System and method for transmitting obstacle alerts to aircraft from a ground based database

Patent metadata

Field	Value
Publication number	US-10347141-B2
Application number	US-201715498032-A
Country	US
Kind code	B2
Filing date	Apr 26, 2017
Priority date	Apr 26, 2017
Publication date	Jul 9, 2019
Grant date	Jul 9, 2019

Abstract

A method for providing obstacle alerts to an in-flight aircraft has been developed. First, parameters of an in-flight aircraft are transmitted to a ground based processor station. The station calculates an aircraft safety envelope based on these parameters. The station accesses the characteristics of obstacles stored in a terrain database and calculates an obstacle safety envelope. Finally, the station determines if the aircraft safety envelope conflicts with the obstacle safety envelope and generates an alert for the aircraft if a conflict exists.

First claim

What is claimed is:

1. A method for providing obstacle alerts to an in-flight aircraft, comprising:
transmitting parameters of the in-flight aircraft to a ground-based processor station;
calculating an aircraft safety envelope that surrounds the in-flight aircraft, where the aircraft safety envelope is based on the transmitted parameters of the in-flight aircraft with the ground-based processor station;
calculating an obstacle safety envelope that surrounds terrestrial obstacles, where the obstacle safety envelope is based on characteristics of terrestrial obstacles stored in a terrain database that is accessible by the ground-based processor station;
recalculating the aircraft safety envelope once every 3-4 seconds;
determining if the aircraft safety envelope conflicts with the obstacle safety envelope with the ground-based processor station; and
generating an obstacle alert for the in-flight aircraft if a conflict between the aircraft safety envelope and obstacle safety envelope exists.

2. The method of claim 1 , where the in-flight aircraft comprises a rotor aircraft.

3. The method of claim 2 , where the rotor aircraft comprises a helicopter.

4. The method of claim 2 , where the rotor aircraft comprises a tilt rotor aircraft.

5. The method of claim 1 , where the in-flight aircraft comprises an unmanned aerial vehicle (UAV).

6. The method of claim 5 , where the unmanned aerial vehicle is autonomously piloted.

7. The method of claim 5 , where the unmanned aerial vehicle is remotely piloted.

8. The method of claim 1 , where the parameters of the in-flight aircraft and the obstacle alert are transmitted via satellite communications (SATCOM).

9. The method of claim 1 , where the parameters of the in-flight aircraft and the obstacle alert are transmitted via very high frequency (VHF) radio.

10. The method of claim 1 , where the parameters of the in-flight aircraft and the obstacle alert are transmitted via high-frequency (HF) radio.

11. The method of claim 1 , where the aircraft safety envelope is periodically recalculated.

12. The method of claim 1 , where the obstacle safety envelope is additionally calculated based on atmospheric conditions.

13. The method of claim 12 , where the atmospheric conditions are accessible by the ground-based processor station via a real-time data stream.

14. A method for providing obstacle alerts to an in-flight aircraft, comprising:
transmitting parameters of the in-flight aircraft to a ground-based processor station:
calculating an aircraft safety envelope based on the transmitted parameters of the in-flight aircraft with the ground-based processor station;
calculating an obstacle safety envelope based on characteristics of terrestrial obstacles stored in a terrain database that is accessible by the ground-based processor station:
recalculating the aircraft safety envelope once every 3-4 seconds;
determining if the aircraft safety envelope conflicts with the obstacle safety envelope with the ground-based processor station; and
generating an obstacle alert for the in-flight aircraft if a conflict between the aircraft safety envelope and obstacle safety envelope exists.

15. A system for providing obstacle alerts to an in-flight aircraft, comprising:
a transceiver on board the in-flight aircraft that transmits flight performance parameters of the in-flight aircraft;
a remotely located antenna that receives the flight performance parameters from the transceiver;
a remotely located terrain database that stores obstacle characteristics of terrestrial obstacles located in proximity to the in-flight aircraft; and
a remotely located computer system that receives the flight performance parameters from the antenna and the obstacle characteristics in proximity to the in-flight aircraft from the terrain database, where the computer system calculates an aircraft safety envelope based on the flight performance parameters, where the aircraft safety envelope is recalculated once every 3-4 seconds, and an obstacle safety envelope based on the obstacle characteristics, where the computer system generates an obstacle alert for the in-flight aircraft if the aircraft safety envelope conflicts with the obstacle safety envelope.

Assignees

• Honeywell Int Inc

Inventors

• Singh Jayant Kumar
• Ambika Nithin
• Pal Subhadeep
• Gohil Saurabh

Classifications

• B64U2201/10

  autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS] · CPC title

• B64U2201/20

  Remote controls · CPC title

• G08G1/165

  for passive traffic, e.g. including static obstacles, trees · CPC title

• G08G9/02

  Anti-collision systems · CPC title

• B64C2201/146

  Operations & Transport · mapped topic