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Statements

Subject Item
n2:RIV%2F68407700%3A21230%2F08%3A03147163%21RIV09-MSM-21230___
rdf:type
n6:Vysledek skos:Concept
dcterms:description
Angular rate sensing is one of basic functions of Inertial Measurement Units (IMU) that are used in Inertial Navigation Systems (INS). These systems can be generally used in any king of transportation where navigation functions are needed, even in aeronautical field. These systems, sensors included, have recorded significant progress since the beginning of 20th century when the first gyrocompass was patented by Dr. Anschutz (1904). Since that time the technology has changed a lot and systems performance has begun to be much more precise and reliable. Thus this paper deals with a description of new kind of angular rate sensors and gyroscopes and their usage in aircraft attitude evaluation. Measured performance of some angular rate sensors will be presented. Příspěvek pojednává o vývoji senzorů úhlových rychlostí a metodách vyhodnocení náklonu letadla či jiného navigovaného objektu. Angular rate sensing is one of basic functions of Inertial Measurement Units (IMU) that are used in Inertial Navigation Systems (INS). These systems can be generally used in any king of transportation where navigation functions are needed, even in aeronautical field. These systems, sensors included, have recorded significant progress since the beginning of 20th century when the first gyrocompass was patented by Dr. Anschutz (1904). Since that time the technology has changed a lot and systems performance has begun to be much more precise and reliable. Thus this paper deals with a description of new kind of angular rate sensors and gyroscopes and their usage in aircraft attitude evaluation. Measured performance of some angular rate sensors will be presented.
dcterms:title
New Trends in Angular Rate Sensing and Attitude Evaluation New Trends in Angular Rate Sensing and Attitude Evaluation Nové trendy ve vývoji senzorů úhlových rychlostí a metod vyhodnocení náklonu
skos:prefLabel
New Trends in Angular Rate Sensing and Attitude Evaluation New Trends in Angular Rate Sensing and Attitude Evaluation Nové trendy ve vývoji senzorů úhlových rychlostí a metod vyhodnocení náklonu
skos:notation
RIV/68407700:21230/08:03147163!RIV09-MSM-21230___
n3:aktivita
n7:Z
n3:aktivity
Z(MSM6840770015)
n3:dodaniDat
n8:2009
n3:domaciTvurceVysledku
n15:8140634 n15:6234968
n3:druhVysledku
n17:D
n3:duvernostUdaju
n11:S
n3:entitaPredkladatele
n9:predkladatel
n3:idSjednocenehoVysledku
382684
n3:idVysledku
RIV/68407700:21230/08:03147163
n3:jazykVysledku
n16:eng
n3:klicovaSlova
Kalman filtering; attitude; low-cost sensors; navigation
n3:klicoveSlovo
n4:low-cost%20sensors n4:navigation n4:attitude n4:Kalman%20filtering
n3:kontrolniKodProRIV
[6AEEFF382443]
n3:mistoKonaniAkce
Praha
n3:mistoVydani
Praha
n3:nazevZdroje
Nové trendy v civilním letectví
n3:obor
n14:JU
n3:pocetDomacichTvurcuVysledku
2
n3:pocetTvurcuVysledku
2
n3:rokUplatneniVysledku
n8:2008
n3:tvurceVysledku
Reinštein, Michal Roháč, Jan
n3:typAkce
n13:EUR
n3:zahajeniAkce
2008-09-25+02:00
n3:zamer
n19:MSM6840770015
s:numberOfPages
7
n12:hasPublisher
České vysoké učení technické v Praze. Fakulta dopravní
n21:isbn
978-80-7204-604-1
n18:organizacniJednotka
21230