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Statements

Subject Item
n2:RIV%2F00010669%3A_____%2F10%3A%230001264%21RIV12-MSM-00010669
rdf:type
n19:Vysledek skos:Concept
rdfs:seeAlso
http://www.ifac-papersonline.net/Detailed/47465.html
dcterms: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.
dcterms:title
Application of the Electrostatic Accelerometer MAC04 in Space Missions Application of the Electrostatic Accelerometer MAC04 in Space Missions
skos:prefLabel
Application of the Electrostatic Accelerometer MAC04 in Space Missions Application of the Electrostatic Accelerometer MAC04 in Space Missions
skos:notation
RIV/00010669:_____/10:#0001264!RIV12-MSM-00010669
n3:aktivita
n11:P
n3:aktivity
P(1M0501)
n3:dodaniDat
n10:2012
n3:domaciTvurceVysledku
n18:3147576 n18:5833566
n3:druhVysledku
n16:D
n3:duvernostUdaju
n4:S
n3:entitaPredkladatele
n21:predkladatel
n3:idSjednocenehoVysledku
247512
n3:idVysledku
RIV/00010669:_____/10:#0001264
n3:jazykVysledku
n15:eng
n3:klicovaSlova
orbit perturbations; instrument performances; simulation; space mission
n3:klicoveSlovo
n5:simulation n5:orbit%20perturbations n5:space%20mission n5:instrument%20performances
n3:kontrolniKodProRIV
[3021E05FA8E3]
n3:mistoKonaniAkce
Nara, Japonsko
n3:mistoVydani
USA
n3:nazevZdroje
18th IFAC Symposium on Automatic Control in Aerospace 2010
n3:obor
n13:JV
n3:pocetDomacichTvurcuVysledku
2
n3:pocetTvurcuVysledku
2
n3:projekt
n8:1M0501
n3:rokUplatneniVysledku
n10:2010
n3:tvurceVysledku
Fedosov, Viktor Chvojka, Milan
n3:typAkce
n17:WRD
n3:zahajeniAkce
2010-09-06+02:00
s:issn
1474-6670
s:numberOfPages
6
n12:doi
10.3182/20100906-5-JP-2022.00088
n7:hasPublisher
Elsevier Limited
n20:isbn
978-1-61839-121-6