02249oam 2200553I 450 991070701080332120160405125912.0(CKB)5470000002461384(OCoLC)777339966(EXLCZ)99547000000246138420120218j199702 ua 0engurbn||||a|a||txtrdacontentcrdamediacrrdacarrierExtraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack /Kenneth W. Iliff, Kon-Sheng Charles Wang[Washington, D.C] :National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program Center,February 1997.1 online resource (iii, 35 pages) illustrationsNASA technical memorandum ;4786Title from title screen (viewed April 5, 2016)."February 1997.""Performing organization: NASA Dryden Flight Research Center, Edwards, California"--Report documentation page.Includes bibliographical references (pages 14-15).Angle of attacknasatF-18 aircraftnasatMaximum likelihood estimatesnasatParameter identificationnasatWind tunnel testsnasatAngle of attack.F-18 aircraft.Maximum likelihood estimates.Parameter identification.Wind tunnel tests.Iliff Kenneth W.13447Wang Kon-Sheng CharlesNASA Dryden Flight Research Center.United States.National Aeronautics and Space Administration.Scientific and Technical Information Program,United States.National Aeronautics and Space Administration,OCLCEOCLCEOCLCQOCLCFOCLCOGPOBOOK9910707010803321Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack3529508UNINA