DocumentCode
2299318
Title
The propulsive-only flight control problem
Author
Biezad, Daniel J.
Author_Institution
Cal Poly State Univ., San Luis Obispo, CA
fYear
1991
fDate
20-24 May 1991
Firstpage
494
Abstract
Attitude control of aircraft using only the throttles is investigated. The long time constants of both the engines and the aircraft dynamics, together with the coupling between longitudinal and lateral aircraft modes, make piloted flight with failed control surfaces hazardous, especially when trying to land. The author documents the results of in-flight operation using simulated failed flight controls and ground simulations of piloted propulsive-only control to touchdown. Augmentation control laws to assist the pilot are described using both optimal control and classical feedback methods. Piloted simulation using augmentation shows that simple and effective augmented control can be achieved in a wide variety of failed configurations
Keywords
aerospace propulsion; aerospace simulation; aircraft; attitude control; feedback; optimal control; aerospace propulsion; aircraft dynamics; aircraft engine; augmented control; coupling; feedback; ground simulations; in-flight operation; optimal control; piloted flight; propulsive-only flight control; throttles; Aerospace control; Aerospace simulation; Aircraft propulsion; Control systems; Engines; Feedback; Geometry; Military aircraft; Optimal control; Stress control;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace and Electronics Conference, 1991. NAECON 1991., Proceedings of the IEEE 1991 National
Conference_Location
Dayton, OH
Print_ISBN
0-7803-0085-8
Type
conf
DOI
10.1109/NAECON.1991.165797
Filename
165797
Link To Document