System Analyses and Autopilot Design for Automatic Roll Stabilization of a Supersonic Pilotless Aircraft (1951)
NASA Technical Reports Server (NTRS) · leaf 41
■fr- O … Figure 9.- Complete cycle of ramp input summation curves for the assumed extreme fli^t conditions as determined from the Fourier synthesizer. Zero time arbitrarily chosen during the cycle. Input period, 3?1^ seconds.
NASA Technical Reports Server (NTRS)
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