Predicting aircraft trajectory

• US 9,250,099 B2
• Filed: 01/25/2015
• Issued: 02/02/2016
• Est. Priority Date: 09/21/2007
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Felix, Francisco A. Navarro, Ruiz, Miguel A. Vilaplana, Querejeta, Carlos, Gallo, Eduardo, Leones, Javier Lopez
• Primary Examiner(s): Cheung, Mary
• Assistant Examiner(s): WONG, YUEN H
• Application Number:
  US14/604,723
• Publication Number:
  US 20150226576A1
• Time in Patent Office: 373 Days
• US Class Current: 1/1
• CPC Class Codes: B64D 43/00 Arrangements or adaptations of instruments arrangements of cameras B64D47/08; aeronautical measuring instruments per se G01C
• CPC Class Codes: G01C 23/005 Flight directors indicating arrangements specially adapted for rotary gyroscopes G01C19/32
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/0052 for cruising combined instruments indicating more than one navigational value G01C23/00
• CPC Class Codes: G08G 5/0065 for taking-off
• CPC Class Codes: G08G 5/025 Navigation or guidance aids radar or analogous systems specially adapted for landing purposes G01S13/913
• CPC Class Codes: G08G 5/045 Navigation or guidance aids, e.g. determination of anti-collision manoeuvers radar or analogous systems specially adapted for anti-collision between aircraft G01S13/933

Abstract

The present invention provides a computer-implemented method of producing a description of aircraft intent expressed using a formal language. The description may be used to predict aircraft trajectory, for example by air traffic management. Rules are used in association with information provided to generate a set of instructions describing both the aerodynamic configuration of the aircraft and the motion of the aircraft. These instructions are checked to ensure that they describe unambiguously the aircraft'"'"'s trajectory. The instructions are then expressed using a formal language.

Claims

1. A method of predicting a trajectory of an aircraft and operating the aircraft, comprising:

receiving, at a processor, information defining how the aircraft is to be flown during an operation interval, and storing the information in an information database;

deriving, by the processor, a set of instructions from the information stored, wherein the set of instructions comprise configuration instructions that describe an aerodynamic configuration of the aircraft and motion instructions that control an aircraft motion, wherein the aerodynamic configuration comprises a physical configuration of at least one of a high lift device of the aircraft, a landing gear of the aircraft, and a speed brake of the aircraft;

confirming, by the processor, that the set of instructions comply with a set of rules stored in a rules database, that the configuration instructions define the aerodynamic configuration of the aircraft and that the motion instructions close degrees of freedom of equations of motion used to describe the aircraft motion during the operation interval;

thereafter formulating, by the processor using the set of instructions, an aircraft intent;

solving, by the processor, a trajectory optimization problem defined by the aircraft intent according to a predefined criterion to obtain an optimized trajectory; and

operating the aircraft according to the optimized trajectory.

2. The method of claim 1, wherein deriving the set of instructions comprises identifying from the information stored information relating to how the aircraft is to be configured, to produce configuration-related information, and providing configuration instructions based on the configuration-related information.

3. The method of claim 1 wherein confirming comprises ensuring that the set of instructions includes one and only one of each of a high-lift related instruction, a landing gear related instruction and a speed brakes related instruction.

4. The method of claim 1, wherein deriving the set of instructions comprises identifying from the information stored information determining the motion of the aircraft, to produce motion-related information, and providing motion instructions based on the motion-related information.

5. The method of claim 4, comprising identifying information relating to lateral motion, vertical motion and speed, and providing motion instructions that determine the lateral motion, vertical motion and speed.

6. The method of claim 5, wherein confirming comprises ensuring that there are three motion instructions, each motion instruction closing one degree of freedom.

7. The method of claim 1, wherein confirming comprises ensuring that the instructions do not provide conflicting requirements.

8. The method of claim 1, wherein instructions are placed into groups, such that instructions are first distributed according to their effect and then incompatible instructions are grouped together.

9. The method of claim 8, comprising deriving the set of instructions such that the set only contains one instruction from each group.

10. The method of claim 1, wherein receiving information comprises receiving information relating to aircraft operator preferences, how a pilot intends to fly the aircraft, or departure/arrival procedures to be followed during a flight.

11. The method of claim 1, further comprising:

expressing the set of instructions using a formal language by providing either necessary information or references to where the necessary information is found, to solve equations of motion describing aircraft flight and so compute a trajectory of the aircraft.

