No AccessOptimization of the mass ratio for a general multi-rotor aircraftMatthias Friedrich and Walter FichterMatthias FriedrichUniversity of StuttgartSearch for more papers by this author and Walter FichterUniversity of StuttgartSearch for more papers by this authorAIAA 2018-0531Session: Aircraft Flight Dynamics IPublished Online:7 Jan 2018https://doi.org/10.2514/6.2018-0531SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for references What's Popular 2018 AIAA Atmospheric Flight Mechanics Conference 8–12 January 2018Kissimmee, Floridahttps://doi.org/10.2514/6.2018-0531 CrossmarkInformationCopyright © 2018 by University of Stuttgart. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAircraft Components and StructureAircraft DesignAircraft OperationsAircraft Operations and TechnologyAircraft PerformanceAircraftsApplied MathematicsElectricityElectrodynamicsElectromagnetismGeneral PhysicsHelicoptersRotorcrafts KeywordsFlight VehicleFlight PerformanceMathematical ModelsElectric CurrentConservation of MassMulticopterAerodynamic ForceFlow PatternsMagnetic InductionSensitivity AnalysisDigital Submission Topic Atmospheric Flight Mechanics