Design of Attitude Estimator and Controller for Multi-Purpose Satellite under Torque Disturbance

Torque Disturbance를 받는 다목적 위성의 자세추정기 및 제어기 설계

  • 김민성 (고려대학교 제어계측공학과) ;
  • 최완식 (한국전자통신연구소) ;
  • 오화석 (한국전자통신연구소) ;
  • 허훈 (고려대학교 제어계측공학과)
  • Published : 1996.04.01

Abstract

Nonlinear Attitude Dynamic Equation for rigid-body satellite is derived and linearzed. Estimator using Kalman filter and controller are designed. Controller using LQR technique implemented on satellite under torque disturbance shows much better performance than those by using of Bang-Bang technique.

Keywords