Hostname: page-component-586b7cd67f-t8hqh Total loading time: 0 Render date: 2024-11-25T02:35:23.048Z Has data issue: false hasContentIssue false
  • English
  • Français

Effective optimal control of an aircraft engine

Published online by Cambridge University Press:  04 July 2016

S. Mahmoud  and
D. McLean
S. Mahmoud
Affiliation:
Department of Transport Technology, Loughborough University
D. McLean
Affiliation:
University of Southampton
Get access Rights & Permissions [Opens in a new window]

Extract

The feasibility of using a single effective on-line control law to regulate the dynamic response of a jet engine throughout its flight envelope is of considerable importance. In this paper, a study was made to find such a single effective control law, which was able to regulate the dynamic responses of the linear, and ultimately the non-linear, model, throughout the engine’s entire operating range. This effective control law was obtained from solving a Linear Quadratic Problem (LQP) to obtain an optimal control law, a linear state feedback control.

Type
Research Article
Information
The Aeronautical Journal , Volume 95 , Issue 941 , January 1991 , pp. 21 - 27
Copyright
Copyright © Royal Aeronautical Society 1991 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Mahmoud, S. Effective Optimal Control of a Fighter Aircraft Engine, Ph.D. Thesis, Sept. 1988, Loughborough University of Technology.Google Scholar
2. Cohen, H., Rogers, G. F. C. and Saravanamuttoo, H. I. H. Gas Turbine Theory, Longman Group Ltd, 1972.Google Scholar
3. Kerrebrock, J. L. Aircraft Engines and Gas Turbines, The MIT Press, 1977.Google Scholar
4. Athans, M. and Falb, P. L. Optimal Control, McGraw-Hill, 1966.Google Scholar
5. Michael, G. J. and Farrar, F. A. An Analytical Method for the Synthesis of Non-Linear Feedback Control, NASA AD 762 797, June 1973.Google Scholar
6. Sellers, F. J. DYNGEN: A Program for Calculating Steady-State and Transient Performance of Turboject and Turbofan Engines, NASA TN D-7901, April 1975.Google Scholar