NASA NTRS · 20030020625
A Nonlinear Observer for Gyro Alignment Estimation
Abstract
A nonlinear observer for gyro alignment estimation is presented. The observer is composed of two error terms, an attitude error and an alignment error. The observer is globally stable with exponential convergence of the attitude errors. The gyro alignment estimate converges to the true alignment when the system is completely observable.
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Thienel, J., Sanner, R. M.. 2003-01-01. A Nonlinear Observer for Gyro Alignment Estimation. https://ntrs.nasa.gov/citations/20030020625
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