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An Entity of Type : http://linked.opendata.cz/ontology/domain/vavai/Vysledek, within Data Space : linked.opendata.cz associated with source document(s)

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Description
  • The article is focused on the Czech high sensitive electrostatic accelerometer MAC04TS on board of the Russian small satellite. The paper provides analysis of the instrument performances. As the first part the accelerometer system is analyzed. The behavior of the test mass and its capacitive feedback system is simulated in the time and the frequency domain for one degree of freedom in linear channel. The second part of the analysis presents the simulation results of the accelerometer measurements on board of the satellite during orbit flight. For the simulation of the non-gravitational forces in relation to orbit and spacecraft parameters were used non-conservative perturbations models developed by Astronomical institutes of Czech Academy of Sciences. Details of the simulation and discussion on its results are presented.
  • The article is focused on the Czech high sensitive electrostatic accelerometer MAC04TS on board of the Russian small satellite. The paper provides analysis of the instrument performances. As the first part the accelerometer system is analyzed. The behavior of the test mass and its capacitive feedback system is simulated in the time and the frequency domain for one degree of freedom in linear channel. The second part of the analysis presents the simulation results of the accelerometer measurements on board of the satellite during orbit flight. For the simulation of the non-gravitational forces in relation to orbit and spacecraft parameters were used non-conservative perturbations models developed by Astronomical institutes of Czech Academy of Sciences. Details of the simulation and discussion on its results are presented. (en)
Title
  • Sensor Analysis for Teaser Project
  • Sensor Analysis for Teaser Project (en)
skos:prefLabel
  • Sensor Analysis for Teaser Project
  • Sensor Analysis for Teaser Project (en)
skos:notation
  • RIV/00010669:_____/09:#0000987!RIV10-MPO-00010669
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • P(FT-TA2/033)
http://linked.open...iv/cisloPeriodika
  • 2
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
  • 340810
http://linked.open...ai/riv/idVysledku
  • RIV/00010669:_____/09:#0000987
http://linked.open...riv/jazykVysledku
http://linked.open.../riv/klicovaSlova
  • non-gravitational perturbations; accelerometer; simulation (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...odStatuVydavatele
  • CZ - Česká republika
http://linked.open...ontrolniKodProRIV
  • [5E49065E4CCD]
http://linked.open...i/riv/nazevZdroje
  • Czech Aerospace Proceedings / Letecký zpravodaj
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...v/svazekPeriodika
  • 2009
http://linked.open...iv/tvurceVysledku
  • Fedossov, Viktor
issn
  • 1211-877X
number of pages
is http://linked.open...avai/riv/vysledek of
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