Ground based system and methods for providing multiple flightplan re-plan scenarios to a pilot during flight
First Claim
1. A method of re-routing an aircraft during flight, comprising:
- a processor configured for determining an existence of an in-flight incursion requiring a work around;
the processor configured for receiving a re-routing request from the aircraft;
the processor configured for computing re-routing options based on at least two of weather, air and ground traffic, aircraft fuel level, wind speed and direction, turbulence, electrical and mechanical problems with the aircraft, airspace restrictions, and diversion, the processor further configured for computing the re-routing options based on a set of pilot defined bounds associated with a pilot of the aircraft, and for generating the re-routing options such that the re-routing options are within the set of pilot defined bounds;
the processor configured for transmitting “
N”
number of the re-routing options to the aircraft;
the processor configured for receiving a selection, from the aircraft, of a unique one of the re-routing options; and
the processor configured for uplinking a micro flight plan corresponding to the selected re-routing option to an on-board flight management system (FMS) of the aircraft.
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Accused Products
Abstract
Methods and apparatus are provided for transmitting re-routing options to a plurality of in-flight aircraft in accordance with preconfigured pilot preferences. The apparatus comprises a data store module containing data sets against which the pilot preferences are evaluated during flight, including weather, airspace and flight restrictions, ground delay programs, and air traffic information. The apparatus further includes a flight path module containing route and position information for each aircraft. An incursion alert processing module evaluates the flight path, data store, and pilot preferences and generates incursion alerts which are transmitted to each aircraft during flight. Upon receipt of an incursion alert or, alternatively, independent of an incursion alert, the pilot may request re-routing options. Once received and reviewed, the pilot selects the optimum re-routing option, and an associated micro flight plan is uplinked and loaded into the FMS (Flight Management System).
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Citations
18 Claims
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1. A method of re-routing an aircraft during flight, comprising:
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a processor configured for determining an existence of an in-flight incursion requiring a work around; the processor configured for receiving a re-routing request from the aircraft; the processor configured for computing re-routing options based on at least two of weather, air and ground traffic, aircraft fuel level, wind speed and direction, turbulence, electrical and mechanical problems with the aircraft, airspace restrictions, and diversion, the processor further configured for computing the re-routing options based on a set of pilot defined bounds associated with a pilot of the aircraft, and for generating the re-routing options such that the re-routing options are within the set of pilot defined bounds; the processor configured for transmitting “
N”
number of the re-routing options to the aircraft;the processor configured for receiving a selection, from the aircraft, of a unique one of the re-routing options; and the processor configured for uplinking a micro flight plan corresponding to the selected re-routing option to an on-board flight management system (FMS) of the aircraft. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13)
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14. A method of re-routing an aircraft during flight, comprising:
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a processor configured for determining an in-flight incursion based on a flight path of said aircraft that requires a work around; the processor configured for generating an incursion alert based on the determination; the processor configured for receiving a re-routing request from said aircraft based on said incursion alert; the processor configured for computing re-routing options based on at least two of weather, air and ground traffic, aircraft fuel level, wind speed and direction, turbulence, electrical and mechanical problems with the aircraft, airspace restrictions, and diversion, said re-routing options associated with the flight path of said aircraft, the processor further configured for computing the re-routing options based on a set of pilot defined bounds associated with a pilot of the aircraft, the set of pilot defined bounds including parameters for air speed, direction and altitude, and for generating the re-routing options such that the re-routing options are within the set of pilot defined bounds; the processor configured for transmitting “
N”
number of the re-routing options to the aircraft;the processor configured for receiving a selection, from the aircraft, of a unique one of the re-routing options; and the processor configured for unlinking a micro flight plan corresponding to the selected re-routing option to an on-board flight management system (FMS) and for loading said micro flight plan into said on-board flight management system (FMS) of said aircraft. - View Dependent Claims (15, 16, 17, 18)
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Specification