The Strong Tracking Augmented Kalman Filter for Satellite Attitude Determination
نویسنده
چکیده
For parameter estimations, we have developed a extended kalman filter(EKF) and unscented kalman filter(UKF) for linear as well as non-linear spacecraft systems. We have described the differences of two approaches mathematical equation for modeling of the system value of mean square error, error covariance and For state estimation of satellite, two different type of filters has been described i.e, extended kalman standard deviation are proposed to be used for determining the accuracy of implemented method.
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