Efficient Linear Modeling Method of Carrier Landing Flight Dynamics

Abstract

No AccessEngineering NotesEfficient Linear Modeling Method of Carrier Landing Flight DynamicsRan Dong, Xingchao Shao, Lipeng Wang, Guoxin Zhao and Xinyi ZhouRan DongBeijing Institute of Petrochemical Technology, 102617 Beijing, People’s Republic of China*Lecturer, College of Information Engineering; (Corresponding Author).Search for more papers by this author, Xingchao ShaoHarbin Engineering University, 150001 Harbin, Heilongjiang, People’s Republic of China†Lecturer, College of Intelligent Systems Science and Engineering; .Search for more papers by this author, Lipeng WangHarbin Engineering University, 150001 Harbin, Heilongjiang, People’s Republic of China‡Lecturer, College of Intelligent Systems Science and Engineering; .Search for more papers by this author, Guoxin ZhaoBeijing Institute of Petrochemical Technology, 102617 Beijing, People’s Republic of China§Professor, College of Information Engineering; .Search for more papers by this author and Xinyi ZhouBeijing Institute of Petrochemical Technology, 102617 Beijing, People’s Republic of China¶Undergraduate Student, College of Information Engineering; .Search for more papers by this authorPublished Online:30 Aug 2021https://doi.org/10.2514/1.C036404SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Hess R. A., “Providing Flight-Path Control Bandwidth for Carrier Landings,” Journal of Aircraft, Vol. 55, No. 1, 2018, pp. 406–409. https://doi.org/10.2514/1.C034596 LinkGoogle Scholar[2] Zhen Z., Jiang S. and Jiang J., “Preview Control and Particle Filtering for Automatic Carrier Landing,” IEEE Transactions on Aerospace and Electronic Systems, Vol. 54, No. 6, 2018, pp. 2662–2674. https://doi.org/10.1109/TAES.2018.2826398 CrossrefGoogle Scholar[3] Rudowsky T., Cook S., Hynes M., Heffley R., Luter M., Lawrence T., Niewoehner R., Bollman D., Senn P., Durham W., Beaufrere H., Yokell M. and Sonntag A., “Review of the Carrier Approach Criteria for Carrier-Based Aircraft,” U.S. Naval Air Warfare Center, Aircraft Division, NAWCADPAX TR-2002/71, Patuxent River, MD, Oct. 2002. CrossrefGoogle Scholar[4] Xia G., Dong R., Xu J. and Zhu Q., “Linearized Model of Carrier-Based Aircraft Dynamics in Final-Approach Air Condition,” Journal of Aircraft, Vol. 53, No. 1, 2016, pp. 33–47. https://doi.org/10.2514/1.C033175 LinkGoogle Scholar[5] Stevens B. L., Lewis F. L. and Johnson E. N., Aircraft Control and Simulation, 3rd ed., Wiley, New York, 2016, Chap. 3. Google Scholar[6] Wu X. and Zhang S., MATLAB in the Application of Automatic Control, Xidian Univ. Press, Xi’an, PRC, 2013, pp. 250–254. Google Scholar[7] Chaturvedi D. K., Modeling and Simulation of Systems Using Matlab and Simulation, Taylor and Francis, Abingdon, VA, 2010, Appendix B. Google Scholar[8] “Flying Qualities of Pilot Aircraft,” Department of Defense Handbook, U.S. Dept. of Defense Interface Sandard, MIL-HDBK-1797, 1997. Google Scholar[9] Dong R. and Xia G., “Simulation of the Ship Burble in a Cooperative Carrier Approach Pattern,” The 26th Chinese Control and Decision Conference (2014 CCDC), IEEE Publ., Piscataway, NJ, 2014, pp. 1461–1466. Google Scholar[10] Michael R. E. and Blaise G. M., “Nonlinear Six-Degree-of-Freedom Aircraft Trim,” Journal of Guidance, Control, and Dynamics, Vol. 23, No. 2, 2000, pp. 305–311. https://doi.org/10.2514/2.4523 LinkGoogle Scholar[11] Chudoba B. and Cook M., “Trim Equations of Motion for Aircraft Design: Steady State Straight-Line Flight,” AIAA Atmospheric Flight Mechanics Conference and Exhibit, AIAA, Reston, VA, 2003, pp. 1–11; also AIAA Paper 2003-5691, 2003. https://doi.org/10.2514/6.2003-5691 Google Scholar[12] Marco A. D., Duke E. and Berndt J., “A General Solution to the Aircraft Trim Problem,” AIAA Modeling and Simulation Technologies Conference and Exhibit, AIAA, Reston, VA, 2007, pp. 1–40; also AIAA Paper 2007-6703, 2007. https://doi.org/10.2514/6.2007-6703 Google Scholar[13] Etkin B., Dynamics of Atmospheric Flight, Wiley, New York, 1972, pp. 148–188, 529–548. Google Scholar[14] Misra G. and Bai X., “Output-Feedback Stochastic Model Predictive Control for Glideslope Tracking During Aircraft Carrier Landing,” Journal of Guidance, Control, and Dynamics, Vol. 42, No. 9, 2019, pp. 2098–2105. https://doi.org/10.2514/1.G004160 LinkGoogle Scholar[15] Urnes J. M. and Hess R. K., “Development of the FA-18A Automatic Carrier Landing System,” Journal of Guidance, Control, and Dynamics, Vol. 8, No. 3, 1985, pp. 289–295. https://doi.org/10.2514/3.19978 LinkGoogle Scholar Previous article Next article FiguresReferencesRelatedDetails What's Popular Volume 58, Number 5September 2021 CrossmarkInformationCopyright © 2021 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 eISSN 1533-3868 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAerodynamic PerformanceAerodynamicsAeronautical EngineeringAeronauticsAerospace SciencesAircraft Components and StructureAircraft DesignAircraft InstrumentsAircraft Landing SystemsAircraft Operations and TechnologyAircraftsAirspeedFlight DynamicsFlight Mechanics KeywordsFlight Path AngleAerodynamic CoefficientsClosed LoopLift CoefficientAirframesAutomatic Carrier Landing SystemMATLABCarrier Based AircraftFlight VelocityWind Over The DeckAcknowledgmentsThis work was supported by the National Natural Science Foundation of China (no. 61803116) and the Undergraduate Research and Training Program of the Beijing Institute of Petrochemical Technology (no. 2021J00017).PDF Received5 February 2021Accepted28 July 2021Published online30 August 2021