This content is not included in your SAE MOBILUS subscription, or you are not logged in.

Linearization of Aircraft Landing Equations of Motion with Airframe Flexibility Effects

Journal Article
01-15-01-0002
ISSN: 1946-3855, e-ISSN: 1946-3901
Published September 21, 2021 by SAE International in United States
Linearization of Aircraft Landing Equations of Motion with Airframe Flexibility Effects
Sector:
Citation: null
Language: English

References

  1. Krüger , W. Design and Simulation of Semi-Active Landing Gears for Transport Aircraft Mechanics of Structures and Machines 30 4 2002 493 526
  2. Zapateiro , M. , Pozo , F. , Karimi , H.R. , and Luo , N. Semiactive Control Methodologies for Suspension Control with Magnetorheological Dampers IEEE/ASME Transactions on Mechatronics 17 2 2012 370 380
  3. Yazici , H. and Sever , M. Observer Based Optimal Vibration Control of a Full Aircraft System Having Active Landing Gears and Biodynamic Pilot Model Shock and Vibration 2016 2016 1 20
  4. Wang , H. , Xing , J.T. , Price , W.G. , and Li , W. An Investigation of an Active Landing Gear System to Reduce Aircraft Vibrations Caused by Landing Impacts and Runway Excitations Journal of Sound and Vibration 317 1 2008 50 66
  5. Sivakumar , S. and Haran , A.P. Mathematical Model and Vibration Analysis of Aircraft with Active Landing Gears Journal of Vibration and Control 21 2 2015 229 245
  6. Zarchi , M. and Attaran , B. Performance Improvement of an Active Vibration Absorber Subsystem for an Aircraft Model Using a Bees Algorithm Based on Multi-Objective Intelligent Optimization Engineering Optimization 49 11 2017 1905 1921
  7. Zarchi , M. and Attaran , B. Improved Design of an Active Landing Gear for a Passenger Aircraft Using Multi-Objective Optimization Technique Structural and Multidisciplinary Optimization 59 5 2019 1813 1833
  8. Li , Y. , Jiang , J.Z. , Neild , S.A. , and Wang , H. Optimal Inerter-Based Shock-Strut Configurations for Landing-Gear Touchdown Performance Journal of Aircraft 54 5 2017 1901 1909
  9. Li , Y. , Jiang , J.Z. , Sartor , P. , Neild , S.A. et al. Including Inerters in Aircraft Landing Gear Shock Strut to Improve the Touch-Down Performance Procedia Engineering 199 2017 1689 1694
  10. Stachiw , T.A. , Khouli , F. , Langlois , R.G. , and Afagh , F.F. The Use of an Inerter in an Aircraft Landing Gear Suspension for Improved Passenger and Crew Comfort at Touchdown AIAA Scitech 2020 Forum Orlando, FL 2020
  11. Stachiw , T. 2020
  12. Cook , F.E. and Milwitzky , B. 1956
  13. Craig , R.R. and Bampton , M.C.C. Coupling of Substructures for Dynamic Analyses AIAA Journal 6 1968 1313 1319
  14. Pritchard , J. Overview of Landing Gear Dynamics Journal of Aircraft 38 2001 130 137
  15. Krüger , W.R. and Morandini , M. Recent Developments at the Numerical Simulation of Landing Gear Dynamics CEAS Aeronautical Journal 1 1-4 2011 55 68
  16. Cesnik , C.E.S. , Palacios , R. , and Reichenbach , E.Y. Reexamined Structural Design Procedures for Very Flexible Aircraft Journal of Aircraft 51 5 2014 1580 1591
  17. Stachiw , T. , Khouli , F. , Langlois , R.G. , Afagh , F.F. et al. A Computationally Low-Cost Method for Capturing Airframe Flexibility Effects in Landing Dynamic Simulations Journal of Computational and Nonlinear Dynamics 16 4 2021 041004
  18. Herlihy , M. and Shavit , N. The Art of Multiprocessor Programming 1st ed. Burlington Elsevier 2015 536
  19. Juang , J.G. , Chang , H.H. , and Cheng , K.C. Intelligent Landing Control Using Linearized Inverse Aircraft Model Proceedings of the American Control Conference 4 2002 3269 3274
  20. Juang , J.-G. and Chio , J.-Z. Fuzzy Modelling Control for Aircraft Automatic Landing System International Journal of Systems Science 36 2005 77 87
  21. Prasad , B. and Pradeep , S. Automatic Landing System Design Using Feedback Linearization Method AIAA Infotech@Aerospace 2007 Conference and Exhibit Rohnert Park, CA 2007
  22. Menon , P.K. , Vaddi , S.S. , and Sengupta , P. Robust Landing-Guidance Law for Impaired Aircraft Journal of Guidance, Control, and Dynamics 35 6 2012 1865 1877
  23. Xia , G. , Dong , R. , Xu , J. , and Zhu , Q. Linearized Model of Carrier-Based Aircraft Dynamics in Final-Approach Air Condition Journal of Aircraft 53 2016 33 47
  24. Khapane , P.D. Simulation of Asymmetric Landing and Typical Ground Maneuvers for Large Transport Aircraft Aerospace Science and Technology 7 2003 611 619
  25. Bronstein , M. , Feldman , E. , Vescovini , R. , and Bisagni , C. Assessment of Dynamic Effects on Aircraft Design Loads: The Landing Impact Case Progress in Aerospace Sciences 78 2015 131 139
  26. Cumnuantip , S. and Krüger , W.R. Assessment of Dynamic Landing Loads by a Hybrid Multibody/Full Finite Element Simulation Approach German Aerospace Congress 2018 Bremen, Germany 2018
  27. Federal Aviation Administration and Department of Transportation 2020
  28. Milwitzky , B. and Cook , F.E. Analysis of Landing-Gear Behavior Washington, DC National Advisory Committee for Aeronautics 1952
  29. Yadav , D. and Ramamoorthy , R.P. Nonlinear Landing Gear Behavior at Touchdown Journal of Dynamic Systems, Measurement, and Control 113 4 1991 677 683
  30. Ijff , J. 1972
  31. Kiébré , R. 2010
  32. Pacejka , H.B. Tire and Vehicle Dynamics 3rd Amsterdam Butterworth-Heinemann 2012 672
  33. Fiala , E. Seitenkraften am rollenden Luftreifen VDI 96 1954 973 979
  34. Daugherty , R.H. A Study of the Mechanical Properties of Modern Radial Aircraft Tires Hampton Langley Research Center 2003
  35. Barnes , A. and Yager , T. 1998
  36. Currey , N.S. Aircraft Landing Gear Design: Principles and Practices Washington DC American Institute of Aeronautics and Astronautics 1988
  37. Lernbeiss , R. and Plöchl , M. Simulation Model of an Aircraft Landing Gear Considering Elastic Properties of the Shock Absorber Proceedings of the Institution of Mechanical Engineers, Part K: Journal of Multi-Body Dynamics 221 1 2007 77 86

Cited By