DocumentCode
326863
Title
Recovery guidance for linear systems with input and state constraints
Author
Devasia, Santosh ; Meyer, George
Author_Institution
Dept. of Mech. Eng., Utah Univ., Salt Lake City, UT, USA
Volume
2
fYear
1998
fDate
21-26 Jun 1998
Firstpage
1122
Abstract
When a fixed regulator is used to stabilize a desired state trajectory (guidance law), large initial tracking errors can lead to input saturation, which can result in performance deterioration. A method to modify the guidance law for recovering state-trajectory tracking (without violating input and state constraints) is presented. Although it may be feasible to find such a satisfactory recovery guidance manoeuvre for a given initial tracking error, online development of recovery guidance manoeuvres may not be computationally tractable. A technique is developed to use precomputed recovery guidance manoeuvres (for a finite set of initial tracking errors) to generate recovery guidance manoeuvres for other initial errors
Keywords
aircraft navigation; feedback; feedforward; linear systems; optimal control; tracking; aircraft guidance; feedback; feedforward; initial errors; linear systems; optimal control; recovery guidance; state constraints; state-trajectory tracking; tracking errors; Actuators; Automatic generation control; Control systems; Error correction; Feedback; Linear systems; Mechanical engineering; NASA; Regulators; Trajectory;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1998. Proceedings of the 1998
Conference_Location
Philadelphia, PA
ISSN
0743-1619
Print_ISBN
0-7803-4530-4
Type
conf
DOI
10.1109/ACC.1998.703586
Filename
703586
Link To Document