DocumentCode
3268065
Title
A study of longitudinal flight maneuvers for the CTOL aircraft model
Author
Al-Hiddabi, Saif A. ; McClamroch, N. Harris
Author_Institution
Dept. of Aerosp. Eng., Michigan Univ., Ann Arbor, MI, USA
Volume
2
fYear
1999
fDate
1999
Firstpage
1199
Abstract
We study several flight control problems for a conventional aircraft take off and landing (CTOL) flight control model, a simplified model for aircraft longitudinal flight dynamics. In particular, we study the execution of a maneuver for which the aircraft is intended to follow a path in a vertical plane corresponding to specified change in altitude. We formulate the problem as a nonlinear tracking control problem. Controllers are developed for two cases: a non-aggressive maneuver, corresponding to a small altitude change, and an aggressive maneuver, corresponding to a large altitude change. We demonstrate the need to develop a controller that includes feedforward terms in order to achieve aggressive maneuvering. Our approach throughout is to make use of nonlinear control theory, which is complicated by the non-minimum phase characteristics of the CTOL model
Keywords
aircraft control; closed loop systems; dynamics; feedback; feedforward; nonlinear control systems; CTOL aircraft model; flight control; longitudinal flight maneuvers; nonaggressive maneuver; nonlinear tracking control problem; nonminimum phase characteristics; vertical plane; Aerodynamics; Aerospace control; Aircraft propulsion; Control design; Control systems; Control theory; Drag; Equations; Liquid crystal on silicon; Motion control;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Applications, 1999. Proceedings of the 1999 IEEE International Conference on
Conference_Location
Kohala Coast, HI
Print_ISBN
0-7803-5446-X
Type
conf
DOI
10.1109/CCA.1999.801143
Filename
801143
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