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• W4384697281 abstract "No AccessEngineering NotesEffects of Structural Flexibility on Flight Control of a QuadrotorChristopher S. Smith and Alok SinhaChristopher S. SmithPennsylvania State University, University Park, Pennsylvania 16802*Researcher, Applied Research Lab at Penn State; . Member AIAA (Corresponding Author).Search for more papers by this author and Alok SinhaPennsylvania State University, University Park, Pennsylvania 16802†Professor of Mechanical Engineering; . Associate Fellow AIAA.Search for more papers by this authorPublished Online:18 Jul 2023https://doi.org/10.2514/1.G007550SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Ahuja V., Hartfield R. and Chakraborty I., “Gust Response Analysis for Early Design of Advanced Air Vehicle Concepts,” APISAT 2019: Asia Pacific International Symposium on Aerospace Technology, Engineers Australia, Gold Coast, Australia, 2019. 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I., “Design, Construction and Control of a Large Quadrotor Micro Air Vehicle,” Ph.D. Thesis, Australian National Univ., Canberra, Australia, 2007. Google Scholar[22] Bouabdallah S., Noth A. and Siegwart R., “PID vs LQ Control Techniques Applied to an Indoor Micro Quadrotor,” 2004 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS)(IEEE Cat. No. 04CH37566), No. 3, IEEE, New York, 2004, pp. 2451–2456. Google Scholar[23] García R. A., Rubio F. R. and Ortega M. G., “Robust PID Control of the Quadrotor Helicopter,” IFAC Proceedings Volumes, Vol. 45, No. 3, 2012, pp. 229–234. https://doi.org/10.3182/20120328-3-IT-3014.00039 CrossrefGoogle Scholar[24] O’Brien R. T. and Howe J. M., “Optimal PID Controller Design Using Standard Optimal Control Techniques,” Proceedings of the American Control Conference, IEEE, New York, 2008. Google Scholar[25] Miranda-Colorado R. and Aguilar L. T., “Robust PID Control of Quadrotors with Power Reduction Analysis,” ISA Transactions, Vol. 98, March 2020, pp. 47–62. https://doi.org/10.1016/j.isatra.2019.08.045 Google Scholar[26] Liu C., Pan J. and Chang Y., “PID and LQR Trajectory Tracking Control for an Unmanned Quadrotor Helicopter: Experimental Studies,” 35th Chinese Control Conference (CCC), IEEE, New York, 2016. Google Scholar[27] Khatoon S., Gupta D. and Das L. K., “PID & LQR Control for a Quadrotor: Modeling and Simulation,” 2014 International Conference on Advances in Computing, Communications and Informatics (ICACCI), IEEE, New York, 2014. Google Scholar[28] Control System Toolbox, MathWorks, Inc., Natick, MA, 2020. Google Scholar Previous article Next article FiguresReferencesRelatedDetails What's Popular Articles in Advance CrossmarkInformationCopyright © 2023 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-3884 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAircraft Components and StructureAircraft ControlAircraft DesignAircraft Flight Control SystemAircraft Operations and TechnologyAircraft Stability and ControlAircraftsControl TheoryFlexible and Active StructuresGuidance, Navigation, and Control SystemsMechanical and Structural VibrationsQuadcopterStructural Design and DevelopmentStructural EngineeringStructural Kinematics and DynamicsStructures, Design and TestUnmanned Aerial Vehicle KeywordsQuadcopterAircraft Flight Control SystemLinear Time Invariant SystemStructural Kinematics and DynamicsFlexible and Active StructuresAircraft Components and StructureAerodynamic AnalysisMechanical and Structural VibrationsFlight DynamicsPDF Received16 February 2023Accepted9 June 2023Published online18 July 2023" @default.
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