On-line performance optimisation of aero engine control system.

DOI10.1016/S0005-1098(03)00224-3zbMath1044.93050OpenAlexW1985098397MaRDI QIDQ1421449

O. D. Lyantsev, G. G. Kulikov, T. V. Breikin, V. Yu. Arkov

Publication date: 26 January 2004

Published in: Automatica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s0005-1098(03)00224-3

zbMATH Keywords

numerical algorithmsaero engine optimal controlfuel flowon-line performance optimizationoutput nozzle areaspecific fuel consumption

Mathematics Subject Classification ID

Numerical mathematical programming methods (65K05) Application models in control theory (93C95) Design techniques (robust design, computer-aided design, etc.) (93B51)

Related Items (1)

Application of Markov chains to identification of gas turbine engine dynamic models

Cites Work

• Linear-quadratic Gaussian with loop-transfer recovery methodology for the F-100 engine

This page was built for publication: On-line performance optimisation of aero engine control system.