Hyun-Shik Oh, Dong-Wan Yoo, Byung-Yoon Lee, Gun-Hee Moon, and Min-Jea Tahk


  1. [1] H.C. Curtiss and F.W. Warburton, Stability and control of thetwin lift helicopter system, Journal of the American HelicopterSociety, 30(2), 1985, 14–23.
  2. [2] M. Mittal and J.V.R. Prasad, Three-dimensional modeling andcontrol of a twin-lift helicopter system, Journal of Guidance,Control, and Dynamics, 16(1), 1993, 86–95.
  3. [3] I. Maza, K. Kondak, M. Bernard, and A. Ollero, Multi-UAV cooperation and control for load transportation anddeployment, Journal of Intelligent and Robotic Systems, 57(1),2010, 417–449.
  4. [4] Y. Song, J.F. Horn, Z. Li, and J.W. Langelaan, Modeling,Simulation and non-linear control of a rotorcraft multi-liftsystem, American Helicopter Society 69th Annual Forum,American Helicopter Society, Phoenix, AZ, May 21–23, 2013,2695–2714.
  5. [5] Z. Li, J.F. Horn, and J.W. Langelaan, Coordinated transportof a slung load by a team of autonomous rotorcraft, AIAAGuidance, Navigation, and Control Conference, AmericanInstitute of Aeronautics and Astronautics, Maryland, USA,2014, 1–23. http://arc.aiaa.org/doi/10.2514/6.2014-0968.
  6. [6] M. Bisgaard, J.D. Bendtsen, and A.l. Cour-Harbo, Modelingof generic slung load system, Journal of Guidance, Control,and Dynamics, 32(2), 2009, 13.
  7. [7] T. Ronen, A.E. Bryson, and W.S. Hindson, Dynamics ofa helicopter with a sling load, AIAA Atmospheric FlightMechanics Conference, (Williamsburg, Va.) AIAA Paper 86-2288, 1986, 1–13.
  8. [8] L.S. Cicolani and G. Kanning, Equations of motion of slungloadsystems, including multi-lift systems, NASA, TP-3280 1992,24–35.
  9. [9] F.E. Udwadia and R.E. Kalaba, A new perspective on con-strained motion, Proceedings: Mathematical and Physical Sci-ences, Vol. 439, Issue 1906 (The Royal Society, 1992), 407–410.
  10. [10] F.E. Udwadia and R.E. Kalaba, Equations of motion formechanical systems, Journal of Aerospace Engineering, 9(3),1996, 6.
  11. [11] A.A. Rodriquez and M. Athans, Multivariable control of a twinlift helicopter system using the LQG/LTR design methodology,American Controls Conference, Seattle, Washington, USA,June 1986, 1325–1332.
  12. [12] P.K. Menon, J.V.R. Prasad, and D.P. Schrage, Nonlinear con-trol of a twin-lift helicopter configuration, Journal of Guidance,Control and Dynamics, 14(6), 1991, 1287–1293.
  13. [13] J.V.R. Prasad, M. Mittal, and D.P. Schrage, Control of a twin-lift helicopter system using nonlinear state feedback, Journalof the American Helicopter Society, 36(4), 1991, 57–65.
  14. [14] M. Mittal, J.V.R. Prasad, and D.P. Schrage, Nonlinear adaptivecontrol of a twin lift helicopter system, IEEE Control Systems,11(3), 1991, 39–45.
  15. [15] H.-I. Lee, D.-W. Yoo, B.-Y. Lee, G.-H. Moon, D.-Y. Lee,and M.-J. Tahk, LQG/LTR-PID based controller design ofUAV slung-load transportation system, Journal of Institute ofControl, Robotics and Systems, 20(12), 2014, 1209–1216.
  16. [16] F.E. Udwadia and R.E. Kalaba, On the foundations of analyti-cal dynamics, International Journal of Non-Linear Mechanics,37, 2002, 12.
  17. [17] A.M. Lekkas, Guidance and path-planning systems for au-tonomous vehicles,Ph.D. Thesis, Norwegian University of Sci-ence and Technology, Trondheim, 2014, 220.

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