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Description
| - 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)
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Title
| - Application of the Electrostatic Accelerometer MAC04 in Space Missions
- Application of the Electrostatic Accelerometer MAC04 in Space Missions (en)
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skos:prefLabel
| - Application of the Electrostatic Accelerometer MAC04 in Space Missions
- Application of the Electrostatic Accelerometer MAC04 in Space Missions (en)
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skos:notation
| - RIV/00010669:_____/10:#0001264!RIV12-MSM-00010669
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http://linked.open...avai/riv/aktivita
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http://linked.open...avai/riv/aktivity
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http://linked.open...vai/riv/dodaniDat
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http://linked.open...aciTvurceVysledku
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http://linked.open.../riv/druhVysledku
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http://linked.open...iv/duvernostUdaju
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http://linked.open...titaPredkladatele
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http://linked.open...dnocenehoVysledku
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http://linked.open...ai/riv/idVysledku
| - RIV/00010669:_____/10:#0001264
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http://linked.open...riv/jazykVysledku
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http://linked.open.../riv/klicovaSlova
| - orbit perturbations; instrument performances; simulation; space mission (en)
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http://linked.open.../riv/klicoveSlovo
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http://linked.open...ontrolniKodProRIV
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http://linked.open...v/mistoKonaniAkce
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http://linked.open...i/riv/mistoVydani
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http://linked.open...i/riv/nazevZdroje
| - 18th IFAC Symposium on Automatic Control in Aerospace 2010
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http://linked.open...in/vavai/riv/obor
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http://linked.open...ichTvurcuVysledku
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http://linked.open...cetTvurcuVysledku
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http://linked.open...vavai/riv/projekt
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http://linked.open...UplatneniVysledku
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http://linked.open...iv/tvurceVysledku
| - Chvojka, Milan
- Fedosov, Viktor
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http://linked.open...vavai/riv/typAkce
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http://linked.open.../riv/zahajeniAkce
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issn
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number of pages
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http://bibframe.org/vocab/doi
| - 10.3182/20100906-5-JP-2022.00088
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http://purl.org/ne...btex#hasPublisher
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https://schema.org/isbn
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is http://linked.open...avai/riv/vysledek
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