Basic requirements of automatic pilots applied to airplanes are defined; dynamic stability equations of airplane are given and modified relations resulting from superposition of automatic flight control requirements are developed; resulting equations establish some of boundary conditions for constants having to do with automatic pilot operation; electric automatic pilot described. (Trans)
Electric automatic pilots for aircraft
Elec Eng
Electrical Engineering ; 63 , n 11 ; p 861-866
1944
6 pages
Article (Journal)
English
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SAE | 1991
SAE | 1947