Investigation of Attainable Equilibrium Sets for Clearance of Flight Control Laws
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 clearance of the LPV control laws designed in a wide subsonic region for the F-18HARV aircraft in level flight conditions and clearance of the F-16 aircraft longitudinal and lateral-directional stability augmentation system for high range of incidence and intensive velocity roll rotation.
Citation : Abramov, N., Goman, M., Kolesnikov, E. N., Sidoryuk, M.E. (2010) Investigation of Attainable Equilibrium Sets for Clearance of Flight Control Laws. AIAA 2010-491, 48th AIAA Aerospace Sciences Meeting, 4-7 January 2010, Orlando, Florida.
Research Group : Centre for Engineering Science and Advanced Systems
Peer Reviewed : Yes