Accession Number : AD0164876
Title : Stability Augumentation System for Light Aircraft Providing Pilot Assist and Turn.
Descriptive Note : Patent,
Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C
Personal Author(s) : Knemeyer,Siegfried
Report Date : 01 MAY 1973
Pagination or Media Count : 8
Abstract : The patent concerns a conventional stability augmentation system for automatically maintaining a wings level constant heading attitude. The system is provided with a switch on the control wheel which introduces an offset signal into the stability augmentation system causing the system to produce and stabilize on a turn rate determined by the magnitude of the offset signal.
Descriptors : *Patents, *Flight control systems, *Turning flight, Stabilization systems, Switches
Subject Categories : Aircraft
Distribution Statement : APPROVED FOR PUBLIC RELEASE