DocumentCode :
1738578
Title :
Executable formal models for validation and specless verification
Author :
Greve, David ; Wilding, Matthew
Author_Institution :
Rockwell Collins, Cedar Rapids, IA, USA
Volume :
1
fYear :
2000
fDate :
2000
Abstract :
Verification and certification of flight critical software and application-specific integrated circuits (ASICs) is currently a labor-intensive, manual process involving extensive testing, inspections, and process documentation. The complexity of these systems and devices will increase both because increases in cockpit automation and application integration offer important safety benefits and because astonishing improvements in digital computing technology can potentially improve performance and decrease cost. The current approach to verification and certification will be challenged by this increased complexity. In order to reap fully the benefits of these technological advances we must develop new methods for verification and certification of flight critical devices that provide higher degrees of assurance for increasingly complex systems while simultaneously streamlining the verification process. The development of executable formal models may offer higher degrees of assurance, address increased complexity, and streamline certain aspects of the verification process. Increased assurance can be obtained as a result of rigorous, mechanical, mathematically complete checks of consistency and completeness of system requirements as well as proofs of correctness of specific implementations. As vector-based testing becomes increasingly inadequate to assure correctness in the face of exponentially growing state space, formal proofs of correctness can encompass the entire design, demonstrating correctness once and for all
Keywords :
aerospace computing; application specific integrated circuits; avionics; certification; formal verification; safety-critical software; ASICs; application-specific integrated circuits; certification; cockpit automation; complex systems; executable formal models; flight critical devices; flight critical software; specless verification; validation; Application software; Application specific integrated circuits; Automation; Certification; Circuit testing; Documentation; Inspection; Integrated circuit testing; Safety devices; Software testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Digital Avionics Systems Conference, 2000. Proceedings. DASC. The 19th
Conference_Location :
Philadelphia, PA
Print_ISBN :
0-7803-6395-7
Type :
conf
DOI :
10.1109/DASC.2000.886875
Filename :
886875
Link To Document :
بازگشت