zili

AEROSPACE CHINA . 2020, (3): 5 -12 . DOI: 10.3969/j.issn.1671-0940.2020.03.001