Optimization-based alignment for inertial navigation systems: Theory and algorithm
Inertial navigation system (INS) necessitates an alignment stage to determine the initial attitude at the very start. A novel alignment approach is devised by way of an optimization method, in contrast to the existing alignment methods, e.g., gyrocompassing and filtering techniques. This paper shows...
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| Published in: | Aerospace science and technology Vol. 15; no. 1; pp. 1 - 17 |
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| Main Authors: | , , , |
| Format: | Journal Article |
| Language: | English |
| Published: |
Issy-les-Moulineaux
Elsevier SAS
01.01.2011
Elsevier |
| Subjects: | |
| ISSN: | 1270-9638, 1626-3219 |
| Online Access: | Get full text |
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