Tracking of Twin Spool Gas Turbine Using Reduced Output Feedback Sliding Mode Control
Authors:
- Rajesh TiwariRTRajesh Tiwari
- S. JanardhananSJS. Janardhanan
- 1 July 2011
- conference paper
- Published by Institute of Electrical and Electronics Engineers (IEEE)
- p. 1-5
Abstract
Twin spool gas turbine engine which is the integral part of the avionics, is a non linear higher order multi input multi output (MIMO) system. Design of tracking controller for turbine engine with the classical techniques is a tedious task and implementation of the complex controller is also an issue. The Basic philosophy of this paper is to design a sliding mode controller with model order reduction. Implementation of this designed tracking controller on the original system is easier due to reduced controller complexity.Keywords
This publication has 11 references indexed in Scilit:
- Sliding mode control design via reduced order model approachInternational Journal of Automation and Computing, 2007
- An Integral Sliding Model Tracking Strategy for 3D Laser Beam Position ControlThe International Journal of Advanced Manufacturing Technology, 2001
- Variable structure control with sliding sectorAutomatica, 2000
- A control engineer's guide to sliding mode controlIEEE Transactions on Control Systems Technology, 1999
- A New Algorithm for Compensator Design for Higher-Order System via Reduced ModelAutomatica, 1998
- Output feedback sliding mode designfor linear uncertainsystemsIEE Proceedings - Control Theory and Applications, 1997
- Output feedback variable structure control designAutomatica, 1995
- Variable structure control: a surveyIEEE Transactions on Industrial Electronics, 1993
- Suboptimal control of linear systems via simplified models of ChidambaraProceedings of the Institution of Electrical Engineers, 1974
- A method for simplifying linear dynamic systemsIEEE Transactions on Automatic Control, 1966