Control method of multi-constraint-condition airborne fuel oil transportation
The invention belongs to the technical field of airborne fuel transportation control and management thereof, in particular to a control method of multi-constraint-condition airborne fuel oil transportation. The method comprises the following steps that flight profile information is acquired, flight...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The invention belongs to the technical field of airborne fuel transportation control and management thereof, in particular to a control method of multi-constraint-condition airborne fuel oil transportation. The method comprises the following steps that flight profile information is acquired, flight profile information at the current moment of an aircraft is acquired; a preferential oil supply tankdetermining step is carried out, the airborne fuel tank which is preferentially used for supplying oil to the aircraft at the current moment is determined according to the flight profile informationand aircraft parameters, the part of the airborne fuel tank is called the preferential oil supply tank; and the fuel oil transportation determining step is carried out, a transport scheme of the airborne fuel of the aircraft at the current moment is determined according to the number of the airborne fuel tank in the preferential oil supply tank and the fuel consumption rate at the current moment of the aircraft.
本申请属于机载燃油输 |
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