SYSTEM AND METHOD TO DETERMINE ENGINE THRUST OF A TAXIING AIRCRAFT

A computing device to determine engine thrust of an aircraft during taxiing. The computing device includes memory circuitry configured to store computer-readable program code. Processing circuitry is configured to execute the computer-readable program code to cause the computing device to: identify...

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Bibliographische Detailangaben
Hauptverfasser:	CABOS, Ralf Rene, SAKKAS, Spyridon
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT AVIATION CONTROLLING COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT MEASURING MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER,MECHANICAL EFFICIENCY, OR FLUID PRESSURE MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION,OR SHOCK PERFORMING OPERATIONS PHYSICS REGULATING SIGNALLING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TESTING TRAFFIC CONTROL SYSTEMS TRANSPORTING
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Beschreibung
Zusammenfassung:	A computing device to determine engine thrust of an aircraft during taxiing. The computing device includes memory circuitry configured to store computer-readable program code. Processing circuitry is configured to execute the computer-readable program code to cause the computing device to: identify an aircraft on an airport surface; calculate an acceleration of the aircraft during the taxiing of the aircraft; compare the acceleration with predetermined data from similar aircraft; and based on the comparison, determine an engine thrust for the aircraft while the aircraft is taxiing.