DocumentCode
488031
Title
Maximum Principle Solutions for Time-Optimal Half-Loop Maneuvers of a High Alpha Fighter Aircraft
Author
Stalford, Harold ; Hoffman, Eric
Author_Institution
Professor, School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, Georgia 30332
fYear
1989
fDate
21-23 June 1989
Firstpage
2453
Lastpage
2458
Abstract
In this paper we present a maximum principle solution of the half-loop maneuver obtained using an analytical model for a high alpha fighter aircraft and compare it with that obtained previously using a simple nonlinear feedback control law derived from singular perturbation analysis.
Keywords
Aerodynamics; Aerospace control; Analytical models; Convergence of numerical methods; Feedback control; Interpolation; Military aircraft; NASA; Nonlinear equations; Shape;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1989
Conference_Location
Pittsburgh, PA, USA
Type
conf
Filename
4790600
Link To Document