02099oam 2200517I 450 991070420380332120160219105215.0(CKB)5470000002439642(OCoLC)703662291(EXLCZ)99547000000243964220110224j199607 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierBiomechanically induced and controller coupled oscillations experienced on the F-16XL aircraft during rolling maneuvers /John W. Smith and Terry MontgomeryEdwards, California :National Aeronautics and Space Administration, Office of Management, Scientific and Technical, Information Program,July 1996.1 online resource (35 pages) color illustrationsNASA technical memorandum ;4752Title from title screen (viewed Feb. 19, 2016)."July 1996.""Performing organization: NASA Dryden Flight Research Center"--Report documentation page.Includes bibliographical references (page 35).Fly by wire controlnasatOscillationsnasatRolling momentsnasatHuman factors engineeringnasatF-16 aircraftnasatFly by wire control.Oscillations.Rolling moments.Human factors engineering.F-16 aircraft.Smith John W.1396303Montgomery TerryDryden Flight Research Facility.United States.National Aeronautics and Space Administration.Scientific and Technical Information Program,United States.National Aeronautics and Space Administration,SSNSSNGPOBOOK9910704203803321Biomechanically induced and controller coupled oscillations experienced on the F-16XL aircraft during rolling maneuvers3456156UNINA