Cessna citation X engine model identification from flight tests
During aircraft development, mathematical models are elaborated from our knowledge of
fundamental physical laws. Those models are used to gain knowledge in order to make …
fundamental physical laws. Those models are used to gain knowledge in order to make …
Development of a high-fidelity simulation model for a research environment
During aircraft development, mathematical models are elaborated from our knowledge of
fundamental physical laws. Those models are used to gain knowledge in order to make the …
fundamental physical laws. Those models are used to gain knowledge in order to make the …
Neural network adaptive controller with approximate dynamic inversion for pitch control of the Cessna Citation X
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 …
technique for designing an adaptive nonlinear controller for the pitch rate of the Cessna …
Design of a Type Two Fuzzy-based system to Control the Pitch Rate of the Cessna Citation X
View Video Presentation: https://doi. org/10.2514/6.2023-3802. vid In this research, a novel
control methodology developed at the Laboratory of Applied Research in Active Controls …
control methodology developed at the Laboratory of Applied Research in Active Controls …
Model-referenced Adaptive Flight Controller based on Recurrent Neural Network for the Longitudinal Motion of Cessna Citation X
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 …
methodology developed at the Laboratory of Applied Research in Active Controls, Avionics …
Flight control clearance of the Cessna Citation X using evolutionary algorithms
In this paper, an Aircraft Research Flight Simulator equipped with Flight Dynamics Level D
(highest level) was used to collect flight test data and develop new controller methodologies …
(highest level) was used to collect flight test data and develop new controller methodologies …
[PDF][PDF] New Methodology for Optimal Flight Control Using Differential Evolution Algorithms Applied on the Cessna Citation X Business Aircraft–Part 1. Design and …
Setting the appropriate controllers for aircraft stability and control augmentation systems are
complicated and time consuming tasks. As in the Linear Quadratic Regulator method gains …
complicated and time consuming tasks. As in the Linear Quadratic Regulator method gains …
[PDF][PDF] Identification of a Cessna Citation X aero-propulsive model in climb regime from flight tests
During aircraft development, several mathematical models are created from our knowledge
of fundamental physical laws. Those models are used in order to make decision at all …
of fundamental physical laws. Those models are used in order to make decision at all …
Application of Type One Adaptive Fuzzy Sliding Mode Control System for the Longitudinal Motion of the Cessna Citation X
View Video Presentation: https://doi. org/10.2514/6.2023-3801. vid This paper presents a
new approach developed at the Laboratory of Applied Research in Active Controls, Avionics …
new approach developed at the Laboratory of Applied Research in Active Controls, Avionics …
New Type-2-Fuzzy-Logic-Based Control System for the Cessna Citation X
This paper presents a new control law based on type-2 fuzzy logic system (T2FLS) for the
Cessna Citation X aircraft during cruise. This methodology combines three control systems …
Cessna Citation X aircraft during cruise. This methodology combines three control systems …