Mathematical Model and Matlab Simulation of Strapdown Inertial Navigation System
Basic principles of the strapdown inertial navigation system (SINS) using the outputs of strapdown gyros and accelerometers are explained, and the main equations are described. A mathematical model of SINS is established, and its Matlab implementation is developed. The theory is illustrated by six e...
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| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Wiley
2012-01-01
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| Series: | Modelling and Simulation in Engineering |
| Online Access: | http://dx.doi.org/10.1155/2012/264537 |
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| Summary: | Basic principles of the strapdown inertial navigation system (SINS) using the outputs of strapdown gyros and
accelerometers are explained, and the main equations are described. A mathematical model of SINS is established,
and its Matlab implementation is developed. The theory is illustrated by six examples which are static status, straight
line movement, circle movement, s-shape movement, and two sets of real static data. |
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| ISSN: | 1687-5591 1687-5605 |