Artigo Acesso aberto Revisado por pares

Framework for Simultaneous Sensor and Actuator Fault-Tolerant Flight Control

2017; American Institute of Aeronautics and Astronautics; Volume: 40; Issue: 8 Linguagem: Inglês

10.2514/1.g002079

ISSN

1533-3884

Autores

Peng Lu, Erik-Jan Van Kampen, Coen C. de Visser, Q. P. Chu,

Tópico(s)

Advanced Data Processing Techniques

Resumo

No AccessEngineering NoteFramework for Simultaneous Sensor and Actuator Fault-Tolerant Flight ControlP. Lu, E. van Kampen, C. C. de Visser and Q. P. ChuP. LuDelft University of Technology, 2600 GB Delft, The Netherlands, E. van KampenDelft University of Technology, 2600 GB Delft, The Netherlands, C. C. de VisserDelft University of Technology, 2600 GB Delft, The Netherlands and Q. P. ChuDelft University of Technology, 2600 GB Delft, The NetherlandsPublished Online:2 Jun 2017https://doi.org/10.2514/1.G002079SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Lombaerts T., Chu Q., Mulder J. and Joosten D., “Modular Flight Control Reconfiguration Design and Simulation,” Control Engineering Practice, Vol. 19, No. 6, 2011, pp. 540–554. doi:https://doi.org/10.1016/j.conengprac.2010.12.008 COEPEL 0967-0661 CrossrefGoogle Scholar[2] “Safety Report,” International Civil Aviation Organization, Technical Rept., Montreal, Quebec, Canada, 2015. Google Scholar[3] Smaili M. H., Breeman J., Lombaerts T. and Joosten D. A., “A Simulation Benchmark for Integrated Fault Tolerant Flight Control Evaluation,” AIAA Modeling and Simulation Technologies Conference and Exhibit, AIAA, Reston, VA, 2006, pp. 1–23. Google Scholar[4] “Uncontrolled Descent and Collision with Terrain, “United Airlines Flight 585, Boeing 737-200, N999UA, 4 Miles South of Colorado Springs Municipal Airport,” Aircraft Accident Rept. NTSB/AAR-01/01, Washington, D.C., 2001. Google Scholar[5] Lombaerts T., “Fault Tolerant Flight Control—A Physical Model Approach,” Ph.D. Thesis, Delft Univ. of Technology, Delft, The Netherlands, 2010. Google Scholar[6] “Final Report on the Accident on 1st June 2009 to the Airbus A330-203 Registered F-GZCP Operated by Air France Flight AF 447 Rio de Janeiro Paris,” Bureau d’Enquêtes et d’Analyses pour la sécurité de l’aviation civile, French, Technical Rept., 2012. Google Scholar[7] “ATSB Transport Safety Report: In-Flight Upset 154 km West of Learmonth, WA 7 October 2008 VH-QPA Airbus A330-303,” Australian Transport Safety Bureau Technical Rept. AO-2008-070, Australia, Oct. 2008. Google Scholar[8] Patton R. J., “Fault-Tolerant Control Systems: The 1997 Situation,” Proceedings of IFAC Symposium on Fault Detection, Supervision and Safety for Technical Processes, IFAC, Hull, U.K., 1997, pp. 1033–1054. Google Scholar[9] Zolghadri A., “Advanced Model-Based FDIR Techniques for Aerospace Systems: Today Challenges and Opportunities,” Progress in Aerospace Sciences, Vol. 53, Aug. 2012, pp. 18–29. doi:https://doi.org/10.1016/j.paerosci.2012.02.004 PAESD6 0376-0421 CrossrefGoogle Scholar[10] Marzat J., Piet-Lahanier H., Damongeot F. and Walter E., “Model-Based Fault Diagnosis for Aerospace Systems: A Survey,” Journal of Aerospace Engineering, Vol. 226, No. 10, 2012, pp. 1329–1360. doi:https://doi.org/10.1177/0954410011421717 Google Scholar[11] Freeman P., Seiler P. and Balas G. J., “Air Data System Fault Modeling and Detection,” Control Engineering Practice, Vol. 21, No. 10, 2013, pp. 1290–1301. doi:https://doi.org/10.1016/j.conengprac.2013.05.007 