DocumentCode
1729972
Title
Sliding mode control design based on Ackermann´s formula
Author
Ackermann, Jürgen ; Utkin, Vadim I.
Author_Institution
Inst. for Robotics & Syst. Dynamics, German Aerosp. Res. Establ., Wessling, Germany
Volume
4
fYear
1994
Firstpage
3622
Abstract
The sliding mode control methods are developed to design systems which have the desired dynamic behavior and are robust with respect to perturbations. It is shown that the discontinuity plane for sliding mode control may be found in an explicit form using Ackermann´s formula. Two design procedures are derived: 1) static controllers are designed to enforce sliding modes with the desired dynamic properties after a finite time interval; and 2) dynamic controllers are designed that exhibit the desired dynamic properties during the entire control process
Keywords
control system synthesis; dynamics; reduced order systems; state feedback; variable structure systems; Ackermann´s formula; design procedures; discontinuity plane; dynamic controllers; dynamics; finite time interval; reduced order systems; sliding mode control; state feedback; static controllers; Artificial intelligence; Control systems; Eigenvalues and eigenfunctions; Equations; Linear feedback control systems; Motion control; Nonlinear control systems; Sliding mode control; State feedback; Vectors;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1994., Proceedings of the 33rd IEEE Conference on
Conference_Location
Lake Buena Vista, FL
Print_ISBN
0-7803-1968-0
Type
conf
DOI
10.1109/CDC.1994.411715
Filename
411715
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