The principle of 'tilted effect' of the narrow interference filter is described and the laser sensor system which described how to measure attitude angles of the target spacecraft by the principle is presented. The result of laboratory experiment and error analysis are given. The experiment illustrated that it is practical to use the laser sensor system as the sensor for rendezvous and docking.
Laser Sensor for Rendezvous and Docking of Spacecraft
1991
3 pages
Report
No indication
English
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