Aircraft fault monitoring system and method

Details Aircraft fault monitoring system and method Aircraft fault monitoring system and method

2005-01-18

2005-01-18

Baderman, Scott (Department: 2114)

Error detection/correction and fault detection/recovery

Data processing system error or fault handling

Reliability and availability

C714S047300

Reexamination Certificate

active

06845468

ABSTRACT:
A fault monitoring system comprises a fault detection mechanism to determine the status of a parameter to be monitored. An integrator counts in one direction when a fault in the measurement system is detected and counts in an opposite direction in the absence of fault detection. A threshold detector generates a hard fault indication when the integrator count reaches a threshold value, and an integrator count monitor generates information indicative of the state of the integrator count when below the threshold value thereby providing an indication of the progression of the fault.

REFERENCES:
patent: 6158021 (2000-12-01), Ziegler et al.
patent: 6553518 (2003-04-01), Ware et al.
patent: 6560725 (2003-05-01), Longwell et al.
patent: 04101523 (1992-04-01), None

Affiliated with

Also associated with

Rating

Aircraft fault monitoring system and method does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Aircraft fault monitoring system and method, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Aircraft fault monitoring system and method will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-3415923