Proceedings of 5th International Conference on Recent Advances in Space Technologies - RAST2011 2011
DOI: 10.1109/rast.2011.5966889
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A cost-effective Software Development and Validation environment and approach for LEON based satellite & payload subsystems

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Cited by 6 publications
(5 citation statements)
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“…Space industry heavily relies on this tool to develop software in a faster way and to provide WCET analysis. For instance, the use of a cycle-accurate model of LEON (TSIM) is key to provide a lightweight, scalable, and cost-efficient solution for integration and validation of satellite subsystems and payload equipment containing embedded software [88]. The vendor reports TSIM to reach 60 MIPS on a Intel i7-2600K @3.4GHz PC, which is close to the MIPS reported for the OBC in third column of Table 2 (−13%).…”
Section: Simulation Modelsmentioning
confidence: 51%
“…Space industry heavily relies on this tool to develop software in a faster way and to provide WCET analysis. For instance, the use of a cycle-accurate model of LEON (TSIM) is key to provide a lightweight, scalable, and cost-efficient solution for integration and validation of satellite subsystems and payload equipment containing embedded software [88]. The vendor reports TSIM to reach 60 MIPS on a Intel i7-2600K @3.4GHz PC, which is close to the MIPS reported for the OBC in third column of Table 2 (−13%).…”
Section: Simulation Modelsmentioning
confidence: 51%
“…In order to use the SMP standard for a distributed simulation, a central network node is needed that transfers the packets based on the configuration to the corresponding subsystem. In other words, the simulation services will be sent to the switching node, which then takes care of the forwarding [12]. In addition, the switching node has to be changed if the model hierarchy or model links are to be changed.…”
Section: Related Workmentioning
confidence: 99%
“…In previous work applying model based verification and validation for software configuration Cordero et al [15] built a software development environment that uses to support the development and verification of on-board software for spacecraft. Tanizaki et al [16] use a SAT solver approach to model and check the consistency of configuration files and discover syntactic and semantic errors.…”
Section: Related Workmentioning
confidence: 99%