发明名称 |
ADAPTATIVE, MULTIPLE SHOOTING OPTIMIZATION METHOD FOR DETERMINING OPTIMAL SPACECRAFT TRAJECTORIES |
摘要 |
Disclosed herein is a method for determining a trajectory for a transfer of a spacecraft from a starting space body to a target space body with respect to a given central space body, wherein the determined trajectory is optimal with respect to a given space mission requirement to be met by the transfer of the spacecraft. The method comprises providing, according to the Pontryagin maximum principle, a physical-mathematical model relating model quantities and physical quantities representing the transfer of the spacecraft with respect to the given central space body. |
申请公布号 |
EP2516272(A1) |
申请公布日期 |
2012.10.31 |
申请号 |
EP20090825639 |
申请日期 |
2009.12.24 |
申请人 |
TELESPAZIO S.P.A. |
发明人 |
BOLLE, ANDREA;CIRCI, CHRISTIAN;CORRAO, GUISEPPE |
分类号 |
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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