COEPEL 0967-0661 CrossrefGoogle Scholar[12] Lu P., Van Eykeren L., van Kampen E. and Chu Q., “Selective-Reinitialisation Multiple Model Adaptive Estimation for Fault Detection and Diagnosis,” Journal of Guidance, Control, and Dynamics, Vol. 38, No. 8, 2015, pp. 1409–1424. doi:https://doi.org/10.2514/1.G000587 JGCODS 0731-5090 LinkGoogle Scholar[13] Lu P., Van Eykeren L., van Kampen E., de Visser C. C. and Chu Q., “Adaptive Three-Step Kalman Filter for Air Data Sensor Fault Detection and Diagnosis,” Journal of Guidance, Control, and Dynamics, Vol. 39, No. 3, 2016, pp. 590–604. doi:https://doi.org/10.2514/1.G001313 JGCODS 0731-5090 LinkGoogle Scholar[14] Alwi H., Chen L. and Edwards C., “Reconstruction of Simultaneous Actuator and Sensor Faults for the Reconfigure Benchmark Using a Sliding Mode Observer,” International Federation of Automatic Control World Congress, Vol. 2, IFAC, Hull, U.K., 2014, pp. 3497–3502. CrossrefGoogle Scholar[15] Varga A. and Ossmann D., “LPV Model-Based Robust Diagnosis of Flight Actuator Faults,” Control Engineering Practice, Vol. 31, Oct. 2014, pp. 135–147. doi:https://doi.org/10.1016/j.conengprac.2013.11.004 COEPEL 0967-0661 CrossrefGoogle Scholar[16] Van Eykeren L. and Chu Q., “Sensor Fault Detection and Isolation for Aircraft Control Systems by Kinematic Relations,” Control Engineering Practice, Vol. 31, Oct. 2014, pp. 200–210. doi:https://doi.org/10.1016/j.conengprac.2014.02.017 COEPEL 0967-0661 CrossrefGoogle Scholar[17] Lu P., Van Eykeren L., van Kampen E., de Visser C. C. and Chu Q., “Double-Model Adaptive Fault Detection and Diagnosis Applied to Real Flight Data,” Control Engineering Practice, Vol. 36, March 2015, pp. 39–57. doi:https://doi.org/10.1016/j.conengprac.2014.12.007 COEPEL 0967-0661 CrossrefGoogle Scholar[18] Lu P., van Kampen E., de Visser C. and Chu Q. P., “Nonlinear Aircraft Sensor Fault Reconstruction in the Presence of Disturbances Validated by Real Flight Data,” Control Engineering Practice, Vol. 49, April 2016, pp. 112–128. doi:https://doi.org/10.1016/j.conengprac.2016.01.012 COEPEL 0967-0661 CrossrefGoogle Scholar[19] Zhang Y. and Jiang J., “Bibliographical Review on Reconfigurable Fault-Tolerant Control Systems,” Annual Reviews in Control, Vol. 32, No. 2, 2008, pp. 229–252. doi:https://doi.org/10.1016/j.arcontrol.2008.03.008 CrossrefGoogle Scholar[20] Yu X., Liu Z. and Zhang Y., “Fault-Tolerant Flight Control with Finite-Time Adaptation Under Actuator Stuck Failures,” IEEE Transactions on Control Systems Technology, Vol. PP, No. 99, Sept. 2016, pp. 1–10. doi:https://doi.org/10.1109/TCST.2016.2603072 CrossrefGoogle Scholar[21] Yu X., Liu Z. and Zhang Y., “Fault-Tolerant Flight Control Design with Explicit Consideration of Reconfiguration Transients,” Journal of Guidance, Control, and Dynamics, Vol. 39, No. 3, 2016, pp. 556–563. doi:https://doi.org/10.2514/1.G001414 JGCODS 0731-5090 LinkGoogle Scholar[22] Lu P., van Kampen E., de Visser C. and Chu Q. P., “Aircraft Fault-Tolerant Trajectory Control Using Incremental Nonlinear Dynamic Inversion,” Control Engineering Practice, Vol. 57, Dec. 2016, pp. 126–141. doi:https://doi.org/10.1016/j.conengprac.2016.09.010 COEPEL 0967-0661 CrossrefGoogle Scholar[23] Kale M. M. and Chipperfield A. J., “Stabilized MPC Formulations for Robust Reconfigurable Flight Control,” Control Engineering Practice, Vol. 13, No. 6, 2005, pp. 