Use of the high sensitive electrostatic accelerometer for orbit perturbation effects investigation on board of LEO spacecraft

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F10%3A%230001102" target="_blank" >RIV/00010669:_____/10:#0001102 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Result language
angličtina
Original language name
Use of the high sensitive electrostatic accelerometer for orbit perturbation effects investigation on board of LEO spacecraft
Original language description
The gravitational force a number of perturbing factors influence a spacecraft?s trajectory on the low Earth orbit (LEO). As an instrument usable for perturbative accelerations measurement is investigated the high sensitive triaxial electrostatic accelerometer MAC04 developed recently in the Czech Republic. The main stages of development of this device, description of the measurement principle, instrument performances, control concept and application of the accelerometer in recent space research projectsare presented in the paper. The emphasis will be placed on aspects of accelerometer orbit operation, in-flight calibration problem and flight verification of accelerometer performances.
Czech name
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Czech description
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Project
<a href="/en/project/1M0501" target="_blank" >1M0501: Aerospace Research Centre</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2010
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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