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dc.contributor.authorAbramov, Nikolayen
dc.contributor.authorGoman, M. (Mikhail G.)en
dc.contributor.authorKolesnikov, E. N.en
dc.contributor.authorSidoryuk, M. E. (Maria E.)en
dc.date.accessioned2013-10-07T09:49:01Z
dc.date.available2013-10-07T09:49:01Z
dc.date.issued2010-01
dc.identifier.citationAbramov, 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.en
dc.identifier.urihttp://hdl.handle.net/2086/9101
dc.description.abstractA 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.en
dc.language.isoenen
dc.publisherAmerican Institute of Aeronautics and Astronautics, AIAAen
dc.titleInvestigation of Attainable Equilibrium Sets for Clearance of Flight Control Lawsen
dc.typeConferenceen
dc.identifier.doihttp://dx.doi.org/10.2514/6.2010-491
dc.researchgroupCentre for Engineering Science and Advanced Systemsen
dc.peerreviewedYesen
dc.funderECen
dc.projectidSUPRAen


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