Inertial reference unit in a directional gyro mode of operation

Rohác, J; Šipoš, Martin; Šimánek, Jakub; Teren, Ondrej

doi:10.1109/icsens.2012.6411226

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Cited by 4 publications

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“…If we ch system, we will assume frequ 1227,6 MHz . Operating frequ variable parameters, in the cas [11] is bandwidth of used senso…”

Section: B Gnss Errorsmentioning

confidence: 99%

Integration architectures of navigation systems for unmanned vehicles

Vaispacher

Bréda

Madarasz

2015

2015 IEEE 13th International Symposium on Applied Machine Intelligence and Informatics (SAMI)

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This contribution is part of analysis and research in field of unmanned vehicles navigation developed at Faculty of Aeronautics, Technical University in Kosice. The content of this contribution is an issue of the INS and GNSS integration. Loosely coupled integration architecture was in this case chosen as the basic for simple explanation of the integration issue. Within this contribution the emphasis is focused on suitable Kalman filtering and mathematical background. In the last part of the contribution is given short review on actualization of the basic discrete equations of inertial navigation. I. , , ∆ , 4

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“…If we ch system, we will assume frequ 1227,6 MHz . Operating frequ variable parameters, in the cas [11] is bandwidth of used senso…”

Section: B Gnss Errorsmentioning

confidence: 99%