Now showing items 1-4 of 4
Aerodynamic model development and simulation of airliner spin for upset recovery
(EDP Sciences, 2013-06)
The aerodynamic model of a generic airliner configuration is developed for a wide range of angles of attack, sideslip and angular rate based on experimental data obtained in wind tunnels using static, forced oscillations ...
Investigation of Attainable Equilibrium Sets for Clearance of Flight Control Laws
(American Institute of Aeronautics and Astronautics, AIAA, 2010-01)
A systematic investigation of aircraft equilibrium states and their local stability characteristics is used for clearance of flight control laws for a large variety of manoeuvres. The proposed approach is illustrated by ...
Aerodynamic model of transport airplane in extended envelope for simulation of upset recovery
(ICAS 2012 CD-ROM PROCEEDINGS, 2012-09)
The paper presents the aerodynamic model in extended flight envelope for a generic airliner with under wing engines and conventional tail developed within the EU Framework Programme (FP7) research project Simulation of ...
Design and analysis of combined nonlinear dynamic inversion and H_infty-based flight contol laws
(Zhejiang University, China, 2010-05)
There is a significant interest in developing flight control laws which need minimum gain scheduling across the whole flight envelope while providing required robust performance and stability properties to the closed-loop ...