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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.
  • 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. (en)
  • Příspěvek pojednává o vývoji senzorů úhlových rychlostí a metodách vyhodnocení náklonu letadla či jiného navigovaného objektu. (cs)
Title
  • New Trends in Angular Rate Sensing and Attitude Evaluation
  • Nové trendy ve vývoji senzorů úhlových rychlostí a metod vyhodnocení náklonu (cs)
  • New Trends in Angular Rate Sensing and Attitude Evaluation (en)
skos:prefLabel
  • New Trends in Angular Rate Sensing and Attitude Evaluation
  • Nové trendy ve vývoji senzorů úhlových rychlostí a metod vyhodnocení náklonu (cs)
  • New Trends in Angular Rate Sensing and Attitude Evaluation (en)
skos:notation
  • RIV/68407700:21230/08:03147163!RIV09-MSM-21230___
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • Z(MSM6840770015)
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  • 382684
http://linked.open...ai/riv/idVysledku
  • RIV/68407700:21230/08:03147163
http://linked.open...riv/jazykVysledku
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  • Kalman filtering; attitude; low-cost sensors; navigation (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...ontrolniKodProRIV
  • [6AEEFF382443]
http://linked.open...v/mistoKonaniAkce
  • Praha
http://linked.open...i/riv/mistoVydani
  • Praha
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  • Nové trendy v civilním letectví
http://linked.open...in/vavai/riv/obor
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http://linked.open...UplatneniVysledku
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  • Roháč, Jan
  • Reinštein, Michal
http://linked.open...vavai/riv/typAkce
http://linked.open.../riv/zahajeniAkce
http://linked.open...n/vavai/riv/zamer
number of pages
http://purl.org/ne...btex#hasPublisher
  • České vysoké učení technické v Praze. Fakulta dopravní
https://schema.org/isbn
  • 978-80-7204-604-1
http://localhost/t...ganizacniJednotka
  • 21230
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