Volume 20, Issue 3 No AccessPrediction of Pilot-in-the-Loop Oscillations Due to Rate SaturationHolger DudaHolger Duda DLR, German Aerospace Research Establishment, 38022 Brunswick, GermanySearch for more papers by this authorPublished Online:23 May 2012https://doi.org/10.2514/2.4080SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous article Next article FiguresReferencesRelatedDetailsSee PDF for referencesCited byDesigning a Robust Predictive Controller to Prevent Rate-Limiter-Based Pilot-Induced Oscillations in the Frequency Domain8 November 2022 | Iranian Journal of Science and Technology, Transactions of Electrical Engineering, Vol. 40Coaxial-Compound Helicopter Flight Control Design and High-Speed Handling Qualities AssessmentJournal of the American Helicopter Society, Vol. 67, No. 3Tiltrotor Flight Control Design and High-Speed Handling Qualities AssessmentJournal of the American Helicopter Society, Vol. 67, No. 3Nonlinear Stability Region Determination of Pilot-Aircraft Closed-Loop Based on Differential Manifold Theory30 October 2021Method of predicting nonlinear pilot-induced oscillations due to flight control degradation based on digital virtual flightAerospace Science and Technology, Vol. 116Business Jet Fly-by-Wire Control Laws Handling Qualities Flight Test AssessmentTom Berger, Mark B. 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Neild 1 March 2021 | Journal of Guidance, Control, and Dynamics, Vol. 44, No. 5Analysis of Rotorcraft Pilot-Induced Oscillations Triggered by Active Inceptor FailuresMichael Jones and Miles Barnett6 January 2019A handling qualities analysis tool for rotorcraft conceptual designs31 May 2018 | The Aeronautical Journal, Vol. 122, No. 1252Pilot induced oscillation suppression controller design via nonlinear optimal output regulation methodAerospace Science and Technology, Vol. 68References13 December 2022In-Flight Simulator VFW 614 ATTAS17 March 2017Analysis of Pilot-Induced-Oscillation and Pilot Vehicle System Stability Using UAS Flight Experiments29 November 2016 | Aerospace, Vol. 3, No. 4Pilot-Induced-Oscillations Alleviation Through Anti-windup Based Approach1 January 2017Practices to identify and preclude adverse Aircraft-and-Rotorcraft-Pilot Couplings – A design perspectiveProgress in Aerospace Sciences, Vol. 76Stabilization of motion control system with rate limiter using linear reference modelTransactions of the JSME (in Japanese), Vol. 81, No. 829Deflection Limit in Open-Loop Onset-Point Pilot-in-the-Loop Oscillation AnalysisSanghyuk Park21 February 2014 | Journal of Guidance, Control, and Dynamics, Vol. 37, No. 2Adverse rotorcraft pilot couplings—Past, present and future challengesProgress in Aerospace Sciences, Vol. 62Lateral/Directional Control Law Design and Handling Qualities Optimization for a Business Jet Flight Control SystemTom Berger, Mark Tischler, Steven G. Hagerott, Dagfinn Gangsaas and Nomaan Saeed15 August 2013Flight Data Analysis of Pilot-Induced-Oscillations of a Remotely Controlled AircraftTanmay Kumar, Yu Gu, Haiyang Chao and Matthew B. Rhudy15 August 2013Development of the Phase-Aggression Criterion for Rotorcraft—Pilot Coupling DetectionMichael Jones, Michael Jump and Linghai Lu30 January 2013 | Journal of Guidance, Control, and Dynamics, Vol. 36, No. 1Evaluation on novel architecture for harmonizing manual and automatic flight controls under atmospheric turbulenceAerospace Science and Technology, Vol. 24, No. 1Application of parameter plane method to pilot-induced oscillationsAerospace Science and Technology, Vol. 23, No. 1Longitudinal Control Law Design and Handling Qualities Optimization for a Business Jet Flight Control System Tom Berger, Mark Tischler, Steven G. Hagerott, Dagfinn Gangsaas and Nomaan Saeed8 April 2013Pilot-Involved-Oscillation Suppression Using Low-Order Antiwindup: Flight-Test Evaluation Oliver Brieger , Murray Kerr , Ian Postlethwaite , Matthew C. Turner and Jorge Sofrony 28 August 2012 | Journal of Guidance, Control, and Dynamics, Vol. 35, No. 2A Survey of Force Feedback in Flight Safety EnhancementProcedia Engineering, Vol. 29Anti-windup Compensator SynthesisA test evaluation of a Pilot-Induced-Oscillation prediction criterionHandling Deflection Limit in Open-Loop-Onset-Point PIO AnalysisJournal of the Korean