Resumen
Theoretical tools are presented to analyze the relationship between the design choices for a class of NASA-inspired fault-tolerant, reconfigurable computer architectures and the tracking performance degradation of a digital flight control system implemented on such a platform while operating in a high-intensity radiated field (HIRF) environment. A HIRF experiment was conducted at the NASA Langley Research Center to validate the theory for a distributed Boeing 747 flight control system subject to HIRF upsets.
| Idioma original | Inglés |
|---|---|
| Número de artículo | 6404118 |
| Páginas (desde-hasta) | 521-542 |
| Número de páginas | 22 |
| Publicación | IEEE Transactions on Aerospace and Electronic Systems |
| Volumen | 49 |
| N.º | 1 |
| DOI | |
| Estado | Publicada - 2013 |