Kalman-Filter-Based Adaptive Control: Flight Testing on General Aviation Aircraft
2017; American Institute of Aeronautics and Astronautics; Volume: 40; Issue: 9 Linguagem: Inglês
10.2514/1.g002693
ISSN1533-3884
AutoresMelvin Rafi, James E. Steck, John Watkins,
Tópico(s)Risk and Safety Analysis
ResumoNo AccessThe Kalman Filter and Its Aerospace ApplicationsKalman-Filter-Based Adaptive Control: Flight Testing on General Aviation AircraftMelvin Rafi, James E. Steck and John WatkinsMelvin RafiWichita State University, Wichita, Kansas 67260*Graduate Research Assistant, Aerospace Engineering. Student Member AIAA.Search for more papers by this author, James E. SteckWichita State University, Wichita, Kansas 67260†Professor, Aerospace Engineering. Associate Fellow AIAA.Search for more papers by this author and John WatkinsWichita State University, Wichita, Kansas 67260‡Professor and Chair, Electrical Engineering and Computer Science.Search for more papers by this authorPublished Online:7 Aug 2017https://doi.org/10.2514/1.G002693SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Yodo N. and Wang P., “Resilience Modeling and Quantification for Engineered Systems Using Bayesian Networks,” Journal of Mechanical Design, Vol. 138, No. 3, Jan. 2016, Paper 031404. doi:https://doi.org/10.1115/1.4032399 CrossrefGoogle Scholar[2] Yodo N. and Wang P., “Engineering Resilience Quantification and System Design Implications: A Literature Survey,” Journal of Mechanical Design, Vol. 138, No. 11, Sept. 2016, Paper 111408. doi:https://doi.org/10.1115/1.4034223 CrossrefGoogle Scholar[3] Kim B. and Calise A., “Nonlinear Flight Control Using Neural Networks,” Guidance, Navigation, and Control Conference and Exhibit, AIAA Paper 1994-3646-CP, Aug. 1994. doi:https://doi.org/10.2514/6.1994-3646 LinkGoogle Scholar[4] Rokhsaz K., Steck J. and Shue S., “Longitudinal Flight Control Decoupling Using Artificial Neural Networks,” 32nd Aerospace Sciences Meeting and Exhibit, AIAA Paper 1994-0274, Jan. 1994. doi:https://doi.org/10.2514/6.1994-274 LinkGoogle Scholar[5] Kim B. and Calise A., “Nonlinear Flight Control Using Neural Networks,” Journal of Guidance, Control, and Dynamics, Vol. 20, No. 1, 1997, pp. 26–33. doi:https://doi.org/10.2514/2.4029 JGCODS 0731-5090 LinkGoogle Scholar[6] Schumacher C., “Adaptive Flight Control Using Dynamic Inversion and Neural Networks,” Guidance, Navigation, and Control Conference and Exhibit, AIAA Paper 1999-4086, Aug. 1999. doi:https://doi.org/10.2514/6.1999-4086 LinkGoogle Scholar[7] Balakrishnan S. and Esteban S., “Nonlinear Flight Control System with Neural Networks,” Atmospheric Flight Mechanics Conference and Exhibit, AIAA Paper 2001-4257, Aug. 2001. doi:https://doi.org/10.2514/6.2001-4257 LinkGoogle Scholar[8] Steck J., Rokhsaz K. and Shue S.-P., “Linear and Neural Network Feedback for Flight Control Decoupling,” IEEE Control Systems Magazine, Vol. 16, No. 4, Aug. 1996, pp. 22–30. doi:https://doi.org/10.1109/37.526912 ISMAD7 0272-1708 CrossrefGoogle Scholar[9] Steck J. E., Rokhsaz K., Pesonen U. J. and Duerksen N., “An Advanced Flight Control System for General Aviation Application,” General Aviation Technology Conference and Exhibit, Soc. of Automotive Engineers Paper SAE-2004-01-1807, Warrendale, PA, April 2004. doi:https://doi.org/10.4271/2004-01-1807 Google Scholar[10] Pesonen U. J., Steck J. E., Rokhsaz K., Bruner S. and Duerksen N., “Adaptive Neural Network Inverse Controller for General Aviation Safety,” AIAA 41st Aerospace Sciences Meeting and Exhibit, AIAA Paper 2003-0573, Jan. 2003. doi:https://doi.org/10.2514/6.2003-578 LinkGoogle Scholar[11] Steck J., Rokhsaz K., Namuduri K. and Bruner S., “Exploring Critical Flight Conditions, Controller Modes, and Parameter Estimation for Adaptive Flight Controls in General Aviation Aircraft,” Federal Aviation Administration Final Rept. DOT/FAA/AR-01-C-AW-WISU-50, May 2006. Google Scholar[12] Hinson B. T., Steck J. E. and Rokhsaz K., “Adaptive Control of