Space-Friendly Attitude Determination and Control Subsystem for CubeSat-class Mission

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21230%2F13%3A00205442" target="_blank" >RIV/68407700:21230/13:00205442 - 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
Space-Friendly Attitude Determination and Control Subsystem for CubeSat-class Mission
Original language description
In this paper we propose the electrical design approaches to build a radiationtolerant Attitude Determination and Control Subsystem and subsystem providing the telemetry status of the ADCS to the On-board Computer. The 2-Unit CubeSat-class satellite project 'CzechTechSat' which is being built for one year at the CTU FEE implements this subsystem to prove the radiation mitigation concepts. Fully mature and light-weight ADCS board implements powerful Kalman filter with International Geomagnetic ReferenceField v11. PC/104 format subsystem is equipped with six inputs for analogue Sun Sensors, three outputs for Magnetorquers with dedicated current measurements, one output for one axis Reaction Wheel with current and RPM control, three space-tolerant and 5000 g shock resistant 100 °/s Angular Rate sensors, AMR magnetometer and thermometer. Each peripheral is monitored by housekeeping measurement and ready to work in power saving mode.
Czech name
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Czech description
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Publication year
2013
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
ICMT'13 - Proceedings of the International Conference on Military Technologies
ISBN
978-80-7231-917-6
ISSN
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e-ISSN
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Number of pages
6
Pages from-to
873-878
Publisher name
Univerzita obrany
Place of publication
Brno
Event location
Brno
Event date
May 22, 2013
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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