Identification and validation of an engine performance database model for the flight management system
This Paper presents the validation studies results of an engine mathematical performance
model identification for flight management system trajectory prediction and optimization …
model identification for flight management system trajectory prediction and optimization …
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 …
Optimal input design and system identification for an agile aircraft
M Millidere - 2021 - open.metu.edu.tr
This doctorate study aims to provide a methodology for developing aerodynamic and engine
thrust models using simulated flight test data for the F16 fighter aircraft. An accurate and …
thrust models using simulated flight test data for the F16 fighter aircraft. An accurate and …
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 …
New economical cruise methodology for the cessna citation X business jet by an original morphing horizontal tail application
I. Introduction erospace industry has for goal to reduce its emissions by 50% until 2050 with
respect to emissions saved in 2005 [1]. Consequently, several alternatives allowing …
respect to emissions saved in 2005 [1]. Consequently, several alternatives allowing …
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 …