Methods and systems for health monitoring for aircraft
First Claim
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1. A method for initiating health monitoring for an aircraft by a ground station, the ground station including a ground station computer system and a set-up tool, the set-up tool comprising a computer module executed by the ground station computer system, the method comprising the steps of:
- receiving user input at the computer system of the ground station from an onboard computer system of the aircraft, the user input including aircraft-specific geometric information regarding a plurality of details as to a make-up of the aircraft;
downloading the aircraft-specific geometric information to a database in a memory of the computer system on the ground station; and
configuring the ground station computer system using the aircraft specific geometric information via the set-up tool using a processor;
wherein the ground station computer system is generic to various different aircraft, and is configured for specific use in connection with a specific aircraft based on the aircraft-specific geometric information from the aircraft, corresponding to the aircraft based on the aircraft-specific geometric information from the aircraft, and specifically configured for use in connection with an onboard computer system residing onboard the aircraft, via the set-up tool based on the aircraft-specific geometric information; and
wherein the step of configuring the ground station comprises utilizing the aircraft-specific geometric information to select a plurality of algorithms for a program of the ground station that are tailored specifically for the aircraft based on the aircraft-specific geometric information, and utilizing the aircraft-specific geometric information to select a plurality of parameters for the selected algorithms based on the aircraft-specific geometric information.
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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.
53 Citations
20 Claims
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1. A method for initiating health monitoring for an aircraft by a ground station, the ground station including a ground station computer system and a set-up tool, the set-up tool comprising a computer module executed by the ground station computer system, the method comprising the steps of:
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receiving user input at the computer system of the ground station from an onboard computer system of the aircraft, the user input including aircraft-specific geometric information regarding a plurality of details as to a make-up of the aircraft; downloading the aircraft-specific geometric information to a database in a memory of the computer system on the ground station; and configuring the ground station computer system using the aircraft specific geometric information via the set-up tool using a processor; wherein the ground station computer system is generic to various different aircraft, and is configured for specific use in connection with a specific aircraft based on the aircraft-specific geometric information from the aircraft, corresponding to the aircraft based on the aircraft-specific geometric information from the aircraft, and specifically configured for use in connection with an onboard computer system residing onboard the aircraft, via the set-up tool based on the aircraft-specific geometric information; and wherein the step of configuring the ground station comprises utilizing the aircraft-specific geometric information to select a plurality of algorithms for a program of the ground station that are tailored specifically for the aircraft based on the aircraft-specific geometric information, and utilizing the aircraft-specific geometric information to select a plurality of parameters for the selected algorithms based on the aircraft-specific geometric information. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13)
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14. A system for initiating health monitoring for an aircraft by a ground station including a ground station computer system, the system comprising:
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a user interface configured to receive user input at the computer system of the ground station from an onboard computer system of the aircraft, the input including aircraft-specific geometric information regarding a plurality of details as to a make-up of the aircraft; a memory configured to store the aircraft-specific geometric information to a database in a memory of the computer system on the ground station; a set-up tool comprising a computer module executed by the ground station computer system of the ground station; and a processor configured to configure the computer system of the ground station using the aircraft specific geometric information via the set-up tool using a processor; wherein the computer system of the ground station is generic to various different aircraft, and is configured for specific use in connection with a specific aircraft based on the aircraft-specific geometric information from the aircraft, and specifically configured for use in connection with an onboard computer system residing onboard the aircraft, via the set-up tool based on the aircraft-specific geometric information; and wherein the processor is configured to configure the ground station by utilizing the aircraft-specific geometric information to; select a plurality of algorithms for a program of the ground station that are tailored specifically for the aircraft based on the aircraft-specific geometric information; and select a plurality of parameters for the selected plurality of algorithms, the selected plurality of parameters also tailored specifically for the aircraft based on the aircraft-specific geometric information. - View Dependent Claims (15, 16, 17, 18, 19)
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20. A method for initiating health monitoring for an aircraft by a ground station, the ground station including a ground station computer system and a set-up tool, the set-up tool comprising a computer module executed by the ground station computer system, the method comprising the steps of:
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receiving user input at the computer system of the ground station from an onboard computer system of the aircraft, the user input including aircraft-specific geometric information regarding a plurality of details as to a make-up of the aircraft; downloading the aircraft-specific geometric information to a database in a memory of the computer system on the ground station; and configuring the ground station computer system using the aircraft specific geometric information via the set-up tool using a processor; wherein the ground station computer system is generic to various different aircraft design configurations, and is configured for specific use in connection with a specific aircraft design configuration, corresponding to the aircraft based on the aircraft-specific geometric information from the aircraft, and specifically configured for use in connection with an onboard computer system residing onboard the aircraft, via the set-up tool based on the aircraft-specific geometric information; and wherein the step of configuring the ground station comprises utilizing the aircraft-specific geometric information to select a plurality of algorithms for a program of the ground station that are tailored specifically for the aircraft based on the aircraft-specific geometric information, and utilizing the aircraft-specific geometric information to select a plurality of parameters for the selected algorithms based on the aircraft-specific geometric information.
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Specification