Investigation of Attainable Equilibrium Sets for Clearance of Flight Control Laws
Date
2010-01
Advisors
Journal Title
Journal ISSN
ISSN
Volume Title
Publisher
American Institute of Aeronautics and Astronautics
Type
Conference
Peer reviewed
Yes
Abstract
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.
Description
Keywords
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.