Review of basic design parameters which largely determine functional and hardware design of flight control system of any manned spacecraft, namely, vehicle type, mission duration, mission objective, vehicle weight, and method of thermal equipment control; X-20 flight control system for delta-winged orbital glider; Apollo's command module's stabilization and control system (SCS); its control functions and elements; flight control for orbital stations; future control systems.
Flight control for manned spacecraft
Space/Aeronautics
Space/Aeronautics ; 40 , n 6
1963
9 pages
Article (Journal)
English
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