771–788. doi:https://doi.org/10.1016/j.conengprac.2004.09.001 COEPEL 0967-0661 CrossrefGoogle Scholar[24] Utkin V. I., Sliding Modes in Control and Optimization, Springer–Verlag, Berlin, 1992, pp. 75–199. CrossrefGoogle Scholar[25] Cieslak J., Henry D., Zolghadri A. and Goupil P., “Development of an Active Fault-Tolerant Flight Control Strategy,” Journal of Guidance, Control, and Dynamics, Vol. 31, No. 1, 2008, pp. 135–147. doi:https://doi.org/10.2514/1.30551 JGCODS 0731-5090 LinkGoogle Scholar[26] Krsti C. M., Kanellakopoulos I. and Kokotovic P., Nonlinear and Adaptive Control Design, Wiley, New York, 1995, pp. 87–121. Google Scholar[27] Farrell J. A., Polycarpou M., Sharma M. and Dong W., “Command Filtering Backstepping,” IEEE Transactions on Automatic Control, Vol. 54, No. 6, 2009, pp. 1391–1395. doi:https://doi.org/10.1109/TAC.2009.2015562 IETAA9 0018-9286 CrossrefGoogle Scholar[28] Acquatella P., van Kampen E. and Chu Q., “Incremental Backstepping for Robust Nonlinear Flight Control,” Proceedings of the EuroGNC 2013, 2nd CEAS Special Conference on Guidance, Navigation & Control, CEAS, 2013, pp. 1444–1463. Google Scholar[29] Lu P., van Kampen E. and Chu Q., “Robustness and Tuning of Incremental Backstepping,” AIAA Guidance, Navigation and Control Conference, AIAA, Reston, VA, 2015, pp. 1–15; also AIAA Paper 2015-1762, 2015. Google Scholar[30] Chen R. H. and Speyer J. L., “Sensor and Actuator Fault Reconstruction,” Journal of Guidance, Control, and Dynamics, Vol. 27, No. 2, 2004, pp. 186–196. doi:https://doi.org/10.2514/1.9163 JGCODS 0731-5090 LinkGoogle Scholar[31] Yu X. and Jiang J., “A Survey of Fault-Tolerant Controllers Based on Safety-Related Issues,” Annual Reviews in Control, Vol. 39, No. 39, 2015, pp. 46–57. doi:https://doi.org/10.1016/j.arcontrol.2015.03.004 CrossrefGoogle Scholar[32] Zhang Y. and Li X., “Detection and Diagnosis of Sensor and Actuator Failures Using IMM Estimator,” IEEE Transactions on Aerospace and Electronic Systems, Vol. 34, No. 4, 1998, pp. 1293–1313. doi:https://doi.org/10.1109/7.722715 IEARAX 0018-9251 CrossrefGoogle Scholar[33] Marzat J., Piet-Lahanier H., Damongeot F. and Walter E., “Control-Based Fault Detection and Isolation for Autonomous Aircraft,” Journal of Aerospace Engineering, Vol. 226, No. 5, 2012, pp. 510–531. doi:https://doi.org/10.1177/0954410011413834 Google Scholar[34] Gillijns S. and De Moor B., “Unbiased Minimum-Variance Input and State Estimation for Linear Discrete-Time Systems with Direct Feedthrough,” Automatica, Vol. 43, No. 1, 2007, pp. 111–116. doi:https://doi.org/10.1016/j.automatica.2006.08.002 ATCAA9 0005-1098 CrossrefGoogle Scholar[35] Julier S. J. and Uhlmann J. K., “Unscented Filtering and Nonlinear Estimation,” Proceedings of the IEEE, Vol. 92, No. 3, 2004, pp. 401–422. doi:https://doi.org/10.1109/JPROC.2003.823141 IEEPAD 0018-9219 CrossrefGoogle Scholar[36] Van Der Merwe R. and Wan E. A., “The Square-Root Unscented Kalman Filter for State and Parameter-Estimation,” IEEE International Conference on Acoustics, Speech, and Signal Processing, IEEE Publ., Piscataway, NJ, 2001, pp. 3461–3464. Google Scholar[37] Bacon B. J., Ostroff A. J. and Joshi S. M., “Reconfigurable NDI Controller Using Inertial Sensor Failure Detection & Isolation,” IEEE Transactions on Aerospace and Electronic Systems, Vol. 37, No. 4, 2001, pp. 1373–1383. doi:https://doi.org/10.1109/7.976972 IEARAX 0018-9251 CrossrefGoogle Scholar[38] Sonneveldt