No AccessHigh Fidelity Simulation of a Nonlinear AircraftAlejandro Azocar and John ValasekAlejandro AzocarTexas A&M UniversitySearch for more papers by this author and John ValasekTexas A&M UniversitySearch for more papers by this authorAIAA 2014-0014Session: International Student Conference - Undergraduate DivisionPublished Online:10 Jan 2014https://doi.org/10.2514/6.2014-0014SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byUnified Devs-Based Platform for Modeling and Simulation of Hybrid Control SystemsEuler–Lagrange as Pseudo-metric of the RRT algorithm for optimal-time trajectory of flight simulation model in high-density obstacle environment14 December 2015 | Robotica, Vol. 35, No. 5Preliminary Evaluation of an Electromyographically Controlled QuadrotorAlejandro Azocar2 January 2016 What's Popular 52nd Aerospace Sciences Meeting 13-17 January 2014National Harbor, Marylandhttps://doi.org/10.2514/6.2014-0014 CrossmarkInformationCopyright © 2014 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. TopicsAircraft Components and StructureAircraft DesignAircraft Operations and TechnologyAircraft Stability and ControlAircraft Wing ComponentsAircraft Wing DesignAircraftsFixed-Wing AircraftFlight Control SurfacesFlight TrainingFlying Qualities KeywordsHigh Performance AircraftHandling QualitiesFlight SimulatorsNonlinear ControlElevator DeflectionAerodynamic Force CoefficientsLevel FlightAileronsFlight TestingClosed LoopPDF Topics