Abstract
Firstly, the failure model of Satelliteborne communication software is given for space environment, especially SEU(Single Event Upset), unlike common communication software, then the design flow for satelliteborne software is set , and some measures are taken such as register renewed periodically, memory voting and redundancy design. Finally fault injection is applied to validate. Practical results show that the design is necessary and effective.
This is a preview of subscription content, log in via an institution to check access.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
Duan, X.H., Jianwen, D.Z.: Research on Designing-Methods for Reliability of On-Board Software. Computer Engineering 35, 73–75 (2009)
Liu, H.F.: Fault-tolerance Design and Verification of Satelliteborne Software. Journal of China Academy Electronics and Information Technology 4, 313–316 (2009)
Chunru, Y., Taian, L.: Embedded software reliability estimation based on testing-coverage. Computer Engineering and Design 30, 2198–2200 (2009)
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2011 Springer-Verlag Berlin Heidelberg
About this paper
Cite this paper
Dai, S., Wang, H. (2011). Communication Software Reliability Design of Satelliteborne. In: Zhu, M. (eds) Electrical Engineering and Control. Lecture Notes in Electrical Engineering, vol 98. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-21765-4_32
Download citation
DOI: https://doi.org/10.1007/978-3-642-21765-4_32
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-21764-7
Online ISBN: 978-3-642-21765-4
eBook Packages: EngineeringEngineering (R0)