Sensor Fusion Based on Mathematical Model of LEO Satellite
نویسندگان
چکیده
In this study, the mathematical model of attitude motion is obtained for low orbit sattelite (LEO) with its kinematic and dynamic equations. The LEO satellite using Kepler parameters. Sensor data are generated adding zero mean Gaussian noise to comes from response. These measurement fused INS/GPS integration structure. Extended Kalman filter algorithm used sensor fusion. Compare estimated extended actual model. It has been observed results that closest data. All study performed at MATLAB/Simulink environment.
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ژورنال
عنوان ژورنال: Europan journal of science and technology
سال: 2022
ISSN: ['2148-2683']
DOI: https://doi.org/10.31590/ejosat.1216679