发明名称 |
Device and method for orbit determination and prediction of satellites providing signals to users |
摘要 |
<p>The invention relates to device (10) for orbit prediction of satellites comprising
- an accelerometer (12) being provided and adapted for measuring non-gravity forces acting on a satellite (14), and
- processing means (16) being adapted
-- to receive measured non-gravity forces from the accelerometer (12), to estimate the contributions of the measured non-gravity forces to the movement of the satellite (14), and
-- to predict the orbit (18) of the satellite (14) based on the estimated contributions of the non-gravity forces to the movement of the satellite (14).</p> |
申请公布号 |
EP2020381(A1) |
申请公布日期 |
2009.02.04 |
申请号 |
EP20070014887 |
申请日期 |
2007.07.30 |
申请人 |
ASTRIUM GMBH |
发明人 |
TRAUTENBERG, HANS L, DR.;KIRCHNER, MICHAEL |
分类号 |
B64G1/24;B64G1/10;B64G1/36 |
主分类号 |
B64G1/24 |
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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