No AccessAerodynamic predictions of pitch and roll control for canard-controlled missilesMichael Landers, Les Hall and Lamar AumanMichael LandersDynetics, Inc., Huntsville, ALSearch for more papers by this author, Les HallDynetics, Inc., Huntsville, ALSearch for more papers by this author and Lamar AumanU.S. Army, Aviation and Missile Command, Redstone Arsenal, ALSearch for more papers by this authorPublished Online:22 Aug 2012https://doi.org/10.2514/6.2000-4516SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byApproximate Method to Calculate Nonlinear Rolling Moment due to Differential Fin Deflection F. G. Moore and L. Y. Moore 9 September 2013 | Journal of Spacecraft and Rockets, Vol. 49, No. 2Adaptive sliding mode roll control of a canard-controlled missile1 May 2010Controlled canard configuration study for a solid rocket motor based unmanned air vehicle20 January 2010 | Journal of Mechanical Science and Technology, Vol. 23, No. 12Experimental investigation of nose-mounted controls for a hypersonic missileMichael Landers and Lamar Auman22 August 2012 What's Popular 18th Applied Aerodynamics Conference 14 August 2000 - 17 August 2000Denver,CO,U.S.A.https://doi.org/10.2514/6.2000-4516 Crossmark TopicsAerodynamic PerformanceAerodynamicsAerospace SciencesBoundary LayersCFD CodesComputational Fluid DynamicsFlow RegimesFluid DynamicsShock WavesVortex DynamicsWind Tunnels KeywordsControl SurfacesMissile ConfigurationsCanardAerodynamic CharacteristicsVortex StructureCFD CodesAngle of AttackReynolds Averaged Navier StokesWind Tunnel ModelsBoundary Layer SeparationDigital Topics Applied Aerodynamics