Lean backstepping design for a jet engine compressor model
- 19 November 2002
- conference paper
- Published by Institute of Electrical and Electronics Engineers (IEEE)
- p. 1047-1052
- https://doi.org/10.1109/cca.1995.555901
Abstract
Backstepping offers flexibilities not present in other nonlinear design procedures. One of them is the possibility to avoid cancellation of useful nonlinearities. Such cancellations, which are common in feedback linearization designs, require large control effort and cause nonrobustness. As an illustration of a design that avoids cancellations we develop controllers for the Moore-Greitzer model of a jet engine compressor system. The resulting backstepping controllers use less control effort than feedback linearizing controllers.Keywords
This publication has 5 references indexed in Scilit:
- Inverse Optimality in Robust StabilizationSIAM Journal on Control and Optimization, 1996
- Modeling for control of rotating stallAutomatica, 1994
- Bifurcation Analysis of Axial Flow Compressor StabilitySIAM Journal on Applied Mathematics, 1990
- Smooth stabilization implies coprime factorizationIEEE Transactions on Automatic Control, 1989
- A Theory of Post-Stall Transients in Axial Compression Systems: Part I—Development of EquationsJournal of Engineering for Gas Turbines and Power, 1986