The operational well-being of aircraft-engine turbine components is paramount for engine
safety. Monitoring exhaust gas temperature (EGT) serves as a key indicator of their …

A deterioration cycle model is presented, designed to consider the turbomachinery efficiency
losses that are expected during real engine in-service operations. The cycle model was …

View Video Presentation: https://doi. org/10.2514/6.2023-3797. vid This paper presents a
methodology developed at the Laboratory of Applied Research in Active Controls, Avionics …

This paper presents a methodology developed at the Laboratory of Applied Research in
Active Controls, Avionics, and Aeroservoelasticity to identify a performance model of the …

View Video Presentation: https://doi. org/10.2514/6.2023-3798. vid This paper presents a
technique for designing an adaptive nonlinear controller for the pitch rate of the Cessna …

Abstract An accurate Unmanned Aerial System (UAS) Flight Dynamics Model (FDM) allows
us to design its efficient controller in early development phases and to increase safety while …

This research presents a technique for designing an adaptive nonlinear controller for the
pitch rate of the Cessna Citation X business jet aircraft. The proposed control algorithm …

This work outlines a method for designing an adaptive nonlinear controller for the lateral
control of the Cessna Citation X business aircraft. The objective of the proposed controller is …

A local scale Aerothermodynamic Generic Cycle Model (AGCM) is proposed. The AGCM
accounts for several improvements not considered in similar models, such as compressor …

Purpose This study aims to present the concept of aircraft turbofan engine health status
prediction with artificial neural network (ANN) pattern recognition but augmented with …