METHOD, SYSTEM, AND COMPUTER-READABLE MEDIUM FOR CALIBRATING PERFORMANCE PARAMETERS OF AN AIRCRAFT DURING A PHANTOM FUEL PROCEDURE
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United States of America
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Issued Date -
Dec 19, 2024
app pub date -
Jun 13, 2024
filing date -
Jun 13, 2024
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Abstract
A system, method, and computer-readable medium for calibrating performance parameters of an aircraft during a phantom fuel procedure, including determining an independent fuel weight parameter during operation of the aircraft value based on output of fuel level sensors of a fuel quantity subsystem coupled to the aircraft flight control system, receiving a zero fuel weight parameter, receiving a fuel weight parameter corresponding to a weight of fuel onboard the aircraft and a phantom fuel value, determining a gross weight parameter based on the zero fuel weight, determining a fuel consumption parameter value of the aircraft based on output of fuel flow sensors coupled to the aircraft flight control system, updating the gross weight parameter during operation of the aircraft based on the fuel weight parameter and the fuel consumption parameter value, and determining performance parameter for the aircraft during operation of the aircraft based on the gross weight parameter.
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