DocumentCode :
971843
Title :
Linear time-varying eigenstructure assignment with flight control application
Author :
Lee, Ho Chul ; Choi, Jae Weon
Author_Institution :
Sch. of Mech. Eng., Pusan Nat. Univ., South Korea
Volume :
40
Issue :
1
fYear :
2004
fDate :
1/1/2004 12:00:00 AM
Firstpage :
145
Lastpage :
157
Abstract :
This work is concerned with the assignment of a desired PD-eigenstructure for linear time-varying systems. Despite its well-known limitations, gain scheduling control appeared to be a focus of the research efforts. Scheduling of frozen-time, frozen-state controllers for fast time-varying dynamics is known to be mathematically fallacious, and practically hazardous. Therefore, recent research efforts are being directed towards applying time-varying controllers. In this paper we: 1) introduce a differential algebraic eigenvalue theory for linear time-varying systems; and 2) propose a PD-eigenstructure assignment scheme via a differential Sylvester equation and a command generator tracker (CGT) for linear time-varying systems. The PD-eigenstructure assignment is utilized as a regulator. A feedforward gain for tracking control is computed by using the command generator tracker. The whole design procedures of the proposed PD-eigenstructure assignment scheme are systematic in nature. The scheme could be used to determine the stability of linear time-varying systems easily as well as to provide a new horizon of designing controllers for the linear time-varying systems. A missile flight control application is presented to validate the proposed schemes.
Keywords :
aerospace control; eigenstructure assignment; feedforward; linear systems; missile control; time-varying systems; command generator tracker; differential Sylvester equation; differential algebraic eigenvalue theory; feedforward gain; gain scheduling control; linear time-varying eigenstructure assignment; missile flight control application; time-varying dynamics; tracking control; Acceleration; Aerospace control; Aircraft; Control systems; Differential equations; Dynamic scheduling; Eigenvalues and eigenfunctions; Missiles; Stability; Time varying systems;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.2004.1292149
Filename :
1292149
Link To Document :
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