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- W2355892886 abstract "An autonomous attitude determination algorithm based on Unscented Kalman Filter (UKF) for low-Earth orbit(LEO) satellite is developed by processing geomagnetic field measurements.The Earth's magnetic field is well modeled and can be calculated from estimated attitude,orbit parameters and international geomagnetic reference field(IGRF).The difference between the calculated geomagnetic vectors and the measured geomagnetic vectors from the onboard three-axis magnetometer (TAM) is used as updating information,such that the attitude angle and angular velocity can be estimated online.A compared research on UKF and conventional Extended Kalman Filter(EKF) was carried out by means of numerical simulation for three different attitude determination missions which were attitude stabilization,large angle rapid maneuver and attitude loss control.The simulation results show the validity of the proposed approach." @default.
- W2355892886 created "2016-06-24" @default.
- W2355892886 creator A5028870837 @default.
- W2355892886 date "2006-01-01" @default.
- W2355892886 modified "2023-09-26" @default.
- W2355892886 title "UKF for Satellite Attitude Estimation Based on Geomagnetic Field" @default.
- W2355892886 hasPublicationYear "2006" @default.
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