Manjunath, B and Nandini, - and Sreenivasan, KG and Renuka Devi, M and Krishnan, A (1997) Software Testing Paradigm for Safety13; Critical Software. Technical Report. National Aerospace Laboratories, Bangalore,India.
Full text available as:| PDF Restricted to Archive staff only Download (1082Kb) |
Abstract
environment, time factor interrupt occurances and problems multilane. To make testibility built into the program a ANSI C language standard for software development is adopted. Testing is carried out by 1) designing a test suite in host computer 2) setting up a hardware simulator and by 3) desining a software monitor for testing time factor and interrupt occurances in target board. The design and function of each of these tasks is described in this document.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Software Testing;Real-Time Software;Test Data;Multilane Testing;Adequecy Criteria;White-Box testing;Block-Box Testing; Coverage Table; Multilane Architecture |
| Subjects: | AERONAUTICS > Aircraft Design, Testing & Performance |
| Division/Department: | Aerospace Electronics and Controls Division, Aerospace Electronics and Controls Division, Aerospace Electronics and Controls Division, Aerospace Electronics and Controls Division, Aerospace Electronics and Controls Division |
| Depositing User: | Mr. N A |
| Date Deposited: | 09 May 2006 |
| Last Modified: | 24 May 2010 09:41 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1275 |
Actions (login required)
| View Item |

