Effects of Covariance Modeling on Estimation Accuracy in an IMU-based Attitude Estimation Kalman Filter
نویسندگان
چکیده
منابع مشابه
Kalman Filter for Spinning Spacecraft Attitude Estimation
This paper presents a Kalman filter using a seven-component attitude state vector comprising the angular momentum components in a n inertial reference frame, the angular momentum components in the body frame, and a rotation angle. The relatively slow variation of these parameters makes this parameterization advantageous for spinning spacecraft attitude estimation. The filter accounts for the co...
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ژورنال
عنوان ژورنال: JOURNAL OF SENSOR SCIENCE AND TECHNOLOGY
سال: 2020
ISSN: 1225-5475,2093-7563
DOI: 10.46670/jsst.2020.29.6.440