发明名称 |
System for high efficiency spacecraft orbit transfer |
摘要 |
The present invention relates generally to systems and methods for transferring a spacecraft from a first orbit to a second orbit. In accordance with one embodiment of the invention, the method comprises calculating thruster-off regions within an orbit transfer in which it is efficient to turn-off spacecraft thrusters, and in those thruster-off regions, turning off the spacecraft thrusters.
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申请公布号 |
US6845950(B1) |
申请公布日期 |
2005.01.25 |
申请号 |
US20030723915 |
申请日期 |
2003.11.26 |
申请人 |
LOCKHEED MARTIN CORPORATION |
发明人 |
GOODZEIT NEIL EVAN;RATAN SANTOSH |
分类号 |
B64G1/00;B64G1/40;(IPC1-7):B64G1/00 |
主分类号 |
B64G1/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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