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.
Linear time-varying eigenstructure assignment with flight control application
IEEE Transactions on Aerospace and Electronic Systems ; 40 , 1 ; 145-157
2004
13 Seiten, 32 Quellen
Article (Journal)
English
Linear Time-Varying Eigenstructure Assignment with Flight Control Application
Online Contents | 2004
|British Library Conference Proceedings | 2002
|Robust Multirate Eigenstructure Assignment with Flight Control Application
British Library Conference Proceedings | 1994
|Robust Multirate Eigenstructure Assignment with Flight Control Application
Online Contents | 1995
|