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 |
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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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| _version_ | 1849412066924822528 |
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| author | Wen Zhang Mounir Ghogho Baolun Yuan |
| author_facet | Wen Zhang Mounir Ghogho Baolun Yuan |
| author_sort | Wen Zhang |
| collection | DOAJ |
| description | 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. |
| format | Article |
| id | doaj-art-5e4fa95e1c594a5894e78c061e49fd5f |
| institution | Kabale University |
| issn | 1687-5591 1687-5605 |
| language | English |
| publishDate | 2012-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | Modelling and Simulation in Engineering |
| spelling | doaj-art-5e4fa95e1c594a5894e78c061e49fd5f2025-08-20T03:34:33ZengWileyModelling and Simulation in Engineering1687-55911687-56052012-01-01201210.1155/2012/264537264537Mathematical Model and Matlab Simulation of Strapdown Inertial Navigation SystemWen Zhang0Mounir Ghogho1Baolun Yuan2College of Opto-Electronic Science and Technology, National University of Defense Technology, Changsha 410073, ChinaSchool of Electronic and Electrical Engineering, University of Leeds, Leeds LS2 9JT, UKCollege of Opto-Electronic Science and Technology, National University of Defense Technology, Changsha 410073, ChinaBasic 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.http://dx.doi.org/10.1155/2012/264537 |
| spellingShingle | Wen Zhang Mounir Ghogho Baolun Yuan Mathematical Model and Matlab Simulation of Strapdown Inertial Navigation System Modelling and Simulation in Engineering |
| title | Mathematical Model and Matlab Simulation of Strapdown Inertial Navigation System |
| title_full | Mathematical Model and Matlab Simulation of Strapdown Inertial Navigation System |
| title_fullStr | Mathematical Model and Matlab Simulation of Strapdown Inertial Navigation System |
| title_full_unstemmed | Mathematical Model and Matlab Simulation of Strapdown Inertial Navigation System |
| title_short | Mathematical Model and Matlab Simulation of Strapdown Inertial Navigation System |
| title_sort | mathematical model and matlab simulation of strapdown inertial navigation system |
| url | http://dx.doi.org/10.1155/2012/264537 |
| work_keys_str_mv | AT wenzhang mathematicalmodelandmatlabsimulationofstrapdowninertialnavigationsystem AT mounirghogho mathematicalmodelandmatlabsimulationofstrapdowninertialnavigationsystem AT baolunyuan mathematicalmodelandmatlabsimulationofstrapdowninertialnavigationsystem |