12. The method of claim 11, wherein providing references to where the information is found comprises providing references to a database storing information relating to the aircraft performance or atmospheric conditions.

13. The method of claim 11, comprising providing a graphical display of the set of instructions expressed using the formal language.

14. A method of predicting a trajectory of an aircraft and operating the aircraft, the method comprising:

reading, by a processor, data providing a description of aircraft intent expressed using a formal language, the data provided by;

receiving information defining how the aircraft is to be flown during an operation interval, and storing the information in an information database;

deriving a set of instructions from the information stored, wherein the set of instructions comprise configuration instructions that describe an aerodynamic configuration of the aircraft and motion instructions that control an aircraft motion, wherein the aerodynamic configuration comprises a physical configuration of at least one of a high lift device of the aircraft, a landing gear of the aircraft, and a speed brake of the aircraft;

confirming, by the processor ensuring that the set of instructions comply with a set of rules stored in a rules database, that the configuration instructions define the aerodynamic configuration of the aircraft and that the motion instructions close degrees of freedom of equations of motion used to describe the aircraft motion during the operation interval; and

expressing the set of instructions using the formal language;

solving, by the processor, equations of motion defining aircraft motion using the data and with reference to an aircraft performance model and an Earth model, whereby solved equations of motion are produced; and

operating the aircraft using at least the predicted trajectory and the solved equations of motion.

15. A method of air traffic management, the method comprising:

predicting, by a processor, trajectories of at least two aircraft, comprising for each prediction;

reading data providing a description of aircraft intent expressed using a formal language, the data provided by;

receiving information defining how the at least two aircraft are to be flown during an operation interval, and storing the information in an information database;

deriving a set of instructions from the information stored, wherein the set of instructions comprise configuration instructions that describe an aerodynamic configuration of the at least two aircraft and motion instructions that control motions of the at least two aircraft, wherein the aerodynamic configuration comprises a physical configuration of at least one of a high lift device, a landing gear, and a speed brake of each of the at least two aircrafts;

confirming, by the processor, that the set of instructions comply with a set of rules stored in a rules database, that the configuration instructions define the aerodynamic configuration of the at least two aircraft and that the motion instructions close degrees of freedom of equations of motion used to describe the aircraft motion of the at least two aircraft during the operation interval; and

expressing the set of instructions using the formal language;

solving, by the processor, equations of motion defining the aircraft motion using the data and with reference to an aircraft performance model and an Earth model;

comparing, by the processor, the at least two predicted trajectories to identify potential conflicts; and

managing, by the processor, air traffic, including the at least two aircraft, using the at least two predicted trajectories.

16. The method of claim 15, further comprising resolving conflicts by advising aircraft of necessary changes to their aircraft intent.

17. A method of avoiding aircraft collisions, comprising:

an aircraft predicting a trajectory of the aircraft, comprising;

reading, by a processor on the aircraft, data providing a description of aircraft intent expressed using a formal language, the data provided by;

receiving information defining how the aircraft is to be flown during an operation interval, and storing the information in an information database;

deriving a set of instructions from the information stored, wherein the set of instructions comprise configuration instructions that describe an aerodynamic configuration of the aircraft and motion instructions that control an aircraft motion, wherein the aerodynamic configuration comprises a physical configuration of at least one of a high lift device of the aircraft, a landing gear of the aircraft, and a speed brake of the aircraft;

confirming, by the processor ensuring that the set of instructions comply with a set of rules stored in a rules database, that the configuration instructions define the aerodynamic configuration of the aircraft and that the motion instructions close degrees of freedom of equations of motion used to describe the aircraft motion during the operation interval; and

expressing the set of instructions using the formal language;

solving equations of motion defining aircraft motion using said data and with reference to an aircraft performance model and an Earth model; and

predicting the trajectory of the aircraft to form a predicted trajectory of the aircraft;

receiving, by the processor, a set of instructions expressed in the formal language that relate to an aircraft intent of another aircraft;

predicting, by the processor, a trajectory of the another aircraft;

comparing, by the processor, the two predicted trajectories to identify any conflicts in the two predicted trajectories between the aircraft and the another aircraft, wherein an identified conflict is formed; and

issuing, by the processor, instructions to the aircraft and the another aircraft to avoid the aircraft collisions based on the identified conflict.

18. The method of claim 17, comprising providing a graphical display of the predicted trajectories on a graphical display connected to the processor and on the aircraft.