Virtual integrated software testbed for avionics

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364578, 36442406, G05B 1702

Patent

active

055418635

ABSTRACT:
A virtual integrated software testbed for avionics is disclosed which allows avionics software to be developed on a host computer using a collection of computer programs running simultaneously as processes and synchronized by a central process. The software testbed disclosed uses separate synchronized processes, permits signals from an avionics device to be generated by a simulation running on the host computer or from actual equipment and data bus signals coming from and going to actual avionics hardware is connected to their virtual bus counterparts in the host computer on a real-time basis.

REFERENCES:
patent: 5111402 (1992-05-01), Brooks et al.
patent: 5161158 (1992-11-01), Chakravarty et al.
patent: 5184312 (1993-02-01), Ellis
patent: 5260874 (1993-11-01), Berner et al.
Finley et al., Real time Avionics Processor Emulators, 1993, pp. 129-136.

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