Sensors and Data Processing Methods Used in Navigation Systems

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F11%3A00182794" target="_blank" >RIV/68407700:21230/11:00182794 - isvavai.cz</a>

Výsledek na webu

<a href="http://www.mosatt.org/en/" target="_blank" >http://www.mosatt.org/en/</a>

DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

Sensors and Data Processing Methods Used in Navigation Systems

Popis výsledku v původním jazyce

Navigation systems of civil aircrafts are used for vertical and horizontal situation estimation and indication. They provide information about position, velocity, and orientation of the aircraft in a reference framework. They commonly consist of InertialMeasurement Unit (IMU) and computation units. The IMU primary uses inertial sensors, such as accelerometers and angular rate sensors/gyros, which are sometimes supplemented by magnetometers. The vertical situation can be described by altitude and two Euler angles corresponding to roll and pitch. The third angle (yaw) defines the heading and with position it forms the information about the horizontal situation. The navigation systems can be divided into two groups such as Attitude and Heading ReferenceSystems (AHRS) and Inertial Navigation Systems (INSs). The accuracy of estimated Euler angles also affects the precision of estimated position gotten through two consecutive integrations of acceleration and velocity.

Název v anglickém jazyce

Sensors and Data Processing Methods Used in Navigation Systems

Popis výsledku anglicky

Navigation systems of civil aircrafts are used for vertical and horizontal situation estimation and indication. They provide information about position, velocity, and orientation of the aircraft in a reference framework. They commonly consist of InertialMeasurement Unit (IMU) and computation units. The IMU primary uses inertial sensors, such as accelerometers and angular rate sensors/gyros, which are sometimes supplemented by magnetometers. The vertical situation can be described by altitude and two Euler angles corresponding to roll and pitch. The third angle (yaw) defines the heading and with position it forms the information about the horizontal situation. The navigation systems can be divided into two groups such as Attitude and Heading ReferenceSystems (AHRS) and Inertial Navigation Systems (INSs). The accuracy of estimated Euler angles also affects the precision of estimated position gotten through two consecutive integrations of acceleration and velocity.

Druh

D - Stať ve sborníku

CEP obor

JU - Aeronautika, aerodynamika, letadla

OECD FORD obor

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Projekt

<a href="/cs/project/GD102%2F09%2FH082" target="_blank" >GD102/09/H082: Senzory a inteligentní senzorové systémy</a><br>

Návaznosti

Z - Vyzkumny zamer (s odkazem do CEZ)<br>S - Specificky vyzkum na vysokych skolach

Rok uplatnění

2011

Kód důvěrnosti údajů

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

Název statě ve sborníku

Proceedings of the International Scientific Conference Modern Safety Technologies in Transportation

ISBN

978-80-970772-0-4

ISSN

1338-5232

e-ISSN

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Počet stran výsledku

7

Strana od-do

342-348

Název nakladatele

SUPREMA Ltd.

Místo vydání

Košice

Místo konání akce

Zlatá Idka

Datum konání akce

20. 9. 2011

Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

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