Integration of suitable flight controls into X-15 was task of using analytical methods of flight dynamics and analog computing equipment and flight-control simulators to formulate system providing satisfactory control characteristics throughout flight envelope; operating characteristics of rate command, tandem, single motor, and solenoid bypass system; evaluation of proposed configuration and block diagram showing final solenoid bypass system; rate damping integrated. (p 36-37, 74, 76, 78, 80)
Systems approach to flight controls
Astronautics
Astronautics ; 7 , n 5
1962
Aufsatz (Zeitschrift)
Englisch
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A systems approach to flight controls
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