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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Main Authors | , , , , , , , |
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Format | Patent |
Language | Chinese English |
Published |
19.07.2019
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Subjects | |
Online Access | Get full text |
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