System Analyses and Autopilot Design for Automatic Roll Stabilization of a Supersonic Pilotless Aircraft (1951)
NASA Technical Reports Server (NTRS) · leaf 28
NACA RM L51E07 27 … (a) Comparison of airframe 0/&a frequency responses for varj'ing ■-x- M = 2.5; altitude^ 40,000 feet; estimated value of LM. Figure 3.- Nyquist diagrams of airframe frequency responses for inertia-. aerodynamic-, and flight-parameter changes.
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
