System Analyses and Autopilot Design for Automatic Roll Stabilization of a Supersonic Pilotless Aircraft (1951)
NASA Technical Reports Server (NTRS) · leaf 33
(a) 0/5a airframe frequency responses constructed graphically on semilog graph paper for the assumed extreme conditions of flight. Figure 6.- Series of graphs used to analyze the characteristics of the airframe and gyro-actuated-control roll-stabilization system.
NASA Technical Reports Server (NTRS)
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