Linear model of 2-shaft turbojet and its properties

• 1 January 1971
• journal article
• Published by Institution of Engineering and Technology (IET) in Proceedings of the Institution of Electrical Engineers
• Vol. 118  (6) , 813-815
• https://doi.org/10.1049/piee.1971.0160

Abstract

Keywords

• FEEDBACK LOOPS STABLE CONFIGURATION
• PARTIALLY EXPERIMENTAL METHOD
• OBSERVABILITY
• NUMERICAL MODEL PARAMETERS
• AIRCRAFT ENGINES
• NONLINEAR SYSTEMS
• STABILITY CONDITIONS
• MULTIVARIABLE SYSTEMS
• POINTWISE STATE
• LEFT HALFPLANE
• GAS TURBINES
• THEORETICAL APPROACH
• LINEAR MODEL DEVELOPMENT
• 2-SHAFT TURBOJETS