Optimal configuration of redundant inertial sensors for navigation and FDI performance

This paper considers the optimal sensor configuration for inertial navigation systems which have redundant inertial sensors such as gyroscopes and accelerometers. We suggest a method to determine the optimal sensor configuration which considers both the navigation and FDI performance. Monte Carlo si...

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Bibliographic Details
Published inSensors (Basel, Switzerland) Vol. 10; no. 7; pp. 6497 - 6512
Main Authors Shim, Duk-Sun, Yang, Cheol-Kwan
Format Journal Article
LanguageEnglish
Published Switzerland MDPI AG 01.07.2010
Molecular Diversity Preservation International (MDPI)
Subjects
Accelerometers
Aircraft
fault detection and isolation
FDI performance
Geographic Information Systems
icosahedrons
Localization
Monte Carlo Method
navigation performance
Navigation systems
optimal sensor configuration
platonic solid
redundant inertial sensor
Sensors
optimal sensor configuration
platonic solid
FDI performance
icosahedrons
redundant inertial sensor
fault detection and isolation
navigation performance
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Summary:This paper considers the optimal sensor configuration for inertial navigation systems which have redundant inertial sensors such as gyroscopes and accelerometers. We suggest a method to determine the optimal sensor configuration which considers both the navigation and FDI performance. Monte Carlo simulations are performed to show the performance of the suggested optimal sensor configuration method.
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ISSN:1424-8220
1424-8220
DOI:10.3390/s100706497