发明名称 |
Compact, lightweight central position guiding plant, e.g. for orbiting missile or spacecraft, includes core structure with accelerometer(s), gyroscope(s), mirrors and Cassegrain telescope as star viewer |
摘要 |
<p>In a central position guiding plant for a moving machine, having a core structure (2) with accelerometer(s) (A3) and gyroscope(s) (G1) and a star viewer, the core structure consists of a single rigid element traversed by a bore (9). A primary mirror (22) and an electro-optical detector (26) for the viewer are fixed at one end (19) of the bore; and a secondary mirror (18) is fixed at the other end (13). The star viewer is in the form of a Cassegrain telescope. In a central position guiding plant for a moving machine, having a core structure (2) with accelerometer(s) (A3) and gyroscope(s) (G1) (optionally supported on cardan structures) and a star viewer, the core structure consists of a single rigid element traversed by a bore (9). A primary mirror (22) and an electro-optical detector (26) for the star viewer (behind an opening (23)) are fixed at one end (19) of the bore; and a secondary mirror (18) is fixed at the other end (13). The star viewer is in the form of a Cassegrain telescope. Fixing plates (16) are provided on the core structure for the accelerometers, gyroscopes etc. and an electronic actuator for the detector.</p> |
申请公布号 |
FR2886724(A1) |
申请公布日期 |
2006.12.08 |
申请号 |
FR19860000289 |
申请日期 |
1986.01.10 |
申请人 |
SAGEM SA SOCIETE ANONYME |
发明人 |
GODART DIDIER;DEFFONTAINE CHRISTOPHE;DAUSSY CHRISTOPHE |
分类号 |
G01C19/00;F42B15/01;G01C21/18;G05D1/12 |
主分类号 |
G01C19/00 |
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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