an Elastic General Aviation Aircraft,” AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA Paper 2011-6560, Aug. 2011. doi:https://doi.org/10.2514/6.2011-6560 LinkGoogle Scholar[13] Lemon K. A., Steck J. E. and Hinson B. T., “Model Reference Adaptive Fight Control Adapted for General Aviation: Controller Gain Simulation and Preliminary Flight Testing on a Bonanza Fly-By-Wire Testbed,” AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA Paper 2010-8278, Aug. 2010. doi:https://doi.org/10.2514/6.2010-8278 LinkGoogle Scholar[14] Rokhsaz K., Steck J. E., Chandramohan R. and Singh B., “Response of an Advanced Flight Control System to Microburst Encounters,” SAE AeroTech Congress and Exhibit, Soc. of Automotive Engineers Paper SAE-2005-01-3420, Warrendale, PA, Oct. 2005. doi:https://doi.org/10.4271/2005-01-3420 Google Scholar[15] Rafi M., Steck J. E. and Rokhsaz K., “A Microburst Response and Recovery Scheme Using Advanced Flight Envelope Protection,” AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA Paper 2012-4444, Aug. 2012. doi:https://doi.org/10.2514/6.2012-4444 LinkGoogle Scholar[16] Rafi M. and Steck J. E., “Response and Recovery of an MRAC Advanced Flight Control System to Wake Vortex Encounters,” AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA Paper 2013-5209, Aug. 2013. doi:https://doi.org/10.2514/6.2013-5209 LinkGoogle Scholar[17] Steck J. E., Rokhsaz K., Pesonen U. J., Mochrie S. and Maxfield M., “Pilot Evaluation of an Adaptive Controller on a General Aviation SATS Testbed Aircraft,” AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA Paper 2004-5239, Aug. 2004. doi:https://doi.org/10.2514/6.2004-5239 Google Scholar[18] Pappu V. S. R., Steck J. E., Rajagopal K. and Balakrishnan S. N., “Modified State Observer Based Adaptation of a General Aviation Aircraft—Simulation and Flight Test,” AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA Paper 2014-1297, Jan. 2014. doi:https://doi.org/10.2514/6.2014-1297 Google Scholar[19] Kalman R. E., “A New Approach to Linear Filtering and Prediction Problems,” Journal of Basic Engineering, Vol. 82, No. 1, 1960, pp. 35–45. doi:https://doi.org/10.1115/1.3662552 CrossrefGoogle Scholar[20] Kalman R. E. and Bucy R. S., “New Results in Linear Filtering and Prediction Theory,” Journal of Basic Engineering, Vol. 83, No. 1, 1961, pp. 95–108. doi:https://doi.org/10.1115/1.3658902 CrossrefGoogle Scholar[21] Zarchan P. and Musoff H., Fundamentals of Kalman Filtering: A Practical Approach, 4th ed., Progress in Astronautics and Aeronautics, AIAA, Reston, VA, 2015, pp. 107–163. LinkGoogle Scholar[22] Yucelen T. and Calise A., “A Kalman Filter Optimization Approach to Direct Adaptive Control,” AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2009-5858, Aug. 2009. doi:https://doi.org/10.2514/6.2009-5858 LinkGoogle Scholar[23] Yucelen T. and Calise A., “Kalman Filter Modification in Adaptive Control,” Journal of Guidance, Control, and Dynamics, Vol. 33, No. 2, March 2010, pp. 426–439. doi:https://doi.org/10.2514/1.45307 JGCODS 0731-5090 LinkGoogle Scholar[24] Chandramohan R., Yucelen T., Calise A., Chowdhary G. and Johnson E., “Experimental Results for Kalman Filter Modification in Adaptive Control,” AIAA [email protected], AIAA Paper 2010-3300, April 2010. doi:https://doi.org/10.2514/6.2010-3300 LinkGoogle Scholar[25] Chandramohan R., Yucelen T., Calise A., Chowdhary G. and Johnson E., “Flight Test Results for Kalman Filter and H2 Modification in Adaptive Control,” AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2010-7574, Aug. 2010. doi:https://doi.org/10.2514/6.2010-7574 LinkGoogle Scholar[26] Rafi M., Steck J. E. and Watkins J., “Application of a Kalman Filter for Reduction of Sensor/Turbulence-Induced Noise Within a Model Reference Adaptive Controller,” AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2016-1625, Jan. 2016. doi:https://doi.org/10.2514/6.2016-1625 LinkGoogle Scholar[27] Yucelen T., De La Torre G. and Johnson