Accession Number : ADD007958
Title : Control Augmentation System for Flight Vehicles.
Descriptive Note : Patent,
Corporate Author : DEPARTMENT OF THE ARMY WASHINGTON DC
Personal Author(s) : Murray,James B
Report Date : 15 Apr 1980
Pagination or Media Count : 6
Abstract : This invention relates to a control augmentation system for stabilization and control of flight vehicles, wherein control of vehicle angular velocities in proportion to control input is effected, and where stabilization of the corresponding vehicle attitude is also effected. The system consists of both feedforward and feedback signal paths. The feedback paths provide augmentation of the vehicle's inherent stability. The feedforward paths augment the controllability factors available to the pilot. The control augmentation system is a solution to hingeless rotor control problems.
Descriptors : *Patents, *Flight control systems, Augmentation, Attitude control systems, Hydraulic servomechanisms, Control sticks, Stabilization systems, Feedback, Attack helicopters
Subject Categories : Flight Control and Instrumentation
Hydraulic and Pneumatic Equipment
Distribution Statement : APPROVED FOR PUBLIC RELEASE