Microprocessor electronics in space instrument making

Alferyev, I.S.; Mochalov, A.V.; Fedyuk, R.S.; Danilenko, V.V; Mironov, K.K.

Please use this identifier to cite or link to this item: http://essuir.sumdu.edu.ua/handle/123456789/39902

Or use following links to share this resource in social networks: Recommend this item

Title	Microprocessor electronics in space instrument making
Authors	Alferyev, I.S. Mochalov, A.V. Fedyuk, R.S. Danilenko, V.V Mironov, K.K.
ORCID
Keywords	мікропроцесорна електроніка микропроцессорная электроника microprocessor electronics
Type	Conference Papers
Date of Issue	2014
URI	http://essuir.sumdu.edu.ua/handle/123456789/39902
Publisher	Sumy State University
License
Citation	Microprocessor electronics in space instrument making [Текст] / I.S. Alferyev, A.V. Mochalov, R.S. Fedyuk et al. // Фізика, електроніка, електротехніка : матеріали та програма науково-технічної конференції, м. Суми, 21-26 квітня 2014 р. / Відп. за вип. С.І. Проценко. - Суми : СумДУ, 2014. - С. 165.
Abstract	Volumes of information processed on board the spacecraft (SC) is constantly growing, the algorithms of the onboard systems - complicated. Therefore, a need for new solutions in the field of system architecture SC. Operating conditions are very complex spacecraft: overload when starting, temperature, radiation, and other negative factors of outer space , as well as the inability to repair a running companion , require onboard equipment reliability and survivability. Architecture used today onboard control systems and data do not satisfy in full all these requirements. Need a new concept of architecture - board information and control systems of spacecraft, which provides high functionality and reliability of such systems. Volumes of information processed on board the spacecraft (SC) is constantly growing, the algorithms of the onboard systems - complicated. Therefore, a need for new solutions in the field of system architecture SC. Operating conditions are very complex spacecraft: overload when starting, temperature, radiation, and other negative factors of outer space , as well as the inability to repair a running companion , require onboard equipment reliability and survivability. Architecture used today onboard control systems and data do not satisfy in full all these requirements. Need a new concept of architecture - board information and control systems of spacecraft, which provides high functionality and reliability of such systems.
Appears in Collections:	Наукові видання (ЕлІТ)