New approach to problem of designing intercoupled multiloop control systems; method illustrated by design of fully automatic air-speed-altitude control for Northrop F-61C airplane; by satisfying requirement that thrust and pitch attitude be controlled in cordination, method allows separate design of air speed and altitude control functions.
Design method for automatic longitudinal control systems
Aeronautical Eng Rev
Aeronautical Engineering Review ; 10 , n 1
1951
6 pages
Aufsatz (Zeitschrift)
Englisch
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