The feasibility of an autonomous video guidance system that is capable of observing a planetary surface during terminal descent and selecting the most acceptable landing site was demonstrated. The system was breadboarded and "flown" on a physical simulator consisting of a control panel and monitor, a dynamic simulator, and a PDP-9 computer. The breadboard VGLIS consisted of an image dissector camera and the appropriate processing logic. Results are reported.
Video Guidance, Landing, and Imaging system (VGLIS) for space missions
1975-02-01
Report
Keine Angabe
Englisch
Video guidance, landing, and imaging systems
NTRS | 1975
|Video Guidance, Landing, and Imaging Systems
NTIS | 1975
|Variable point guidance for space missions
AIAA | 1964
|Variable point guidance for space missions.
AIAA | 1966
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