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  • As is well known, in Low Earth Orbit, besides gravitational force, a number of perturbing factors influence a spacecraft’s trajectory. It is possible to divide these perturbations into two basic groups: gravitational – due to Earth’s non-sphericity, other celestial bodies attraction (The Sun, the Moon) and non-gravitational – due to mainly atmosphere drag and direct/indirect solar radiation pressure. In this paper attention will be paid to method of assessment and measurement on the spacecraft board, especially accelerations rising by virtue of non-gravitational perturbing forces. The development of a special measurement instrument – the microaccelerometer - its block diagram, control concept and its application in space research projects are presented in this paper also. New developed electrostatic accelerometer is considered and analyzed as a smart sensor. The areas of aerospace application and advantages are described.
  • As is well known, in Low Earth Orbit, besides gravitational force, a number of perturbing factors influence a spacecraft’s trajectory. It is possible to divide these perturbations into two basic groups: gravitational – due to Earth’s non-sphericity, other celestial bodies attraction (The Sun, the Moon) and non-gravitational – due to mainly atmosphere drag and direct/indirect solar radiation pressure. In this paper attention will be paid to method of assessment and measurement on the spacecraft board, especially accelerations rising by virtue of non-gravitational perturbing forces. The development of a special measurement instrument – the microaccelerometer - its block diagram, control concept and its application in space research projects are presented in this paper also. New developed electrostatic accelerometer is considered and analyzed as a smart sensor. The areas of aerospace application and advantages are described. (en)
Title
  • Application of the Electrostatic Accelerometer MAC04 in Space Missions
  • Application of the Electrostatic Accelerometer MAC04 in Space Missions (en)
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  • Application of the Electrostatic Accelerometer MAC04 in Space Missions
  • Application of the Electrostatic Accelerometer MAC04 in Space Missions (en)
skos:notation
  • RIV/00010669:_____/10:#0001264!RIV12-MSM-00010669
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • P(1M0501)
http://linked.open...vai/riv/dodaniDat
http://linked.open...aciTvurceVysledku
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  • 247512
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  • RIV/00010669:_____/10:#0001264
http://linked.open...riv/jazykVysledku
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  • orbit perturbations; instrument performances; simulation; space mission (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...ontrolniKodProRIV
  • [3021E05FA8E3]
http://linked.open...v/mistoKonaniAkce
  • Nara, Japonsko
http://linked.open...i/riv/mistoVydani
  • USA
http://linked.open...i/riv/nazevZdroje
  • 18th IFAC Symposium on Automatic Control in Aerospace 2010
http://linked.open...in/vavai/riv/obor
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http://linked.open...vavai/riv/projekt
http://linked.open...UplatneniVysledku
http://linked.open...iv/tvurceVysledku
  • Chvojka, Milan
  • Fedosov, Viktor
http://linked.open...vavai/riv/typAkce
http://linked.open.../riv/zahajeniAkce
issn
  • 1474-6670
number of pages
http://bibframe.org/vocab/doi
  • 10.3182/20100906-5-JP-2022.00088
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  • Elsevier Limited
https://schema.org/isbn
  • 978-1-61839-121-6
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