The Boeing Company

Sheila Ruth Conway

Charles Otis Adler

Douglas A Stoll

A method, computing system and computer program product are provided to identify the alignment of an aircraft with an incorrect surface, such as a taxiway or a runway that is closed or unsuited for current conditions. In a method, the trajectory of an aircraft approaching an airport is determined. Based upon the trajectory and information regarding a configuration of the airport, the method determines whether the aircraft is approaching the incorrect surface. If the aircraft is approaching the incorrect surface, the method interacts via an interface to cause an alert to be issued. If the aircraft is approaching a correct surface, the method determines whether the trajectory of the aircraft is consistent with predefined procedures of the airport. If the trajectory of the aircraft is inconsistent with predefined procedures of the airport, the method interacts via the interface to cause the alert to be issued.

Method and computing system for identifying incorrect aircraft alignment

An example method for modifying a flight path of an aircraft includes receiving real time positioning estimates for an aircraft, receiving an actual navigation performance (ANP) of the aircraft informative of uncertainty in the position estimate, receiving a required navigation performance (RNP) instrument flight procedure for the aircraft, receiving spacing input from an air traffic controller that indicates spacing requirements between the aircraft and one or more other aircraft, receiving information relating to communities underneath the flight path, calculating, by a system onboard the aircraft, a modification to the flight path to be flown by the aircraft that causes the aircraft to remain within the containment boundaries of the RNP instrument flight procedure while reducing noise impact to the communities underneath the flight path and meeting the spacing requirements of the air traffic controller, and displaying a visual representation of a modified flight path for the aircraft.

Performance-based track variation for aircraft flight management

An example method for aircraft traffic spacing and timing control with flight path variation of an aircraft includes receiving information of aircraft traffic for an area, determining an aircraft spacing plan for the aircraft traffic for the area based on spacing requirements due to separation standards or flow management constraints for the aircraft traffic, determining that a modification to a flight path of an aircraft is required to meet a longitudinal spacing requirement between the aircraft and one or more additional aircraft of the aircraft traffic based on the aircraft spacing plan, determining a flight path modification to the flight path for the aircraft based on the modification that causes the aircraft to remain within associated margins of the RNP instrument flight procedure and alters the longitudinal spacing between the aircraft and the additional aircraft of the aircraft traffic, and assigning the flight path modification to the aircraft via a data communication link.

Aircraft traffic spacing and timing control with dynamic flight path variation

An example method for flight path variation of an aircraft for noise management includes receiving noise inquiries of a community related to aircraft noise during flight over the community, receiving an output from noise sensors positioned within the community, determining a noise distribution plan for additional aircraft flying over the community so as to steer the additional aircraft and distribute additional aircraft noise in response to the noise inquiries and the output from the noise sensors, and based on flight path data of the additional aircraft and the noise distribution plan, assigning a flight path modification to aircraft via a data communication link. The flight path modification informs the aircraft to adjust the flight path to remain within associated margins of a required navigation performance (RNP) instrument flight procedure and to reduce noise impact to the community underneath the flight path.

Community noise management with aircraft dynamic path variation

A method, computing system and computer program product are provided to monitor compliance with a non-transgression zone between aircraft approach corridors, thereby facilitating simultaneous instrument approaches. In the context of a method, a predicted path of an aircraft is determined during a flight based upon at least a representation of a roll angle of the aircraft and a cross-track component of the velocity of the aircraft. The method also includes identifying an instance in which the predicted path of the aircraft during the flight intersects a non-transgression zone. The method further includes causing an alert to be issued in the instance in which the predicted path of the aircraft during the flight intersects the non-transgression zone.

Method and apparatus for monitoring compliance with a non-transgression zone between aircraft approach corridors

Method, system, and computer program product for monitoring vehicle compliance with a vehicle operating instruction provided by a traffic controller. A spoken vehicle operating instruction is translated into a computer-readable instruction that can be used for data entry and/or retrieval. The computer-readable instruction is transformed into an expected vehicle operating trajectory by mapping to a published vehicle procedure or by calculating a trajectory based on provided instructions. The vehicle is monitored as it operates. In the event the monitored operation differs or is forecast to differ from conformance limits associated with the expected trajectory, an alert can be provided.

Method and system to monitor for conformance to a traffic control instruction

A particular method includes receiving aircraft state data associated with an aircraft at an air traffic control system. The aircraft state data includes a detected position of the aircraft, a velocity of the aircraft and an orientation of the aircraft. The method also includes predicting at least one future position of the aircraft based on the aircraft state data. The method further includes generating an alert in response to comparing the predicted future position to an air traffic navigation constraint assigned to the aircraft.

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Seattle, WA, United States of America

Sheila Ruth Conway