Technical Paper
An ESL Methodology for Rapid Creation of Embedded Aerospace Systems using Hardware-Software Co-Design on Virtual Platforms
2012-10-22
2012-01-2133
This paper presents an Electronic System-Level (ESL) methodology and framework for the system specification, design space exploration, performance analysis, and hardware/software implementation of aerospace electronic systems subject to Quality of Results (QoR) constraints such as execution time, communication rate, technology, as well as Size, Weight and Power (SWaP). In particular, we show how SWaP constraints could be converted into bounds on the target hardware platform, how several potential architectures could be devised for the system, how each potential architecture and mapping could be evaluated for performance, hardware resource usage and power taking into account the impact of Triple Modular Redundancy (TMR), and how a selected architecture could be exported as a hardware/software Register-Transfer Level (RTL) implementation.
