Method and system for generating an alert for an aircraft potentially exceeding speed limits in restricted airspace

• US 10,569,898 B2
• Filed: 03/26/2018
• Issued: 02/25/2020
• Est. Priority Date: 03/26/2018
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Feyereisen, Thea L., He, Gang, Engels, Jary, Samuthirapandian, Subash
• Primary Examiner(s): Brushaber, Frederick M
• Application Number:
  US15/935,943
• Publication Number:
  US 20190291889A1
• Time in Patent Office: 701 Days
• 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: B64D 45/00 Aircraft indicators or protectors not otherwise provided for camouflage F41H3/00
• CPC Class Codes: G01C 23/00 Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
• CPC Class Codes: G01C 23/005 Flight directors indicating arrangements specially adapted for rotary gyroscopes G01C19/32
• CPC Class Codes: G08G 5/0013 with a ground station
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/003 Flight plan management
• CPC Class Codes: G08G 5/0052 for cruising combined instruments indicating more than one navigational value G01C23/00
• CPC Class Codes: G08G 5/006 in accordance with predefined flight zones, e.g. to avoid prohibited zones

Abstract

Methods and systems are provided for generating an alert for an aircraft potentially exceeding speed limits in airspace with speed limitations. The method comprises retrieving a flight plan for the aircraft and identifying airspace with speed limitations along the flight plan. A speed profile is generated based on the in-flight aircraft'"'"'s current position, speed and trajectory. Any predicted speed violations are identified by comparing the speed profile with the airspace with speed limitations along the flight plan. A predictive time window is calculated that allows for the in-flight aircraft to decelerate sufficiently to comply with the speed limits of the airspace with speed limitations. The predictive time window includes a zone for the aircraft to reduce its airspeed and a reaction buffer zone to allow the aircrew sufficient time to comply with instructions to decelerate the aircraft. Finally, an alert is generated for the crew of the in-flight aircraft upon entering the predictive time window.

Claims

1. A method for generating an alert for an aircraft potentially exceeding speed limits in airspace with speed limitations, comprising:

retrieving a flight plan for an in-flight aircraft from an electronic storage device on board the aircraft;

identifying speed limited airspace along the flight plan by comparing the flight plan with data retrieved from a navigational database, where the speed limited airspace comprises a defined airspace that is classified by regulatory authorities as having a speed limit for aircraft within the defined airspace;

generating a predictive speed profile based on the in-flight aircraft'"'"'s current position, speed and trajectory;

identifying any predicted speed violations by comparing the predictive speed profile with the identified speed limited airspace along the flight plan;

calculating a predictive time window that allows for the in-flight aircraft to decelerate sufficiently to comply with the speed limits of the speed limited airspace, where the predictive time window includes,

a sufficient time period for the in-flight aircraft to reduce its airspeed based on a predetermined deceleration rate, and

a reaction buffer time period to allow the aircrew of the in-flight aircraft sufficient time to comply with instructions to decelerate the in-flight aircraft; and

generating an alert for the crew of the in-flight aircraft upon entering the predictive time window, where the alert is displayed on a graphical display device on board the aircraft.

2. The method of claim 1, where the electronic storage device onboard the aircraft comprises an onboard flight management system (FMS).

3. The method of claim 1, where the speed limited airspace is identified from data retrieved via a data communication link from an off board navigational database.

4. The method of claim 3, where a new predictive speed profile is generated upon detection of any change to the in-flight aircraft'"'"'s current position, speed or trajectory.

5. The method of claim 1, where the predictive speed profile is continuously monitored for any change to the in-flight aircraft'"'"'s current position, speed or trajectory.

6. The method of claim 1, where the predetermined deceleration rate is 2 knots per second.

7. The method of claim 1, where the alert comprises an audio notification.

8. The method of claim 1, where the alert comprises a textual notification.

9. The method of claim 1, where the alert comprises a graphic display notification.

10. The method of claim 1, where the alert may be manually deactivated by the crew of the in-flight aircraft.

11. A system for generating an alert for an in-flight aircraft potentially exceeding speed limits in airspace with speed limitations, comprising:

an electronic data storage medium that stores the flight plan for an in-flight aircraft;

an electronic navigational database that stores data regarding airspace with speed limitations;

a microprocessor located on board the in-flight aircraft, the microprocessor configured to,

retrieve the flight plan for the in-flight aircraft from the electronic data storage medium,

identify airspace with speed limitations along the flight plan by comparing the flight plan with data retrieved from the electronic navigational database, where the airspace with speed limitations comprises a defined airspace that is classified by regulatory authorities as having a speed limit for aircraft within the airspace,

generate a predictive speed profile based on the in-flight aircraft'"'"'s performance parameters,

identify any predicted speed violations of the in-flight aircraft by comparing the predictive speed profile with the identified airspace with speed limitations along the flight plan,

calculate a predictive time window that allows for the in-flight aircraft to decelerate sufficiently to comply with the speed limits of the airspace with speed limitations, where the predictive time window includes, a sufficient time period for the in-flight aircraft to reduce its airspeed based on a predetermined deceleration rate, and a reaction buffer time period to allow the aircrew of the in-flight aircraft sufficient time to comply with instructions to decelerate the in-flight aircraft, and

generate an alert upon the in-flight aircraft entering the predictive time window; and

a graphical display device that receives the alert from the microprocessor and displays the alert to the crew of the in-flight aircraft.

12. The system of claim 11, where the electronic data storage medium comprises a flight management system (FMS).

13. The system of claim 11, where the electronic navigational database is located off board the in-flight aircraft.

14. The system of claim 11, where the electronic navigational database is located on board the in-flight aircraft.

15. The system of claim 11, where the performance parameters of the in-flight aircraft comprise the in-flight aircraft'"'"'s position.

16. The system of claim 11, where the performance parameters of the in-flight aircraft comprise the in-flight aircraft'"'"'s speed.

17. The system of claim 11, where the performance parameters of the in-flight aircraft comprise the in-flight aircraft'"'"'s heading.

18. A method for generating an alert for an aircraft potentially exceeding speed limits in airspace with speed limitations, comprising:

generating a predictive speed profile based on the in-flight aircraft'"'"'s current position, speed and trajectory;

identifying airspace with speed limitations with data retrieved from a navigational database, where the airspace with speed limitations comprises a defined airspace that is classified by regulatory authorities as having a speed limit for aircraft within the airspace;

identifying any predicted speed violations by comparing the predictive speed profile with the identified airspace with speed limitations;

calculating a predictive time window that allows for the in-flight aircraft to decelerate sufficiently to comply with the speed limits of the airspace with speed limitations, where the predictive time window includes,

a sufficient time period for the in-flight aircraft to reduce its airspeed based on a predetermined deceleration rate, and

a reaction buffer time period to allow the aircrew of the in-flight aircraft sufficient time to comply with instructions to decelerate the in-flight aircraft; and

generating an alert for the crew of the in-flight aircraft upon entering the predictive time window, where the alert is displayed on a graphical display device on board the aircraft.