Abstract
A software-safety analysis approach for distributed systems, based on a technique called component-message fault analysis, is presented. This technique checks the safety-critical logic, using the safety specification for different categories of component fault events, to uncover ambiguous safety requirements or design deficiencies. To demonstrate the power of this technique, a dual-purpose missile system is introduced and analyzed with regard to its software-safety requirements.
| Original language | English |
|---|---|
| Pages | 29-43 |
| Number of pages | 15 |
| State | Published - 1988 |