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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 ...
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 ...