Rocket upper stage optimal accessible orbit rapid planning calculation method

The invention discloses a rocket upper stage optimal accessible orbit rapid planning calculation method. The method comprises the following steps: firstly, acquiring upper stage maneuvering-before initial state information; secondly, calculating the number of orbits of satellite injection after mane...

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Bibliographic Details
Main Authors WANG BAOHUA, SHEN HONGXIN, ZHANG ZHIBIN, HUANG ANYI, LI ZHAO, DAN PENG, LI HENGNIAN, ZHANG TIANJIAO
Format Patent
LanguageChinese
English
Published 19.07.2019
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