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  • Precise attitude and position determination is one of main tasks in navigation procedure. Nowadays, there is possibility to navigate military Unmanned Aerial System (UAS) accurately also in case of its flight on other side of the Earth. But such precise navigation system based on inertial sensors (angular rate sensors and accelerometers) is not only expensive, but also large-sized and it has high power consumption for proper functionality. Costs, power consumption and size together with area restriction limit usage of such system especially in military application. This paper describes such a modular system based on low-cost inertial sensors with aiding sensors (distance sensors, pressure sensors, and tilt sensors). Described modular system finds its utilization not only as navigation system of small UAS, but also as part of intelligent metal detector equipped as added discrimination ability or in robot and indoor navigation.
  • Precise attitude and position determination is one of main tasks in navigation procedure. Nowadays, there is possibility to navigate military Unmanned Aerial System (UAS) accurately also in case of its flight on other side of the Earth. But such precise navigation system based on inertial sensors (angular rate sensors and accelerometers) is not only expensive, but also large-sized and it has high power consumption for proper functionality. Costs, power consumption and size together with area restriction limit usage of such system especially in military application. This paper describes such a modular system based on low-cost inertial sensors with aiding sensors (distance sensors, pressure sensors, and tilt sensors). Described modular system finds its utilization not only as navigation system of small UAS, but also as part of intelligent metal detector equipped as added discrimination ability or in robot and indoor navigation. (en)
Title
  • Modular System for Attitude and Position Determination
  • Modular System for Attitude and Position Determination (en)
skos:prefLabel
  • Modular System for Attitude and Position Determination
  • Modular System for Attitude and Position Determination (en)
skos:notation
  • RIV/68407700:21230/11:00180451!RIV12-MSM-21230___
http://linked.open...avai/predkladatel
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • P(GD102/09/H082), S, Z(MSM6840770015)
http://linked.open...vai/riv/dodaniDat
http://linked.open...aciTvurceVysledku
http://linked.open.../riv/druhVysledku
http://linked.open...iv/duvernostUdaju
http://linked.open...titaPredkladatele
http://linked.open...dnocenehoVysledku
  • 213404
http://linked.open...ai/riv/idVysledku
  • RIV/68407700:21230/11:00180451
http://linked.open...riv/jazykVysledku
http://linked.open.../riv/klicovaSlova
  • Modular system; Inertial navigation; UAS; metal detection; mine detection; attitude; GPS; CAN aerospace; air data computer; center of image gravity algorithm (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...ontrolniKodProRIV
  • [5EDB62226878]
http://linked.open...v/mistoKonaniAkce
  • Prague
http://linked.open...i/riv/mistoVydani
  • Praha
http://linked.open...i/riv/nazevZdroje
  • POSTER 2011 - 15th International Student Conference on Electrical Engineering
http://linked.open...in/vavai/riv/obor
http://linked.open...ichTvurcuVysledku
http://linked.open...cetTvurcuVysledku
http://linked.open...vavai/riv/projekt
http://linked.open...UplatneniVysledku
http://linked.open...iv/tvurceVysledku
  • Nováček, Petr
  • Šipoš, Martin
  • Pačes, Pavel
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 elektrotechnická
https://schema.org/isbn
  • 978-80-01-04806-1
http://localhost/t...ganizacniJednotka
  • 21230
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