Distributed flight condition data validation system and method

Details Distributed flight condition data validation system and method Distributed flight condition data validation system and method

F - Mech Eng,Light,Heat,Weapons

02

C

354/18

F02C 9/28 (2006.01)

Patent

CA 1258126

ABSTRACT DISTRIBUTED FLIGHT CONDITION DATA VALIDATION SYSTEM AND METHOD A distributed data acquisition system for a first engine controller determines a final, validated value of a critical flight condition variable by first determining: a first tentative value based on local environmental conditions, a second tentative value based on the performance of a first engine, and a third tentative value transferred directly from a similar data acquisition system linked to a second engine on the same aircraft. The data acquisition system compares the three tentative values and selects a final, validated value for use by the controller.

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