Dual Extended Kalman Filter Based Momentum Wheel Identification
As the most important actuator of the attitude control subsystem of the spacecraft, the momentum wheel should be precisely simulated. In this paper, Dual Extended Kalman filter is expressed and used to identify the momentum wheel system. In this way, the identification result can be used in the momentum wheel system simulation. This makes simulations run both fast and precisely. The numerical simulation results show that the algorithm can converge in given error.
Z. Z. Li et al., "Dual Extended Kalman Filter Based Momentum Wheel Identification", Applied Mechanics and Materials, Vols. 29-32, pp. 2278-2284, 2010