Society for Aeronautical & Space Sciences, Vol. 38, No. 2Flight testing of a rate saturation compensation scheme on the ATTAS aircraftAerospace Science and Technology, Vol. 13, No. 2-3Anti-windup design: an overview of some recent advances and open problemsIET Control Theory & Applications, Vol. 3, No. 1A Tutorial on Modern Anti-windup DesignEuropean Journal of Control, Vol. 15, No. 3-4Enhancemet of the NonLinear OLOP-PIO-Criterion Regarding Phase-Compensated Rate-LimitersDaniel Ossmann, Matthias Heller and Oliver Brieger15 June 2012Flight testing of low-order anti-windup compensators for improved handling and PIO suppressionPractical approaches to low-order anti-windup compensator design: a flight control comparisonIFAC Proceedings Volumes, Vol. 41, No. 2Anti-windup compensation of rate saturation in an experimental aircraftModel Predictive Controller Design to Suppress Rate-Limiter-Based Pilot-Induced OscillationsTRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, Vol. 49, No. 166Robust Antiwindup for Manual Flight Control of an Unstable Aircraft Giulio Avanzini and Sergio Galeani 23 May 2012 | Journal of Guidance, Control, and Dynamics, Vol. 28, No. 6Non-linear anti-windup for manual flight control20 February 2007 | International Journal of Control, Vol. 78, No. 14Real Time Prevention of Aircraft Pilot Coupling Using Multi-Model Adaptive ControlXiaohong Li19 June 2012Pilot-Induced Oscillation Analysis with Actuator Rate Limiting and Feedback Control LoopRyoji Katayanagi22 June 2012Gain-Phase Margin Analysis of Pilot-Induced Oscillations for Limit-Cycle Prediction Bing-Fei Wu and Jau-Woei Perng 23 May 2012 | Journal of Guidance, Control, and Dynamics, Vol. 27, No. 1A Study of Multiloop Feedback Flight Control System Having a Positive Effect on Pilot-Induced Oscillation (PIO)JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, Vol. 52, No. 601A limited flight test evaluation of a pilot-induced-oscillation prediction criterionGregory Gilbreath and Andrew Markofski22 August 2012Category II Pilot in-the-Loop Oscillations Analysis from Robust Stability Methods Francesco Amato , Raffaele Iervolino , Stefano Scala and Leopoldo Verde 23 May 2012 | Journal of Guidance, Control, and Dynamics, Vol. 24, No. 3Pilot-Induced Oscillation Analysis with Actuator Rate Limiting and Feedback Control LoopTRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, Vol. 44, No. 143SCARLET 3 - A flight experiment considering rate saturationGunnar Duus22 August 2012An LFT framework for limit-cycle analysis - Application to PIO detectionJ.-M. Biannic22 August 2012New Flight Simulator Experiments on Pilot-Involved Oscillations due to Rate Saturation Holger Duda , Gunnar Duus , Gunnar Hovmark and Lars Forssell 23 May 2012 | Journal of Guidance, Control, and Dynamics, Vol. 23, No. 2μ Tools for flight control robustness assessmentAerospace Science and Technology, Vol. 3, No. 3Extraction of pilot-vehicle characteristics in the presence of rate limitingDavid Klyde and David Mitchell22 August 2012Assessing Aircraft Susceptibility to Nonlinear Aircraft-Pilot Coupling/Pilot-Induced Oscillations R. A. Hess and P. W. Stout 23 May 2012 | Journal of Guidance, Control, and Dynamics, Vol. 21, No. 6Pilot-Induced Oscillations Involving Multiple Nonlinearities Mark R. Anderson 23 May 2012 | Journal of Guidance, Control, and Dynamics, Vol. 21, No. 5New flight simulator experiments on PIO due to rate saturationHolger Duda, Gunnar Duus, Gunnar Hovmark and Lars Forssell22 August 2012Flight control system design considering rate saturationAerospace Science and Technology, Vol. 2, No. 4Analysis of pilot-in-the-loop oscillations due to position and rate saturations What's Popular Volume 20, Number 3May 1997 Crossmark TopicsAeronauticsAircraft Components and StructureAircraft ControlAircraft DesignAircraft Flight Control SystemAircraft OperationsAircraft Operations and TechnologyAircraft PerformanceAircraft Stability and ControlAircraft SystemsAircraft Wing DesignAircraftsAviationFlight Control SurfacesMilitary AircraftMilitary AviationRotorcrafts KeywordsAircraft PilotClosed Loop SystemControl System DesignFeedback LoopPilot ModelingControl SurfacesYF 16 AircraftAircraft SystemsBank AngleGerman Aerospace Research EstablishmentPDF Published online23 May 2012