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System Analyses and Autopilot Design for Automatic Roll Stabilization of a Supersonic Pilotless Aircraft (1951)

NASA Technical Reports Server (NTRS) · leaf 37

An illustration from System Analyses and Autopilot Design for Automatic Roll Stabilization of a Supersonic Pilotless Aircraft, 1951, leaf 37
(b) System open-loop frequency responses on M-N contour chart. Closed- loop contours (other than 0 db) omitted. Figure 7*- Continued.

NASA Technical Reports Server (NTRS)

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