Control of Aerodynamic-Driven Morphing

No AccessEngineering NotesControl of Aerodynamic-Driven MorphingLiangtao Feng, Tingyu Guo, Chenhua Zhu and Haixin ChenLiangtao Feng https://orcid.org/0000-0002-9145-3456Tsinghua University, 100084 Beijing, People’s Republic of China*Ph.D. Student, School of Aerospace Engineering; .Search for more papers by this author, Tingyu GuoTsinghua University, 100084 Beijing, People’s Republic of China†Ph.D. Student, School of Aerospace Engineering; .Search for more papers by this author, Chenhua ZhuTsinghua University, 100084 Beijing, People’s Republic of China‡Ph.D. Student, School of Aerospace Engineering; .Search for more papers by this author and Haixin ChenTsinghua University, 100084 Beijing, People’s Republic of China§Professor, School of Aerospace Engineering; . Associate Fellow AIAA (Corresponding Author).Search for more papers by this authorPublished Online:26 Sep 2022https://doi.org/10.2514/1.G006906SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Gu H., Healy F., Rezgui D. and Cooper J. E., “Sizing of High Aspect Ratio Wings with Folding Wing Tips,” AIAA SciTech 2022 Forum, AIAA Paper 2022-0723, Jan. 2022. https://doi.org/10.2514/6.2022-0723 LinkGoogle Scholar[2] Yavrucuk I. and Kargin V., “Auto Landing Strategies for a Fixed Wing UAV in Adverse Atmospheric Conditions,” AIAA Guidance, Navigation and Control Conference and Exhibit, AIAA Paper 2008-6963, Aug. 2008. https://doi.org/10.2514/6.2008-6963 LinkGoogle Scholar[3] Xiaopeng Z. and Haixin C., “Conceptual Design of Self-Expanding/Folding Extremely Large Aspect Ratio Wing Airplane,” European Conference for Aeronautics and Space Sciences, EUCASS2017-209, Belgium, 2015. https://doi.org/10.13009/EUCASS2017-209 Google Scholar[4] Olson E. C. and Selberg B. P., “Experimental Determination of Improved Aerodynamic Characteristics Utilizing Biplane Wing Configurations,” Journal of Aircraft, Vol. 13, No. 4, 1976, pp. 256–261. https://doi.org/10.2514/3.44523 LinkGoogle Scholar[5] Guo T., Feng L., Zhu C., Zhou X. and Chen H., “Conceptual Research on a Mono-Biplane Aerodynamics-Driven Morphing Aircraft,” Aerospace, Vol. 9, No. 7, 2022, Paper 380. https://doi.org/10.3390/aerospace9070380 Google Scholar[6] Seigler T. M., “Dynamics and Control of Morphing Aircraft,” Ph.D. Dissertation, Dept. of Mechanical Engineering, Virginia Polytechnic Inst. and State Univ., Blacksburg, VA, Aug. 2005. Google Scholar[7] Meirovitch L. and Tuzcu I., “Integrated Approach to the Dynamics and Control of Maneuvering Flexible Aircraft,” NASA CR-2003-211748, 2003. Google Scholar[8] Yan B., Li Y., Dai P. and Liu S., “Aerodynamic Analysis, Dynamic Modeling, and Control of a Morphing Aircraft,” Journal of Aerospace Engineering, Vol. 32, No. 5, 2019, Paper 04019058. https://doi.org/10.1061/(ASCE)AS.1943-5525.0001047 Google Scholar[9] Avanzini G. and Galeani S., “Robust Antiwindup for Manual Flight Control of an Unstable Aircraft,” Journal of Guidance, Control, and Dynamics, Vol. 28, No. 6, 2005, pp. 1275–1282. https://doi.org/10.2514/1.12004 LinkGoogle Scholar[10] Wen N., Liu Z., Sun Y. and Zhu L., “Design of LPV-Based Sliding Mode Controller with Finite Time Convergence for a Morphing Aircraft,” International Journal of Aerospace Engineering, Vol. 2017, Dec. 2017, Paper 8426348. https://doi.org/10.1155/2017/8426348 Google Scholar[11] Yan B., Dai P., Liu R., Xing M. and Liu S., “Adaptive Super-Twisting Sliding Mode Control of Variable Sweep Morphing Aircraft,” Aerospace Science and Technology, Vol. 92, May 2019, pp. 198–210. https://doi.org/10.1016/j.ast.2019.05.063 CrossrefGoogle Scholar[12] Udwadia F. E. and Wanichanon T., “Control of Uncertain Nonlinear Multi-Body Mechanical Systems,” Journal of Applied Mechanics, Vol. 81, No. 4, 2013, Paper 04120. https://doi.org/10.1115/1.4025399 CrossrefGoogle Scholar[13] Ashrafiuon H. and Erwin R. S., “Sliding Mode Control of Underactuated Multibody Systems and Its Application to Shape Change Control,” International Journal of Control, Vol. 81, No. 12, 2008, pp. 1849–1858. https://doi.org/10.1080/00207170801910409 CrossrefGoogle Scholar[14] Nicassio F., “Shape Prediction of Bistable Plates Based on Timoshenko and Ashwell Theories,” Composite Structures, Vol. 265, Nov. 2021, Paper 113645. https://doi.org/10.1016/j.compstruct.2021.113645 