E. N., “Improving Transient Performance of Adaptive Control Architectures Using Frequency-Limited System Error Dynamics,” International Journal of Control, Vol. 87, No. 11, June 2014, pp. 2383–2397. doi:https://doi.org/10.1080/00207179.2014.922702 IJCOAZ 0020-7179 Google Scholar[28] Calise A. and Yucelen T., “Adaptive Loop Transfer Recovery,” Journal of Guidance, Control, and Dynamics, Vol. 35, No. 3, May–June 2012, pp. 807–815. doi:https://doi.org/10.2514/1.55835 JGCODS 0731-5090 LinkGoogle Scholar[29] Miller C. J., “Nonlinear Dynamic Inversion Baseline Control Law: Flight-Test Results for the Full-Scale Advanced Systems Testbed F/A-18 Airplane,” AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2011-6468, Aug. 2011. doi:https://doi.org/10.2514/6.2011-6468 LinkGoogle Scholar[30] Nguyen N., Hanson C., Burken J. and Schaefer J., “Normalized Optimal Control Modification and Flight Experiments on NASA F/A-18 Aircraft,” Journal of Guidance, Control, and Dynamics, Vol. 40, No. 4, July 2016, pp. 1061–1075, doi:https://doi.org/10.2514/1.G001826 LinkGoogle Scholar[31] Chowdhary G. and Johnson E. N., “Flight Test Validation of a Neural Network Based Long Term Learning Adaptive Flight Controller,” AIAA Guidance, Navigation, and Control Conference, AIAA Paper 2009-5854, Aug. 2009. doi:https://doi.org/10.2514/6.2009-5854 LinkGoogle Scholar[32] Beechcraft Bonanza F33A and F33C Acrobatic: Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual, Raytheon Aircraft Company, Wichita, KS, 1996, pp. 1–7, 1–10. Google Scholar[33] Roskam J., Airplane Flight Dynamics and Automatic Flight Controls Pt. 1, DARcorporation, Lawrence, KS, 2001, p. 21. Google Scholar[34] Steck J. E., Rokhsaz K., Pesonen U. J., Singh B. and Chandramohan R., “Effect of Turbulence on an Adaptive Dynamic Inverse Flight Controller,” AIAA [email protected], AIAA Paper 2005-7038, Sept. 2005. doi:https://doi.org/10.2514/6.2005-7038 LinkGoogle Scholar Previous article Next article FiguresReferencesRelatedDetailsCited byA Limited Evaluation of a Model-Free Control Law SystemShawn S. Stephens, Maximo Navarro, Kota Ban, Jacob Anthony Fischer, Marc-Antoine Pelletier, Timothy Sick, Marcus Trautschold, M Christopher Cotting and Agamemnom Crassidis19 January 2023Detection of critical mode-shapes in flexible multibody system dynamics: The case study of a racing motorcycleMechanical Systems and Signal Processing, Vol. 180Nonlinear Filter and Neural Modeling for Calibration of Aircraft Airdata SystemMajeed Mohamed and Nidhin Joy13 October 2021 | Journal of Aerospace Information Systems, Vol. 18, No. 12Online Adaptive Kalman Filter for Target Tracking With Unknown Noise StatisticsIEEE Sensors Letters, Vol. 5, No. 3Sensor placement and moving horizon state/parameter estimation for flexible hypersonic vehicles11 February 2019 | Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 233, No. 13Hybrid Kalman Filtering Algorithm With Stochastic Nonlinearities and Multiple Missing MeasurementsIEEE Access, Vol. 7 What's Popular Volume 40, Number 9September 2017Special Issue on The Kalman Filter and Its Aerospace Applications CrossmarkInformationCopyright © 2017 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 ISSN 0731-5090 (print) or 1533-3884 (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAerodynamic PerformanceAerodynamicsAeronautical EngineeringAeronauticsAircrewAirspeedAviationAviation SafetyCivil AviationCommercial AviationFlight TestTurbulenceTurbulence Models KeywordsKalman FilterFlight TestingAircraftsModel Reference Adaptive ControlGeneral AviationAirspeedFlight Path AngleNeural NetworksFlying WiresTextron AviationAcknowledgmentThis material is based upon work supported by NASA under award number NNXO9AP20A. Any opinions, findings, and conclusions or recommendations expressed in this material are those of the authors and do not necessarily reflect the views of NASA.PDF Received26 December 2016Accepted10 July 2017Published online7 August 2017
Referência(s)