Automatic alignment and calibration of an inertial navigation system
In this paper we derive a simple six degree of freedom navigator, Earth-surface navigator, for terranean vehicle application, using low grade gyros. The calibration and alignment of the navigator are investigated when the system is at rest. Based on the observability of the error model when the syst...
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| Format: | conferenceObject |
| Published: |
1994
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| Online Access: | http://hdl.handle.net/10725/11206 http://dx.doi.org/10.1109/PLANS.1994.303400 http://libraries.lau.edu.lb/research/laur/terms-of-use/articles.php https://ieeexplore.ieee.org/abstract/document/303400 |
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