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• W2920502473 abstract "No AccessEngineering NotesTime-Domain System Identification of Helicopters Using Nonlinear Acceleration and Jerk Prediction ModelSagar Setu, Abhishek Abhishek and C. VenkatesanSagar SetuIndian Institute of Technology Kanpur, Kanpur 208 016, India*Graduate Student, Department of Aerospace Engineering; .Search for more papers by this author, Abhishek AbhishekIndian Institute of Technology Kanpur, Kanpur 208 016, India†Associate Professor, Department of Aerospace Engineering; . Member AIAA.Search for more papers by this author and C. VenkatesanIndian Institute of Technology Kanpur, Kanpur 208 016, India‡Visiting Professor, Department of Mechanical Engineering; . Member AIAA.Search for more papers by this authorPublished Online:4 Mar 2019https://doi.org/10.2514/1.C035273SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Setu S., Abhishek A. and Venkatesan C., “Framework for Attitude Controller Development Using Physics Based Flight Dynamics and Hardware-in-the-Loop Simulation for Rotary Wing UAVs,” 73rd American Helicopter Society Annual Forum [CD-ROM], AHS International, Alexandria, VA, May 2017. Google Scholar[2] Cai G., Chen B. M., Lee T. 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S. and Chopra I., “Gramian Analysis of a Shrouded Rotor Micro Air Vehicle in Hover,” Journal of Guidance, Control, and Dynamics, Vol. 37, No. 5, 2014, pp. 1684–1691. doi:https://doi.org/10.2514/1.G000066 LinkGoogle Scholar[38] Bousman W. G. and Norman T., “Assessment of Predictive Capability of Aeromechanics Methods,” Journal of the American Helicopter Society, Vol. 55, No. 1, 2010, Paper 12001. doi:https://doi.org/10.4050/JAHS.55.012001 CrossrefGoogle Scholar Previous article FiguresReferencesRelatedDetailsCited bySystem Identification Approach for eVTOL Aircraft Demonstrated Using Simulated Flight DataBenjamin M. Simmons 1 February 2023 | Journal of Aircraft, Vol. 0, No. 0Kalman filter identification method for micro-vibration transfer paths of satellites6 December 2021 | Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 236, No. 11Flight Dynamics and Control of an Unmanned Helicopter with Underslung Double PendulumKuldeep K. Dhiman, Abhishek and Mangal Kotharic18 January 2022 | Journal of Aircraft, Vol. 59, No. 1 What's Popular Volume 56, Number 3May 2019Special Section on Second Sonic Boom Prediction Workshop CrossmarkInformationCopyright © 2019 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 1533-3868 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 ControlAircraft Wing DesignAircraftsFlight Control SurfacesFlight RecorderFlight TrainingHelicopter DynamicsHelicoptersRotorcraftsUnmanned Aerial Vehicle KeywordsHelicoptersProportional Integral DerivativeUnmanned HelicopterRotor BladesRotary WingAttitude and Heading Reference SystemFlight TestingAerodynamic Force VectorYawAngular MotionAcknowledgmentThe authors gratefully acknowledge the funding for autonomous helicopter research from the Department of Science and Technology, India.PDF Received24 September 2018Accepted15 January 2019Published online4 March 2019" @default.
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