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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 Reference Field 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.
- 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 Reference Field 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. (en)
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Title
| - Space-Friendly Attitude Determination and Control Subsystem for CubeSat-class Mission
- Space-Friendly Attitude Determination and Control Subsystem for CubeSat-class Mission (en)
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skos:prefLabel
| - Space-Friendly Attitude Determination and Control Subsystem for CubeSat-class Mission
- Space-Friendly Attitude Determination and Control Subsystem for CubeSat-class Mission (en)
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skos:notation
| - RIV/68407700:21230/13:00205442!RIV15-MSM-21230___
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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/68407700:21230/13:00205442
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http://linked.open...riv/jazykVysledku
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http://linked.open.../riv/klicovaSlova
| - ADCS; CubeSat; Space (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
| - ICMT'13 - Proceedings of the International Conference on Military Technologies
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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...UplatneniVysledku
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http://linked.open...iv/tvurceVysledku
| - Papaj, Jan
- Laifr, Jaroslav
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http://linked.open...vavai/riv/typAkce
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http://linked.open.../riv/zahajeniAkce
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number of pages
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http://purl.org/ne...btex#hasPublisher
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https://schema.org/isbn
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http://localhost/t...ganizacniJednotka
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