SLUNG-LOAD TRAJECTORY CONTROL USING AN INPUT-SHAPING METHOD WITH MODEL-FOLLOWING CONTROL, 60-75.

Byung-Yoon Lee,∗ Hyun-Shik Oh,∗∗ Min-Jea Tahk,∗∗∗ and Hae-In Lee∗∗∗∗

References

  1. [1] Russian Helicopters Company’s News., Mi-26T completesunique transport mission, 2010, http://www.russianhelicopters.aero/en/rostvertol/news/6590.html.
  2. [2] J. Sessions and W. Chung, An approach to optimizing heli-copter logging operations, in G.J. Arthaud and T.M. Barrett(eds.), Systems Analysis in Forest Resources, vol. 7 (SpringerNetherlands, 2003), 81–86.
  3. [3] K. Stampfer, H. Gridling, and R. Visser, Analyses of parametersaffecting helicopter timber extraction, International Journalof Forest Engineering, 13(2), 2002, 61–68.
  4. [4] M. Bisgaard, A. la Cour-Harbo, and J.D. Bendtsen, Adap-tive control system for autonomous helicopter slung loadoperations, Control Engineering Practice, 18(7), 2010,800–811.
  5. [5] C. Adams, J. Potter, and W. Singhose, Input-shaping andmodel-following control of a helicopter carrying a suspendedload, Journal of Guidance, Control, and Dynamics, 38(1),2015, 94–105.
  6. [6] K. Kang, J.V.R. Prasad, and E. Johnson, Active control of aUAV helicopter with a slung load for precision airborne cargodelivery, Unmanned Systems, 4(3), 2016, 213–226.
  7. [7] H.M. Kim, et al., Initial flight tests of an automatic slungload control system for the ACT/FHS, CEAS AeronauticalJournal, 7(2), 2016, 209–224.
  8. [8] F.A. Goodarzi, D. Lee, and T. Lee, Geometric stabilization ofa quadrotor UAV with a payload connected by flexible cable,American Control Conf. (ACC), 2014, 4925–4930.
  9. [9] I. Palunko, R. Fierro, and P. Cruz, Trajectory generation forswing-free maneuvers of a quadrotor with suspended payload:A dynamic programming approach, Robotics and Automation(ICRA), 2012, 2691–2697.
  10. [10] J. Trachte, F. Gonzalez, and A. McFadyen, Nonlinear modelpredictive control for a multi-rotor with heavy slung load,Unmanned Aircraft Systems (ICUAS), 2014, 1105–1110.
  11. [11] A. Faust, et al., Automated aerial suspended cargo deliverythrough reinforcement learning, Artificial Intelligence, 247,2017, 381–398.
  12. [12] B.Y. Lee, et al., Study on payload stabilization method withthe slung-load transportation system using a quad-rotor, 2015European Control Conf. (ECC), 2015, 2097–2102.
  13. [13] H.S. Oh, et al., Leader steering method for the guidanceand control of multi-lift transportation system, InternationalJournal of Robotics and Automation, 32(5), 2017, 471–481.
  14. [14] H.I. Lee, et al., Parameter-robust linear quadratic Gaussiantechnique for multi-agent slung load transportation, AerospaceScience and Technology, 71, 2017, 119–127.
  15. [15] H. Tourajizadeh, M.H. Korayem, and S.R. Nekoo, Sensitivityanalysis of dynamic load carrying capacity of a cable-suspendedrobot, International Journal of Robotics and Automation,33(1), 2018, 1–11.
  16. [16] M. Trentini and J.K. Pieper, Model-following control of ahelicopter in hover, IEEE International Conference on ControlApplications, 1996, 7–12.
  17. [17] N.C. Singer and W.P. Seering, Preshaping command inputsto reduce system vibration, Journal of Dynamic Systems,Measurement, and Control, 112(1), 1990, 76–82.
  18. [18] T. Singh and W. Singhose, Input shaping/time delay controlof maneuvering flexible structures, American Control Conf.,2002, 1717–1731.
  19. [19] L.D. Morrow and R. Balasubramanian, Real model followingcontrol, Journal of Aircraft, 12(12), 1975, 996–998.
  20. [20] B.Y. Lee, D.W. Yoo, and M.J. Tahk, Performance comparisonof three different types of attitude control systems of the quad-rotor UAV to perform flip maneuver, International JournalAeronautical and Space Sciences, 14(1), 2013, 58–66.
  21. [21] S. Islam, X.P. Liu, and A.E. Saddik, Adaptive sliding modecontrol of unmanned four rotor flying vehicle, InternationalJournal of Robotics and Automation, 30(2), 2015, 140–148.

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