发明名称 |
Efficient orbit sparing system for space vehicle constellations |
摘要 |
A sparing system for space vehicle constellations. A plurality of space vehicles arranged in at least one mission orbit plane. The number of space vehicles is at least one greater than a minimum number necessary to provide at least a minimum level of service necessary to carry out a constellation mission. If one of the space vehicles fails the remaining space vehicles are repositioned in the mission orbit plane to provide the minimum level of service necessary to carry out a constellation mission.
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申请公布号 |
US7051980(B2) |
申请公布日期 |
2006.05.30 |
申请号 |
US20030374750 |
申请日期 |
2003.02.25 |
申请人 |
LOCKHEED MARTIN CORPORATION |
发明人 |
GOODZEIT NEIL EVAN;LEMPKE JAMES DONALD |
分类号 |
B64G1/10;B64G1/24 |
主分类号 |
B64G1/10 |
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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