A Simple Attitude Unscented Kalman Filter: Theory and Evaluation in a Magnetometer-Only Spacecraft Scenario

A Simple Attitude Unscented Kalman Filter: Theory and Evaluation in a Magnetometer-Only Spacecraft Scenario

A quaternion-based attitude unscented Kalman filter is formulated with quaternion errors parameterized by small angle approximations and is applied to a filter with a state vector consisting of the attitude quaternion and the gyro bias vector. The filter is evaluated using extensive Monte Carlo data...

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Bibliographic Details
Main Authors: Murty S. Challa, Jay G. Moore, Daniel J. Rogers
Format: Article
Language:English
Published: IEEE 2016-01-01
Series:IEEE Access
Subjects:
attitude control
calibration
geomagnetism
gyroscopes
Kalman filters
spacecraft
Online Access:https://ieeexplore.ieee.org/document/7460892/

Internet

https://ieeexplore.ieee.org/document/7460892/

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