Methods and systems for health monitoring for aircraft
First Claim
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1. A method for health monitoring for an aircraft, the method comprising the steps of:
- obtaining vibration data for the aircraft via a health monitoring system;
obtaining navigation data for the aircraft via a navigation system;
fusing the vibration data and the navigation data, thereby generating fused data; and
determining a measure of health of the aircraft using the fused data via a processor.
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Abstract
A method for health monitoring for an aircraft includes the steps of obtaining vibration data for the aircraft, obtaining navigation data for the aircraft, and determining a measure of health of the aircraft using the vibration data and the navigation data.
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Citations
16 Claims
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1. A method for health monitoring for an aircraft, the method comprising the steps of:
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obtaining vibration data for the aircraft via a health monitoring system; obtaining navigation data for the aircraft via a navigation system; fusing the vibration data and the navigation data, thereby generating fused data; and determining a measure of health of the aircraft using the fused data via a processor. - View Dependent Claims (2, 3, 4, 5, 10)
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6. The method of step 1, further comprising the steps of:
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generating a vibration signature of the aircraft; and generating a plurality of flight regime characteristics of the aircraft; wherein the step of fusing the vibration data and the navigation data comprises the step of fusing the vibration signature and the flight regime characteristics of the aircraft, to thereby generate the fused data. - View Dependent Claims (7, 8, 9)
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11. A system for health monitoring for an aircraft, the system comprising:
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a health monitoring system configured to at least facilitate measuring vibration data for the aircraft during flight of the aircraft; a navigation system configured to at least facilitate measuring navigation data for the aircraft during flight of the aircraft; and a processor coupled to the health monitoring system and the navigation system, the processor configured to at least facilitate; fusing the vibration data and the navigation data, thereby generating fused data; and determining a measure of health of the aircraft using the fused data. - View Dependent Claims (12, 13, 14, 15, 16)
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Specification