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Dohee Kim

Dohee Kim received his B.S. Degree in 2006 and his M.S. degree in 2008 in Dept. of Astronomy from Yonsei University, Korea. In his thesis, he designed and developed Hardware-In-the-Loop(HIL) simulator for spacecraft attitude control (Movie). He has a big interest about validation of nonlinear controller using hardware systems, optimal control, and various filtering techniques. He is currently a Doctoral student in the Nonlinear Control and Robotics Group in the Department of Mechanical and Aerospace Engineering under the advisement of Dr. Warren Dixon.
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Journal Papers

  1. D. Kim, H. T. Chung, S. Bhasin, and W. E. Dixon,"Composite Adaptive Fuzzy Identification and Control for a Class of MIMO Nonlinear Systems," In preparation
  2. D. Kim, F. Leve, N. Fitz-Coy, and W. E. Dixon,"Integrated Power Reduction and Adaptive Attitude Control System of a VSCMG-based Satellite," AIAA Journal of Guidance, Control, and Dynamics, to be submitted
  3. D. Kim, F. A. Leve, N. Fitz-Coy and W. E. Dixon, “A New Initial Start-up Method Using Momentum Management” AIAA Journal of Guidance, Control, and Dynamics, to be submitted
  4. D. Kim, W. Mackunis, N. Fitz-Coy and W. E. Dixon, “Precision IPACS in the Presence of Dynamic Uncertainty” AAS The Journal of the Astronautical Sciences, to appear.
  5. D. Koh, S. Park, D. Kim, and K. Choi, “Development of a Hardware-In-the Loop (HIL) Simulator for Spacecraft Attitude Control Using Thrusters” Journal of Astronomy and Space Sciences. Vol. 26, no. 1, 47-58
  6. D. Kim, S. Park, J. Kim, and K. Choi, “Development of a Hardware-In-the Loop (HIL) Simulator for Spacecraft Attitude Control Using Momentum Wheels” Journal of Astronomy and Space Sciences. Vol. 25, no. 4, 347-360

Conference Papers

  1. D. Kim, H. Dinh, W. MacKunis, N. Fitz-Coy, and W. E. Dixon,"A Recurrent Neural Network (RNN)-based Attitude Control Method for a VSCMG-actuated Satellite," IEEE Conference on Decision and Controls, Orlando, FL, 2011, submitted.
  2. H. Dinh, S. Bhasin, D. Kim, and W. E. Dixon,"Dynamic Neural Network-based Global Output Feedback Tracking Control for Uncertain Second-Order Nonlinear Systems," IEEE Conference on Decision and Controls, Orlando, FL, 2011, submitted.
  3. D. Kim, F. Leve, N. Fitz-Coy, and W. E. Dixon,"Integrated Power Reduction and Adaptive Attitude Control System of a VSCMG-based Satellite," 21st AAS/AIAA Space Flight Mechanics Meeting, New Orleans, LA, 2011, AAS 11-136.
  4. D. Kim, F. Leve, N. Fitz-Coy, and W. E. Dixon,"Adaptive Attitude Control for a Small Satellite with Integrated Singularity Avoidance and Momentum Management," American Control Conference, San Francisco, CA, 2011, to appear.
  5. D. Kim, H. T. Chung, S. Bhasin, and W. E. Dixon,"Composite Adaptive Fuzzy Identification and Control for a Class of MIMO Nonlinear Systems," American Control Conference, San Francisco, CA, 2011, to appear.
  6. D. Kim, W. Mackunis, N. Fitz-Coy and W. E. Dixon, “Precision IPACS in the Presence of Dynamic Uncertainty” Proceedings of IEEE Conference on Decision and Control, Shanghai, China, 2009, pp. 5959-5964.

Thesis

  1. D. Kim, "Design and Development of Hardware-In-the-Loop (HIL) Simulator for Spacecraft Attitude Control Using Air-Bearing System" Master of Science Thesis, Department of Astronomy, Yonsei University, December 2007.