Mechanization of pitch control system; its design analyzed in nondimensional form; changes in static stability; effect of fuselage bending; location of gyro elements in aircraft; ability of control system to minimize effect of gust interference.
Recent developments in aircraft control
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 22 , n 3
1955
20 pages
Aufsatz (Zeitschrift)
Englisch
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