Magnetic Torquer Attitude Control of a Satellite Via the Linear Quadratic Regulation and the State-Dependent Riccati Equation Technique

  • Oh Jong-Hyun (CAST, Department of Astronomy and Space Science, Yonsei University) ;
  • Park Sang-Young (CAST, Department of Astronomy and Space Science, Yonsei University) ;
  • Choi Kyu-Hong (CAST, Department of Astronomy and Space Science, Yonsei University)
  • Published : 2005.10.01