Downwash Detection and Avoidance with Small Quadrotor Helicopters
2016; American Institute of Aeronautics and Astronautics; Volume: 40; Issue: 3 Linguagem: Inglês
10.2514/1.g001465
ISSN1533-3884
AutoresDerrick Yeo, Nitin Sydney, Derek A. Paley, Donald Sofge,
Tópico(s)Real-time simulation and control systems
ResumoNo AccessEngineering NoteDownwash Detection and Avoidance with Small Quadrotor HelicoptersDerrick W. Yeo, Nitin Sydney, Derek A. Paley and Donald SofgeDerrick W. YeoUniversity of Maryland, College Park, Maryland 20742, Nitin SydneyUniversity of Maryland, College Park, Maryland 20742, Derek A. PaleyUniversity of Maryland, College Park, Maryland 20742 and Donald SofgeNaval Research Laboratory, Washington, D.C. 20375Published Online:2 Dec 2016https://doi.org/10.2514/1.G001465SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Belkheri M., Rabhi A., Hajjaji A. and Pergard C., "Different Linearization Control Techniques for a Quadrotor System," 2nd International Conference on Communications, Computing and Control Applications (CCCA), Marseilles, 2012, pp. 1–6. doi:https://doi.org/10.1109/CCCA.2012.6417914 Google Scholar[2] Alexander D. and Vogel S., Nature's Flyers: Birds, Insects, and the Biomechanics of Flight, Johns Hopkins Univ. Press, Baltimore, MD, Oct. 2004, pp. 132–134. 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LinkGoogle Scholar Previous article Next article FiguresReferencesRelatedDetailsCited byLane Geometry, Compliance Levels, and Adaptive Geo-fencing in CORRIDRONE Architecture for Urban MobilityAerodynamic imaging by mosquitoes inspires a surface detector for autonomous flying vehicles7 May 2020 | Science, Vol. 368, No. 6491Wind Measurement and Simulation Techniques in Multi-Rotor Small Unmanned Aerial VehiclesIEEE Access, Vol. 8Aerial Robot Control in Close Proximity to Ceiling: A Force Estimation-based Nonlinear MPCCentralized predictive ceiling interaction control of quadrotor VTOL UAVAerospace Science and Technology, Vol. 76 What's Popular Volume 40, Number 3March 2017 CrossmarkInformationCopyright © 2015 by Derrick W. Yeo, Nitin Sydney, Derek A. Paley, and Donald Sofge. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0731-5090 (print) or 1533-3884 (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAerodynamic PerformanceAerodynamicsAeronautical EngineeringAeronauticsAirspeedBoundary LayersComputational Fluid DynamicsFlow Diagnostics and ControlFlow RegimesFluid DynamicsFluid Flow PropertiesVortex DynamicsWind Tunnels KeywordsQuadrotor HelicopterAerodynamic ForceRotary WingHigh Speed FlightFlight TestingBlended Wing BodyAccelerating FlowVelocity ProfilesUAVDifferential Pressure SensorsAcknowledgmentsThis work was performed at the University of Maryland and the Naval Research Laboratory, and it was funded by the U.S. Department of Defense, Office of Naval Research under grant number N0001413WX21045; the Mobile Autonomous Teams for Navy Information Surveillance and Search; the U.S. Army under grant no. W911W6112072; and the U.S. Air Force Office of Scientific Research under grant no. FA95501310162, Dynamic Data Driven Applications Systems. The views, positions, and conclusions expressed herein reflect only the authors opinions and expressly do not reflect those of the U.S. Department of Defense, the Office of Naval Research, or the Naval Research Laboratory.PDF Received12 May 2015Accepted14 December 2015Published online2 December 2016
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