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

AEROSPACE CHINA

Sponsored by

China Aerospace Science and Technology Corporation

Published by

China Aerospace Academy of Systems Science and Engineering

ISSN 1671-0940

CN 11-4673/V

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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