Organisation: |
National Aerospace Laboratory and CWI (THE NETHERLANDS)
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Method: |
muCRL (micro Common Representation Language)
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Tools used: |
B-Toolkit
muCRL toolset CADP (Construction and Analysis of Distributed Processes) |
Domain: |
Embedded Systems.
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Period: |
2002
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Size: |
approximately 250,000 states and 900,000 transitions
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Description: |
AIDA (Automatic In-flight Data Acquisition) is a multi-channel
on-board data acquisition system developed by the Royal Netherlands
Navy in order to facilitate the maintenance and increase the safety of
its Lynx helicopters. The AIDA system records usage and loads data on
main rotor, engines, and airframe. It gathers input data from 15 analog
and 2 discrete signals produced by several measurement and control
devices.
The system runs 39 different tasks responsible for data storage, conditioning and processing, and performs several logging tasks simultaneously (e.g., writing data acquisition files, producing audio and video signals, etc.). There are four different groups of tasks:
To perform refinement, an abstract B model of the AIDA system was developed starting from the AIDA functional requirements, and was validated using the B-Toolkit by animation and proof of internal consistency obligations. Several selected components of the system were further refined and proved to be correct w.r.t. the abstract model. At the end, executable specifications (implementations) were obtained and tested against a general environment which produces chaotic combinations of input signals. To verify progress properties, different components of the AIDA system (tasks, sensors, buttons, data acquisition file, output channels, and environment) were specified in muCRL. This allowed to detect and correct several specification errors. The state space of the muCRL description was generated using the muCRL toolset and checked to be deadlock free (using the muCRL toolset) and livelock free (using the CADP toolset). For each task, two correctness requirements were formulated in regular alternation-free mu-calculus and verified using the EVALUATOR 3.0 model-checker of CADP. This allowed to detect and correct a spurious logging error due to an ambiguity in the informal requirements of the AIDA system. |
Conclusions: |
This case-study demonstrated that the combination of refinement methods
(such as the B method and B-Toolkit) and verification methods (such as
muCRL and the CADP toolbox) can be successfully applied in the
development of naval equipment. Also, the joint use of the muCRL and
CADP toolsets turns out to be very effective for a completely automated
verification of functional properties.
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Publications: |
[Fokkink-Ioustinova-Kesseler-vdPol-Usenko-Yushtein-02]
Wan Fokkink, Natalia Ioustinova, Ernst Kesseler, Jaco van de Pol,
Yaroslav S. Usenko, and Yuri A. Yushtein. "Refinement and Verification
Applied to an In-Flight Data Acquisition Unit". Proceedings of the
13th Conference on Concurrency Theory CONCUR'2002 (Brno, Czech
Republic), Lecture Notes in Computer Science vol. 2421, pp. 1-23,
August 2002.
Available on-line at: http://www.cwi.nl/~wan/WJFmore/ktvfm.ps.gz or from the CADP Web site in PDF or PostScript |
Contact: | Dr. Wan Fokkink CWI / Department of Software Engineering SEN2 (Specification and Analysis of Embedded Systems) Kruislaan 413, 1098 SJ Amsterdam, The Netherlands Room: M342 Tel: +31 20 592 4104 Fax: +31 20 592 4199 E-mail: [email protected] |
Further remarks: | This case study, amongst others, is described on the CADP Web site: http://cadp.inria.fr/case-studies |