L., Chu Q. and Mulder J. A., “Nonlinear Flight Control Design Using Constrained Adaptive Backstepping,” Journal of Guidance, Control, and Dynamics, Vol. 30, No. 2, 2007, pp. 322–336. doi:https://doi.org/10.2514/1.25834 JGCODS 0731-5090 LinkGoogle Scholar[39] Goupil P., “Oscillatory Failure Case Detection in the A380 Electrical Flight Control System by Analytical Redundancy,” Control Engineering Practice, Vol. 18, No. 9, 2010, pp. 1110–1119. doi:https://doi.org/10.1016/j.conengprac.2009.04.003 COEPEL 0967-0661 CrossrefGoogle Scholar Previous article FiguresReferencesRelatedDetailsCited byData-driven fault-tolerant control for unmanned aerial vehicles without using identification model18 April 2022 | Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 236, No. 16Civil Aircraft Fault Tolerant Attitude Tracking based on Extended State Observers and Nonlinear Dynamic InversionJournal of Systems Engineering and Electronics, Vol. 33, No. 1Improved Adaptive Integral-Sliding-Mode Fault-Tolerant Control for Hypersonic Vehicle With Actuator FaultIEEE Access, Vol. 9Dynamics and adaptive fault-tolerant flight control under structure damage of horizontal stabilizerAerospace Science and Technology, Vol. 106Aero‐Engine DCS Fault‐Tolerant Control with Markov Time Delay Based On Augmented Adaptive Sliding Mode Observer29 October 2018 | Asian Journal of Control, Vol. 22, No. 2Active and Passive Fault Tolerant Control for Winged Aircraft with Simultaneous Actuator and Sensor Faults8 September 2019Observer-based H∞ fault-tolerant attitude control for satellite with actuator and sensor faultsAerospace Science and Technology, Vol. 95Observer-based Sliding Mode Fault-Tolerant Control for Spacecraft Attitude System with Actuator FaultsCommand Filtered Model-Free Robust Control for Aircrafts With Actuator DynamicsIEEE Access, Vol. 7Combined Quaternion-Based Error State Kalman Filtering and Smooth Variable Structure Filtering for Robust Attitude EstimationIEEE Access, Vol. 7A reconfiguration control framework for constrained systems with sensor stuck faults10 December 2018 | International Journal of Robust and Nonlinear Control, Vol. 59Command-filtered sensor-based backstepping controller for small unmanned aerial vehicles with actuator dynamics4 November 2018 | International Journal of Systems Science, Vol. 49, No. 16Nonlinear Disturbance Attenuation Control of Hydraulic RoboticsCommand-Filtered Incremental Backstepping Controller for Small Unmanned Aerial VehiclesY. C. Wang, W. S. Chen, S. X. Zhang, J. W. Zhu and L. J. Cao13 February 2018 | Journal of Guidance, Control, and Dynamics, Vol. 41, No. 4 What's Popular Volume 40, Number 8August 2017 CrossmarkInformationCopyright © 2017 by Peng Lu. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0731-5090 (print) or 1533-3884 (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsActuatorsAerodynamic PerformanceAerodynamicsAeronautical EngineeringAeronauticsAirspeedAviationAvionicsCivil AviationControl TheoryFault Detection and IsolationGuidance, Navigation, and Control SystemsSensorsSlip (Aerodynamics)Transducers KeywordsSensorsActuatorsFlight Control SystemFault Detection and DiagnosisControl SurfacesUnscented Kalman FilterLinear Time Invariant SystemAerodynamic CoefficientsIMUAttitude DynamicsPDF Received26 February 2016Accepted17 March 2017Published online2 June 2017

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