An investigation of the stability of a system composed of a subsonic canard airframe and a canted-axis gyroscope automatic pilot

Robert A. Gardiner, Jacob Zarovsky, H. O. Ankenbruck
naca-tn-2004
Jan 1950


An analysis has been made of the stability of a system composed of a subsonic canard airframe and a canted-axis gyroscope automatic pilot. The analysis was based on calculations of the airframe frequency response and measurements of the autopilot frequency response.

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