Control system software execution during fault detection

An example method for uninterrupted execution of control software in an aircraft control system includes creating a plurality of static data copies. A first parity bit is determined for each of the plurality of static data copies. A second parity bit is determined for a first static data copy. A par...

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Hauptverfasser:	THANGAVELU, KAMARAJ, SCHMIDT, JEFFERY S
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	CALCULATING COMPUTING CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING COUNTING ELECTRIC DIGITAL DATA PROCESSING FUNCTIONAL ELEMENTS OF SUCH SYSTEMS MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PHYSICS REGULATING
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Zusammenfassung:	An example method for uninterrupted execution of control software in an aircraft control system includes creating a plurality of static data copies. A first parity bit is determined for each of the plurality of static data copies. A second parity bit is determined for a first static data copy. A parity fault is detected in the first static data copy if the first parity bit does not match the second parity bit. The system switches to read a second static data copy in response to detecting a parity fault in the first static data copy.