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

1986-05-02

1988-11-15

Chin, Gary

Boots, shoes, and leggings

371 68, G06F 1520, G06F 1116

Patent

active

047854030

ABSTRACT:
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.

REFERENCES:
patent: 3401904 (1968-09-01), Nelson
patent: 3811273 (1974-05-01), Martin
patent: 4032757 (1977-06-01), Eccles
patent: 4130241 (1978-12-01), Meredith et al.
patent: 4215412 (1980-07-01), Bernier et al.
patent: 4296601 (1981-10-01), Martin
patent: 4504905 (1985-03-01), Burrage
patent: 4594849 (1986-06-01), Kenison et al.
patent: 4622667 (1986-11-01), Yount
patent: 4644538 (1987-02-01), Cooper et al.
patent: 4651563 (1987-03-01), Zweifel

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