Development of Inertial Navigation System Using Tactical Grade Sensors

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F15%3A00229835" target="_blank" >RIV/68407700:21230/15:00229835 - isvavai.cz</a>

Výsledek na webu

<a href="http://radio.feld.cvut.cz/conf/poster2015/" target="_blank" >http://radio.feld.cvut.cz/conf/poster2015/</a>

DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

Development of Inertial Navigation System Using Tactical Grade Sensors

Popis výsledku v původním jazyce

The navigation systems which provide the attitude, position and velocity of an object play a key role in many applications. The accuracy of them depends on used sensors. Nowadays, the low-cost MEMS based inertial sensors are used but they are not able toprovide position and velocity as a standalone system and thus they need to be aided by other sources of information. To develop the standalone system, which can provide navigation solution independently, there must be utilized more precise inertial sensors with resolution at least 100 times better than in the case of MEMS. This paper presents the development of inertial navigation system using tactical grade inertial sensors. The proposed system consists of three quartz accelerometers INN-204 with analogue output and three digital fiber optic gyroscopes DSP-3100. The data are preprocessed by means of compensation of deterministic sensors errors, temperature compensation, data decimation and pre-filtering using FIR digital filter. The n

Název v anglickém jazyce

Development of Inertial Navigation System Using Tactical Grade Sensors

Popis výsledku anglicky

The navigation systems which provide the attitude, position and velocity of an object play a key role in many applications. The accuracy of them depends on used sensors. Nowadays, the low-cost MEMS based inertial sensors are used but they are not able toprovide position and velocity as a standalone system and thus they need to be aided by other sources of information. To develop the standalone system, which can provide navigation solution independently, there must be utilized more precise inertial sensors with resolution at least 100 times better than in the case of MEMS. This paper presents the development of inertial navigation system using tactical grade inertial sensors. The proposed system consists of three quartz accelerometers INN-204 with analogue output and three digital fiber optic gyroscopes DSP-3100. The data are preprocessed by means of compensation of deterministic sensors errors, temperature compensation, data decimation and pre-filtering using FIR digital filter. The n

Druh

D - Stať ve sborníku

CEP obor

JU - Aeronautika, aerodynamika, letadla

OECD FORD obor

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Projekt

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Návaznosti

S - Specificky vyzkum na vysokych skolach

Rok uplatnění

2015

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název statě ve sborníku

Proceedings of the 19th International Scientific Student Conferenece POSTER 2015

ISBN

978-80-01-05499-4

ISSN

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e-ISSN

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Počet stran výsledku

5

Strana od-do

1-5

Název nakladatele

Czech Technical University in Prague

Místo vydání

Praha

Místo konání akce

Praha

Datum konání akce

14. 5. 2015

Typ akce podle státní příslušnosti

EUR - Evropská akce

Kód UT WoS článku

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