System and method for maintaining system integrity in control systems having multi-lane computational differences

A control system for an aircraft including first and second lanes having respective first and second processors dissimilar to one another and configured to output respective first and second computation data. At least one programmable logic device may be configured to receive the first computation d...

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Bibliographische Detailangaben

Hauptverfasser:	Singer Mark Clifford, Kovalan Mark A, Johnson Douglas R
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING COSMONAUTICS FUNCTIONAL ELEMENTS OF SUCH SYSTEMS HELICOPTERS MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PERFORMING OPERATIONS PHYSICS REGULATING TRANSPORTING
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