文件名称:gyro_EKF
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Aiming at determining the satellite attitude precisely，the gyros bias and m isa lignment were compensated in time by using the quaternion of star-sensor and extended Kalm an filter．The related module of the filter was derived．The theoretic accuracy of the algorithm was acquired from the numerical simulation． The effects of the star-senso r
misalignment on attitude determination were analyzed at last．
misalignment on attitude determination were analyzed at last．
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gyro_EKF.pdf