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Optimal transfer orbit trajectory using electric propulsion
Optimal transfer orbit trajectory using electric propulsion
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机译:使用电推进的最优转移轨道轨迹
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摘要
An apparatus and method for translating a spacecraft (10) from an injection orbit (16) about a central body (12) to geosynchronous orbit (18) in a time efficient manner. The spacecraft (10) includes propulsion thrusters (50) which are fired in predetermined timing sequences controlled by a controller (64) in relation to the apogee (66) and perigee (72) of the injection orbit (16) and successive transfer orbits (74, 76).
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