发明名称 |
Method for orbital correction of an artificial satellite and corresponding device |
摘要 |
Orbital correction method and device for an artificial satellite. In order to stabilise the attitude of the satellite during the correction manoeuvre a polar stellar sensor 20 is used. The thrust axis 28 of the thruster 26 forms a defined angle with the pointing direction 22 of the polar sensor. Application to geostationary satellites. <IMAGE>
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申请公布号 |
FR2532911(A1) |
申请公布日期 |
1984.03.16 |
申请号 |
FR19820015301 |
申请日期 |
1982.09.09 |
申请人 |
CENTRE NAL ETUDES SPATIALES |
发明人 |
PAUL ANDRE JULES DUCHON ET JEAN-MICHEL ADRIEN MARCEL GUILBERT;GUILBERT JEAN-MICHEL ADRIEN MA |
分类号 |
B64G1/24;B64G1/36;(IPC1-7):B64G1/24 |
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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