Validation tests of attitude determination software for nanosatellite embedded systems-Reference-Cited by-同舟云学术

Validation tests of attitude determination software for nanosatellite embedded systems

Published:2018-02 Issue: Volume:116 Page:391-401
ISSN:0263-2241
Container-title:Measurement
language:en
Short-container-title:Measurement

Author:

Garcia Camila B.A.,Vale Samuel R.C.,Martins-Filho Luiz S.,Duarte Ricardo O.,Kuga Helio K.,Carrara Valdemir

Funder

Brazilian Space Agency

Federal University of ABC

Federal University of Minas Gerais

Publisher

Elsevier BV

Subject

Applied Mathematics,Electrical and Electronic Engineering,Condensed Matter Physics,Instrumentation

Reference20 articles.

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2. Single event effects in avionics;Normand;IEEE Trans. Nucl. Sci.,1996

3. R.O. Duarte, L.S. Martins-Filho, G.F.T. Knop, R.S. Prado, A fault-tolerant attitude determination system based on COTS devices, in: 11th IEEE International On-Line Testing Symposium, 2008, Rhodes, Greece, 2008, pp. 85–90. doi:10.1109/IOLTS.2008.20.

4. R.O. Duarte, F.E. Torres, T.H. Gomes, L.S. Martins-Filho, H.K. Kuga, An attitude determination system implementation to low orbit small satellites with fault-tolerant techniques, in: Proc. of 8th IAA Symposium on Small Satellites for Earth Observation, Berlin, Germany, 2011, pp. 453–459.

5. P. Schlyter, How to Compute Planetary Positions, 2016. (Accessed 29.11.16).

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