Application of the Electrostatic Accelerometer MAC04 in Space Missions

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F10%3A%230001264" target="_blank" >RIV/00010669:_____/10:#0001264 - isvavai.cz</a>

Výsledek na webu

<a href="http://www.ifac-papersonline.net/Detailed/47465.html" target="_blank" >http://www.ifac-papersonline.net/Detailed/47465.html</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.3182/20100906-5-JP-2022.00088" target="_blank" >10.3182/20100906-5-JP-2022.00088</a>

Jazyk výsledku

angličtina

Název v původním jazyce

Application of the Electrostatic Accelerometer MAC04 in Space Missions

Popis výsledku v původním jazyce

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 presentedin this paper also. New developed electrostatic accelerometer is considered and analyzed as a smart sensor. The areas of aerospace application and advantages are described.

Název v anglickém jazyce

Application of the Electrostatic Accelerometer MAC04 in Space Missions

Popis výsledku anglicky

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 presentedin this paper also. New developed electrostatic accelerometer is considered and analyzed as a smart sensor. The areas of aerospace application and advantages are described.

Druh

D - Stať ve sborníku

CEP obor

JV - Kosmické technologie

OECD FORD obor

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Projekt

<a href="/cs/project/1M0501" target="_blank" >1M0501: Centrum leteckého a kosmického výzkumu</a><br>

Návaznosti

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Rok uplatnění

2010

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název statě ve sborníku

18th IFAC Symposium on Automatic Control in Aerospace 2010

ISBN

978-1-61839-121-6

ISSN

1474-6670

e-ISSN

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Počet stran výsledku

6

Strana od-do

515-520

Název nakladatele

Elsevier Limited

Místo vydání

USA

Místo konání akce

Nara, Japonsko

Datum konání akce

6. 9. 2010

Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

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