Determining a descent trajectory described by an aircraft intent description language (AIDL)

Patent metadata

Field	Value
Publication number	US-9766630-B2
Application number	US-201514703506-A
Country	US
Kind code	B2
Filing date	May 4, 2015
Priority date	May 23, 2014
Publication date	Sep 19, 2017
Grant date	Sep 19, 2017

Abstract

Determining a descent trajectory described by an Aircraft Intent Description Language (AIDL) is disclosed. An example method includes accessing historical flight data for a recorded flight trajectory, the recorded flight trajectory having been performed by a first aircraft type of multiple aircraft types and for a first airline of multiple airlines; estimating, using a processor, an aircraft intent parameter and an initial condition of the recorded flight trajectory based on an aircraft intent description language (AIDL) representation of the recorded flight trajectory; and mapping, using the processor, the aircraft intent parameter and the initial condition to a combination of the first aircraft type, the first airline, and an identified intended descent procedure.

First claim

The invention claimed is:

1. A method comprising:
accessing historical flight data for a recorded flight trajectory, the recorded flight trajectory having been performed by a first aircraft of a first aircraft type of multiple aircraft types and for a first airline of multiple airlines;
calculating, using a trajectory predictor, a plurality of trajectories for the first aircraft using (1) an initial condition of the first aircraft, and (2) a plurality of values for an aircraft intent parameter;
determining, using an optimization module, an optimal value of the plurality of values for the aircraft intent parameter that results in a calculated trajectory that best fits the recorded flight trajectory;
mapping the optimal value of the aircraft intent parameter to a combination of the first aircraft type, the first airline, and an identified intended descent procedure;
providing, in response to a request to predict a trajectory of a second aircraft of the first aircraft type, the first airline, and the identified intended descent procedure, the optimal value of the aircraft intent parameter from the optimization module to the trajectory predictor; and
calculating, using the trajectory predictor, a trajectory of the second aircraft using (1) an initial condition of the second aircraft and (2) the optimal value of the aircraft intent parameter.

2. The method as defined in claim 1 , further including storing the historical flight data for the recorded flight trajectory based on observing the recorded flight trajectory of the first aircraft of the first aircraft type and for the first airline, the historical flight data including positions of the first aircraft during an observed time period and weather information for the observed time period, the calculating of the plurality of trajectories being based on the positions of the first aircraft and the weather information.

3. The method as defined in claim 1 , wherein the calculating of the plurality of trajectories includes:
calculating, using the trajectory predictor, a lateral path of the first aircraft corresponding to the recorded flight trajectory based on an operational procedure associated with an airport that is associated with the recorded flight trajectory;
calculating, using the trajectory predictor, a vertical profile of the first aircraft corresponding to the recorded flight trajectory and corresponding to the lateral path; and
calculating, using the trajectory predictor, speeds of the first aircraft over the lateral path and the vertical profile, the calculating of the plurality of trajectories being based on the lateral path, the vertical profile, and the speeds.

4. The method as defined in claim 1 , wherein the calculating of the plurality of trajectories includes:
calculating, using the trajectory predictor, a first trajectory using a first value for the aircraft intent parameter and using a first aircraft intent procedure; and
calculating, using the trajectory predictor, a second trajectory using a second value for the aircraft intent parameter and using a second aircraft intent procedure; and
wherein the determining of the optimal value includes:
determining, using the optimization module, a first total error between the first trajectory and the recorded flight trajectory;
determining, using the optimization module, a second total error between the second trajectory and the recorded flight trajectory; and
selecting, using the optimization module, the first value of the aircraft intent parameter as the optimal value of the aircraft intent parameter when the first total error is less than the second total error.

5. The method as defined in claim 4 , wherein the calculating of the first trajectory includes applying a constraint to the first aircraft intent procedure to define the first aircraft intent procedure to be within a flight envelope of the first type of aircraft.

6. The method as defined in claim 4 , wherein the first aircraft intent procedure is an idle descent defined based on a throttle-law instruction, and the second aircraft intent procedure is a non-idle descent defined based on an altitude-law instruction.

7. The method as defined in claim 4 , wherein the calculating of the first trajectory using the first aircraft intent procedure includes describing the first aircraft intent procedure using an instance of aircraft intent description language, the instance including at least one of an idle descent or a non-idle descent and describing a deceleration process of the idle descent or the non-idle descent using at least one of a level-off segment or by a speed reduction.

8. The method as defined in claim 1 , wherein the historical flight data includes combinations of a longitude coordinate, a latitude coordinate, an altitude, and a ground speed.

9. The method as defined in claim 1 , wherein the initial condition of the first aircraft includes longitude and latitude coordinates, an altitude, and a ground speed of the first aircraft corresponding to the recorded flight trajectory.

10. The method as defined in claim 1 , wherein the calculating of the plurality of trajectories is based on an aircraft performance model of the first aircraft corresponding to the recorded flight trajectory.

11. The method as defined in claim 1 , wherein the second aircraft is an aircraft approaching a terminal maneuvering area.

12. The method as defined in claim 1 , wherein the aircraft intent parameter is a mass of the first aircraft.

13. A tangible computer readable storage medium comprising computer readable instructions which, when executed, cause a processor to at least:
access historical flight data for a recorded flight trajectory, the recorded flight trajectory having been performed by a first aircraft of a first aircraft type of multiple aircraft types and for a first airline of multiple airlines;
calculate, using a trajectory prediction process, a plurality of trajectories for the first aircraft using (1) an initial condition of the first aircraft, and (2) a plurality of values for an aircraft intent parameter;
determine, using an optimization process, an optimal value of the plurality of values for the aircraft intent parameter that results in a calculated trajectory that best fits the recorded flight trajectory;
map the optimal value of the aircraft intent parameter to a combination of the first aircraft type, the first airline, and an identified intended descent procedure; and
calculate, using the trajectory prediction process, in response to a request to predict a trajectory of a second aircraft of the first aircraft type, the first airline, and the identified intended descent procedure, a trajectory of the second aircraft using (1) an initial condition of the second aircraft and (2) the optimal value of the aircraft intent parameter.

14. The storage medium as defined in claim 13 , wherein the instructions are further to cause the processor to store the historical flight data for the recorded flight trajectory based on observing the recorded flight trajectory of the first aircraft of the first aircraft type and for the first airline, the historical flight data including positions of the first aircraft during an observed time period and weather information for the observed time period, the instructions to cause the processor to calculate the plurality of trajectories based on the positions of the first aircraft and the weather information.

15. The storage medium as defined in claim 13 , wherein the instructions are to cause the processor to calculate, using the trajectory prediction process, the plurality of trajectories by:
calculating a lateral

Assignees

• Boeing Co

Inventors

• Casado Magaña Enrique Juan
• D'Alto Luis Pedro
• Vilaplana Ruiz Miguel

Classifications

• G08G5/0026

  Physics · mapped topic

• G05D1/0676 Primary

  specially adapted for landing · CPC title

• G08G5/025

  Physics · mapped topic

• G08G5/0043

  Physics · mapped topic

• G08G5/0082

  Physics · mapped topic