Google Scholar[15] Tantaroudas N. D., Ronch A. D., Badcock K. J., Wang Y. and Palacios R., “Model Order Reduction for Control Design of Flexible Free-Flying Aircraft,” AIAA Atmospheric Flight Mechanics Conference, AIAA Paper 2015-0240, 2015. https://doi.org/10.2514/6.2015-0240 LinkGoogle Scholar[16] Avanzini G., Nicassio F. and Scarselli G., “Reduced-Order Short-Period Model of Flexible Aircraft,” Journal of Guidance, Control, and Dynamics, Vol. 40, No. 8, 2017, pp. 2017–2029. https://doi.org/10.2514/1.G002387 LinkGoogle Scholar[17] Schmidt L. V., “Wing Rock due to Aerodynamic Hysteresis,” Journal of Aircraft, Vol. 16, No. 3, 1979, pp. 129–133. https://doi.org/10.2514/3.58495 LinkGoogle Scholar[18] Gil J. J., Rubio Á. R. and Savall J., “Decreasing the Apparent Inertia of an Impedance Haptic Device by Using Force Feedforward,” IEEE Transactions on Control Systems Technology, Vol. 17, No. 4, 2009, pp. 833–838. https://doi.org/10.1109/TCST.2008.2000984 Google Scholar[19] Weisshaar T. A., “Morphing Aircraft Systems: Historical Perspectives and Future Challenges,” Journal of Aircraft, Vol. 50, No. 2, 2013, pp. 337–353. https://doi.org/10.2514/1.C031456 LinkGoogle Scholar[20] Kress R., “Variable Sweep Wing Design,” Proceedings of the Aircraft Prototype and Technology Demonstrator Symposium, AIAA Paper 1983-1051, March 1983. https://doi.org/10.2514/6.1983-1051 LinkGoogle Scholar[21] Barbarino S., Pecora R., Lecce L., Concilio A., Ameduri S. and De Rosa L., “Airfoil Structural Morphing Based on S.M.A. Actuator Series: Numerical and Experimental Studies,” Journal of Intelligent Material Systems and Structures, Vol. 22, No. 10, 2011, pp. 987–1004. https://doi.org/10.1177/1045389x11416032 CrossrefGoogle Scholar[22] Sofla A. Y. N., Meguid S. A., Tan K. T. and Yeo W. K., “Shape Morphing of Aircraft Wing: Status and Challenges,” Materials and Design, Vol. 31, No. 3, 2010, pp. 1284–1292. https://doi.org/10.1016/j.matdes.2009.09.011 CrossrefGoogle Scholar[23] Oktay T. and Sultan C., “Simultaneous Helicopter and Control-System Design,” Journal of Aircraft, Vol. 50, No. 3, 2013, pp. 911–925. https://doi.org/10.2514/1.C032043 LinkGoogle Scholar[24] Sun Y., Zhang R., Wu Z., Yang C. and Yang Y., “Dynamic Property Test and System Identification of Model Aircraft Actuators,” Journal of Beijing University of Aeronautics and Astronautics, Vol. 46, No. 2, 2020, pp. 294–303. https://doi.org/10.13700/j.bh.1001-5965.2019.0202 Google Scholar[25] Seigler T. M., Neal D. A., Bae J.-S. and Inman D. J., “Modeling and Flight Control of Large-Scale Morphing Aircraft,” Journal of Aircraft, Vol. 44, No. 4, 2007, pp. 1077–1087. https://doi.org/10.2514/1.21439 LinkGoogle Scholar[26] Liu J., Sliding Mode Control Using MATLAB, 3rd ed., Tsinghua Press, Beijing, 2015, Chaps. 2, 3. Google Scholar[27] Polycarpou M. M. and Ioannou P. A., “A Robust Adaptive Nonlinear Control Design,” 1993 American Control Conference, Inst. of Electrical and Electronics Engineers, New York, 1993, pp. 1365–1369. https://doi.org/10.23919/ACC.1993.4793094 Google Scholar[28] Liu J. K. and Sun F. C., “Research and Development on Theory and Algorithms of Sliding Mode Control,” Control Theory and Applications, Vol. 23, No. 3, 2007, pp. 407–418. Google Scholar Previous article Next article FiguresReferencesRelatedDetails What's Popular Volume 46, Number 1January 2023 CrossmarkInformationCopyright © 2022 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 1533-3884 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsActuatorsAerodynamicsAeronautical EngineeringAeronauticsAircraft ControlAircraft DesignAircraft Flight Control SystemAircraft OperationsAircraft Operations and TechnologyAircraft Stability and ControlAircraft Wing DesignAircraftsAvionicsControl TheoryFixed-Wing AircraftFlight Control SurfacesFluid DynamicsGuidance, Navigation, and Control SystemsTakeoff and LandingWing ConfigurationsWing Planforms KeywordsState Space RepresentationLift ForcesBiplaneControl SurfacesHigh Aspect RatioActuatorsFlight ControlTake off and LandingAirplaneUnsteady FlowsAcknowledgmentThis research was funded by the National Natural Science Foundation of China through grant number 92052203.PDF Received19 April 2022Accepted30 August 2022Published online26 September 2022