Description of spacecraft configuration, inertial guidance subsystem -- inertial measurement unit and digital computer, and attitude control subsystem; crew-station instrumentation; navigation, prediction and steering; maneuver-capability footprint.
Gemini reentry guidance and control system
Joint Automatic Control Conference
7th Joint Automatic Control Conference ; 1966 ; United States , Seattle, WA Re-entry
1966
6 pages
Conference paper
English
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NTRS | 1965
|Gemini - Guidance and control.
NTRS | 1966
|Engineering Index Backfile | 1965
|