Time-Delay Margin and Robustness of Incremental Nonlinear Dynamic Inversion Control

No AccessEngineering NotesTime-Delay Margin and Robustness of Incremental Nonlinear Dynamic Inversion ControlYingzhi Huang, Ye Zhang, Daan M. Pool, Olaf Stroosma Qiping ChuYingzhi HuangNorthwestern Polytechnical University, 710072 Xi’an, China*Associate Professor, School Power Energy; . Member AIAA.Search for more papers by this author, ZhangNorthwestern China†Associate Astronautics; AIAA (Corresponding Author).Search Pool https://orcid.org/0000-0001-9535-2639Delft University Technology, 2629HS Delft, The Netherlands‡Assistant Control Simulation Section, Faculty Aerospace Engineering; Senior StroosmaDelft Netherlands§Senior Researcher, author ChuDelft Netherlands¶Associate authorPublished Online:13 Oct 2021https://doi.org/10.2514/1.G006024SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Enns D., Bugajski Hendrick R. Stein G., “Dynamic Inversion: An Evolving Methodology Flight Design,” International Journal Control, Vol. 59, No. 1, 1994, pp. 71–91. https://doi.org/10.1080/00207179408923070 CrossrefGoogle Scholar[2] Saha Valasek J., Leshikar C. Reza M., “Multiple-Timescale Aircraft with Model Uncertainties,” Guidance, Dynamics, 43, 3, 2020, 536–552. LinkGoogle Scholar[3] Smith P., “A Simplified Approach Based Control,” 23rd Atmospheric Mechanics Conference, Paper 1998-4461, 1998. Scholar[4] Sieberling S., Chu Q. P. Mulder J. A., “Robust Using Angular Acceleration Prediction,” 33, 6, 2010, 1732–1742. Scholar[5] Huang Y., D. O. Q., “Long-Stroke Hydraulic Robot Motion Inversion,” IEEE/ASME Transactions on Mechatronics, 24, 2019, 304–314. https://doi.org/10.1109/TMECH.2019.2891358 Scholar[6] Smeur E. de Croon G. C., “Adaptive Attitude Micro Aerial Vehicles,” 39, 2016, 450–461. Scholar[7] Pfeifle Fichter W., “Cascaded Three-Dimensional Spline-Tracking Wind Compensation,” 44, 8, 2021, G005785. https://doi.org/10.2514/1.G005785 Google Scholar[8] Simplício Pavel van Kampen “An Measurements-Based Helicopter Engineering Practice, 21, 2013, 1065–1077. Scholar[9] Keijzer T., Looye E.-J. V., “Design Testing Backstepping Laws Accelerometer Feedback,” Scitech 2019 Forum, 2019-0129, 2019. Scholar[10] Kim S. Bae “Force-Mode Rotary Series Elastic Actuators in a Lower Extremity Exoskeleton Model-Inverse Time Delay 22, 2017, 1392–1400. Scholar[11] Hou Z. Xiong “On Model-Free Adaptive Its Stability Analysis,” IEEE Automatic 64, 11, 4555–4569. Scholar[12] Liu Sun L., Tan X. Li “Finite Observer Fault-Tolerant Science 104, Sept. 105986. Scholar[13] Ignatyev I., Shin H.-S. Tsourdos “Two-Layer Augmentation Transport Uncertain Conditions,” 105, Oct. 106051. Scholar[14] Wang X., “Quadrotor Nonsingular Terminal Sliding Mode 95, Dec. 105514. Scholar[15] Zhou “Incremental Online Heuristic Programming Tracking Partial Observability,” 106013. Scholar[16] Van E.-J., Lu “Stability Analysis 2018 Navigation, 2018-1115, 2018. Scholar[17] van’t Veld R., Improvements 2018-1127, Scholar[18] Gu K., Chen Kharitonov V. Time-Delay Systems, Springer & Business Media, New York, 2003, 9–28. Scholar[19] Khalil H. 3rd ed., Prentice-Hall, Englewood Cliffs, NJ, 2002, Chap. 13. Scholar[20] Slotine J.-J. Applied 199, 1991, 6. Scholar[21] Richard J.-P., “Time-Delay Systems: Overview Some Recent Advances Open Problems,” Automatica, 10, 1667–1694. https://doi.org/10.1016/S0005-1098(03)00167-5 Scholar[22] K. Niculescu S.-I., “Survey Results the Systems*,” Measurement, 125, 2, 158–165. https://doi.org/10.1115/1.1569950 Scholar[23] Fu S.-I. Linear Neutral Exact Conditions via Matrix Pencil Solutions,” 51, June 2006, 1063–1069. https://doi.org/10.1109/ACC.2005.1470648 Scholar[24] El’sgol’ts L. Norkin Introduction Theory Application Differential Equations Deviating Arguments, Mathematics Engineering, Academic Press, 1973, 132–138. Scholar[25] Effects Stability: A Robust Approach, Lecture Notes Information Sciences, Springer, London, 3. Scholar[26] Kolmanovskii B. Nosov Functional Equations, 180, Elsevier, 1986, 55–60. Scholar[27] Stevens Lewis F., Simulation, Wiley, 1992, 393–397. Scholar[28] der Linden A. DASMAT-Delft Tool: Matlab/Simulink Environment Dynamics Analysis, Delft Univ. Netherlands, 1998, http://resolver.tudelft.nl/uuid:25767235-c751-437e-8f57-0433be609cc1. Scholar Previous article Next FiguresReferencesRelatedDetailsCited byAdaptive flight control system safety improvement reentry other high-velocity vehiclesActa Astronautica, 204Filter sensor delay synchronization incremental laws19 January 2023 | 39Date-Driven Fuzzy-State AUV under Disturbance Time-Delay12 Marine 1 What's Popular Volume 45, Number 2February 2022 CrossmarkInformationCopyright © 2021 Yingzhi Huang. Published American Institute Aeronautics Astronautics, Inc., permission. All requests copying permission reprint should be submitted CCC at www.copyright.com; employ eISSN 1533-3884 initiate your request. See also Rights Permissions www.aiaa.org/randp. TopicsAircraft ControlAircraft DesignAircraft SystemAircraft Operations TechnologyAircraft Wing DesignAircraftsCessna CitationFixed-Wing AircraftFlight SurfacesJet AircraftUnmanned Vehicle KeywordsNonlinear InversionClosed Loop Transfer FunctionFlight SystemMultiple Input Multiple OutputFixed AircraftBody Reference FrameNonlinear SystemsControl SurfacesMean Aerodynamic ChordFeedback LinearizationAcknowledgmentsThe first corresponding were supported Fundamental Research Funds Central Universities grant nos. G2021KY05122 G2021KY05109.PDF Received24 February 2021Accepted8 September 2021Published online13 October