Modelling and Control of Aircraft Gas Turbine Engines

[摘要] In this thesis the main theme is to demonstrate the potential performance improvements of gas turbine engines that are brought about by using multivariable control systems. Particular emphasis is on designing such control systems using the well-established engine thermodynamic models since these models are considered as the true representations of engine thermodynamic process and enable engine variable geometry features to be easily incorporated and their effects studied.

[发布机构] University:University of Glasgow

[关键词] Mechanical engineering, Aerospace engineering