Author:
Srivastava Suresh,Nataraj P. S. V.,Balakrishnan S.R.
Abstract
We propose a new algorithm based on interval analysis for design of a robust first order compensator for a jet engine. The proposed algorithm generates the entire set of stabilizing controller parameters. We demonstrate the algorithm on the acceleration control loop of a jet engine in the presence of parametric uncertainties.
Reference15 articles.
1. Spang, H. A.. and Brown, H., “Control of Jet Engines”, Control Engg. Practice, 7, 1999.
2. Wright, H.E. and Hall, G.C., “Advanced Aircraft Gas Turbine Engine Controls”, Journal of Engg. for Gas Turbine and Power, 90-GT-342, vol. 112, 1991.
3. Alefeld, G. and Herzberger, J., “Introduction to Interval Computations”, Academic Press, New York, 1983.
4. Bhattacharyya, S. P., “Robust Parametric Stability: The Role of the CB Segments in [5] Control of Uncertain Dynamic Systems”, CRC Press, Littleton, MA, pp. 381-402, 1991.
5. Barmish, B. R., “New Tools for Robustness of Linear Systems”, Macmillan Publishing Company, 1994.