Adaptive Guidance Mode system under development at Marshall Space Flight Center must be sufficiently broad to accommodate variety of vehicle configurations and missions; guidance and control system consists of four-gimbal inertial platform system with necessary items for maximum flexibility and unlimited attitude freedom, computing system capable of meeting requirements for all foreseeable missions, and analog control system that orients and stabilizes vehicle.
Saturn ascending phase guidance and control techniques
Progress Astronautics Aeronautics
1963
27 pages
Article (Journal)
English
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Saturn Ascending Phase Guidance and Control Techniques
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