DocumentCode
1900332
Title
Aggressive flight maneuvers
Author
Hauser, John ; Hindman, Rick
Author_Institution
Dept. of Electr. & Comput. Eng., Colorado Univ., Boulder, CO, USA
Volume
5
fYear
1997
fDate
10-12 Dec 1997
Firstpage
4186
Abstract
We present a strategy for obtaining aggressive flight maneuvers similar to what might be produced by a pilot. We use a highly simplified aircraft model that can account for the lift/drag and thrust characteristics of an aircraft under consideration. When thrust is considered an input, this model is differentially flat (and dynamically feedback linearizable) so that the system can be made to follow any reasonable trajectory. Most trajectories will require significant movement of the throttle. Except in close formation, a pilot does not tend to make rapid throttle adjustments. Indeed, many maneuvers are accomplished using a fixed throttle position. The objective is to fly a desired path rather than a (time indexed) trajectory. Although the aircraft model with throttle fixed (thrust predetermined) is no longer differentially flat, we show that the system can still be made to follow any reasonable path. Roughly speaking, an appropriate derivative of the path parametrization variable acts as the missing control allowing flatness-like results to be obtained
Keywords
aircraft control; attitude control; differential equations; feedback; matrix algebra; aggressive flight maneuvers; differentially flat model; dynamically feedback linearizable model; fixed throttle position; lift/drag characteristics; simplified aircraft model; thrust characteristics; trajectory following; Acceleration; Aerospace control; Aerospace engineering; Aerospace simulation; Military aircraft; Path planning; Stability; Symmetric matrices; Tail; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1997., Proceedings of the 36th IEEE Conference on
Conference_Location
San Diego, CA
ISSN
0191-2216
Print_ISBN
0-7803-4187-2
Type
conf
DOI
10.1109/CDC.1997.649490
Filename
649490
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