| 发明名称 |
SYNTHETIC GUIDE STAR FOR ON-ORBIT ASSEMBLY |
| 摘要 |
An adaptive optic system for an earth-viewing telescope on board an orbiting spacecraft includes a deformable mirror (108), a synthetic guide star laser (116), and a control module (124) that corrects not only on-axis wavefront error, but also off-axis wavefront error.
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| 申请公布号 |
WO0067061(A1) |
申请公布日期 |
2000.11.09 |
| 申请号 |
WO2000US10263 |
申请日期 |
2000.04.14 |
| 申请人 |
BALL AEROSPACE & TECHNOLOGIES CORP. |
发明人 |
FRIEDMAN, EDWARD, JAY;MCCOMAS, BRIAN, KEITH |
| 分类号 |
G01C11/00;G01S17/00;G02B26/06;G02B27/64;(IPC1-7):G02B23/00 |
主分类号 |
G01C11/00 |
| 代理机构 |
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