Transient Dynamics Assessment of a Gain-Scheduled Aircraft Controller Using Nonlinear Frequency Approach
2021; American Institute of Aeronautics and Astronautics; Volume: 44; Issue: 9 Linguagem: Inglês
10.2514/1.g005866
ISSN1533-3884
AutoresDuc H. Nguyen, Mark Lowenberg, Simon A. Neild, Thomas Richardson,
Tópico(s)Control Systems and Identification
ResumoNo AccessEngineering NotesTransient Dynamics Assessment of a Gain-Scheduled Aircraft Controller Using Nonlinear Frequency ApproachDuc H. Nguyen, Mark H. Lowenberg, Simon A. Neild and Thomas S. RichardsonDuc H. NguyenUniversity of Bristol, Bristol, England BS8 1TR, United Kingdom*Ph.D. Student, Department of Aerospace Engineering. Student Member AIAA.Search for more papers by this author, Mark H. LowenbergUniversity of Bristol, Bristol, England BS8 1TR, United Kingdom†Professor of Flight Dynamics, Department of Aerospace Engineering. Senior Member AIAA.Search for more papers by this author, Simon A. NeildUniversity of Bristol, Bristol, England BS8 1TR, United Kingdom‡Professor of Nonlinear Structural Dynamics, Department of Aerospace Engineering.Search for more papers by this author and Thomas S. RichardsonUniversity of Bristol, Bristol, England BS8 1TR, United Kingdom§Professor of Aerial Robotics, Department of Aerospace Engineering. Senior Member AIAA.Search for more papers by this authorPublished Online:10 May 2021https://doi.org/10.2514/1.G005866SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] “Military Specification—Flying Qualities of Piloted Airplanes,” U.S. Department of Defense TR-MIL-F-8785C, 1980. Google Scholar[2] Gibson J. C., “The Development of Alternative Criteria for FBW Handling Qualities,” AGARD Conference Proceedings No. 508, Advisory Group for Aerospace Research and Development, Neuilly sur Seine, France, AGARD Paper 9, 1991, pp. 9-1–9-13. Google Scholar[3] Gill S. J., Lowenberg M. H., Neild S. A., Crespo L. 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See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAircraft DesignAircraft ManeuversAircraft OperationsAircraft Operations and TechnologyAircraft PerformanceAircraft Stability and ControlAircraft Wing DesignAircraftsCombat AircraftFlight Control SurfacesFlight TrainingFlying QualitiesMilitary AircraftStability Augmentation Systems KeywordsOpen Loop Transfer FunctionAircraftsElevator DeflectionPilotHandling QualitiesAerodynamic CoefficientsFlight DynamicsElevatorHarmonic OscillatorNonlinear DynamicsAcknowledgmentsThe first author is partially funded by the University of Bristol’s Alumni Grant. The support of QinetiQ in providing the Hypothetical High Angle of Incidence Research Model flight model is also gratefully acknowledged.PDF Received17 December 2020Accepted9 April 2021Published online10 May 2021
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