Airborne Situational Awareness System

• US 20070222665A1
• Filed: 03/07/2007
• Published: 09/27/2007
• Est. Priority Date: 03/07/2006
• Status: Abandoned Application

• Current Assignee: Dimensional Research Incorporated
• Original Assignee: Dimensional Research Incorporated
• Inventors: Koeneman, Robert
• Application Number:
  US11/683,213
• Publication Number:
  US 20070222665A1
• Time in Patent Office: Days
• US Class Current: 342/29
• CPC Class Codes: G01S 13/933 of aircraft or spacecraft
• CPC Class Codes: G01S 19/18 Military applications
• CPC Class Codes: G08G 5/0008 with other aircraft
• CPC Class Codes: G08G 5/0021 located in the aircraft
• CPC Class Codes: G08G 5/0078 for monitoring traffic from the aircraft radar or analogous systems specially adapted for traffic control G01S13/91

Abstract

A digital airborne situational awareness system and method. The system is installed on multiple aircraft to generate an airborne network providing collision avoidance without ground control. A global positioning system (GPS) receiver unit is coupled to a microprocessor in each aircraft equipped with the system. A software engine receives the raw GPS data and determines location, speed, flight path direction, and altitude. The software engine conditions the GPS data for display on a cockpit display panel. The conditioned data orients the display with the heading, speed, and altitude data of the host system aircraft. A transceiver section provides data transmission to other airborne receiving units within the approximately forty mile range of the airborne network. The transceiver transmits data packets including reconditioned location (track), altitude, and an aircraft class identifier to other aircraft in the network. The transceiver receives data from other airborne vehicles equipped with the system within the network range. Once the computations of positional data for other aircraft are performed, the positional data is sent to the display processing section for appropriate cockpit display. The software engine develops a set of projections that are compared to the relative speed, flight path direction and altitude of the all other units in the airborne network. These projections determine the threat levels of converging flight paths with limits that provide warning data to the pilot of any pending flight path conflict situation.

Claims

1. A method for generating an airborne network for collision avoidance without ground control, wherein the airborne network includes a plurality of aircraft, the method comprising:

establishing a data link for each aircraft to a plurality of navigational satellites for providing global positioning system (GPS) data including location, heading and speed at each time fix for each aircraft;

receiving GPS data and converting the location data into a Cartesian coordinate system data for each aircraft;

transmitting the converted location, heading, speed and time fix data from a host aircraft to a plurality of target aircraft within a coverage range of the network;

receiving the converted location, heading, speed and time fix data from the plurality of target aircraft;

displaying a relative position of each target aircraft to the host aircraft;

determining if any target aircraft is on a collision course with the host aircraft;

providing a warning alert to the host aircraft if any target aircraft is on a collision course with the host aircraft; and

automatically providing a course deviation for the host aircraft to avoid collision.

2. The method for generating an airborne network for collision avoidance of claim 1 wherein the received GPS data conforms to a pre-specified serial data protocol format.

3. The method for generating an airborne network for collision avoidance of claim 2 wherein the received GPS location data includes latitude, longitude, height above mean sea level, and height above ground level.

4. The method for generating an airborne network for collision avoidance of claim 1 wherein the Cartesian coordinate system comprises the Earth-centered Earth-Fixed (ECEF) coordinate system.

5. The method for generating an airborne network for collision avoidance of claim 1 further comprising determining if any target aircraft projected location will approach within a proximity threshold value of the host aircraft location.

6. The method for generating an airborne network for collision avoidance of claim 5 further comprising providing a caution alert to the host aircraft if any target aircraft projected location will approach within a proximity threshold value of the host aircraft location.

7. The method for generating an airborne network for collision avoidance of claim 1 wherein the warning alert comprises a flashing target symbol and an audio warbling tone.

8. The method for generating an airborne network for collision avoidance of claim 6 wherein the caution alert comprises a flashing target symbol and an audio warbling tone.

9. The method for generating an airborne network for collision avoidance of claim 1 wherein displaying a relative position of each target aircraft to the host aircraft comprises:

determining a down range, cross range and altitude differentials between the host aircraft and each target aircraft;

determining a relative position of each target aircraft from the host aircraft based upon the down range, cross range and altitude differentials between the host aircraft and each target aircraft; and

plotting the relative position of each target aircraft on a multi-dimensional display.

10. The method for generating an airborne network for collision avoidance of claim 9 wherein displaying a relative position of each target aircraft to the host aircraft further comprises plotting at least one target aircraft as a vector wherein the vector represents heading and speed of the at least one target aircraft.

11. The method for generating an airborne network for collision avoidance of claim 1 wherein automatically providing a course deviation for the host aircraft to avoid collision with a target aircraft comprises:

determining if an automatic reaction function is set on the host aircraft;

determining if an autopilot on the host aircraft is coupled to an airborne collision avoidance system;

setting a remaining time to initiate a course correction;

determining a course deviation for the host aircraft relative to the current heading; and

generating a steering command sequence to change the host aircraft'"'"'s heading based on the determined course deviation.

12. The method for generating an airborne network for collision avoidance of claim 11 wherein automatically providing a course deviation for the host aircraft to avoid collision with a target aircraft further comprises:

determining if a collision course conflict with the target aircraft has cleared; and

generating a steering command sequence to change the host aircraft'"'"'s heading to an intended course.

13. A system for generating an airborne network for collision avoidance without ground control, wherein the airborne network includes a plurality of aircraft, comprising:

a GPS receiver for establishing a data link for each aircraft to a plurality of navigational satellites and receiving global positioning system (GPS) data including location, heading and speed at each time fix for each aircraft;

a microprocessor coupled to the GPS receiver for executing a software engine comprising a plurality of modules including a module for converting the location data into a Cartesian coordinate system data for each aircraft;

a transceiver coupled to the microprocessor for transmitting the converted location, heading, speed and time fix data from a host aircraft to a plurality of target aircraft within a coverage range of the network and for receiving the converted location, heading, speed and time fix data from the plurality of target aircraft;

a component for displaying a relative position of each target aircraft to the host aircraft;

a module for determining if any target aircraft is on a collision course with the host aircraft;

a module for providing a warning alert to the host aircraft if any target aircraft is on a collision course with the host aircraft; and

a module for automatically providing a course deviation for the host aircraft to avoid collision.

14. The system for generating an airborne network for collision avoidance of claim 13 wherein the received GPS data conforms to a pre-specified serial data protocol format.

15. The system for generating an airborne network for collision avoidance of claim 14 wherein the received GPS location data includes latitude, longitude, height above mean sea level, and height above ground level.

16. The system for generating an airborne network for collision avoidance of claim 13 wherein the Cartesian coordinate system comprises the Earth-centered Earth-Fixed (ECEF) coordinate system.

17. The system for generating an airborne network for collision avoidance of claim 13 further comprising a module for determining if any target aircraft projected location will approach within a proximity threshold value of the host aircraft location.

18. The system for generating an airborne network for collision avoidance of claim 17 further comprising a module for providing a caution alert to the host aircraft if any target aircraft projected location will approach within a proximity threshold value of the host aircraft location.

19. The system for generating an airborne network for collision avoidance of claim 13 wherein the warning alert comprises a flashing target symbol and an audio warbling tone.

20. The system for generating an airborne network for collision avoidance of claim 18 wherein the caution alert comprises a flashing target symbol and an audio warbling tone.

21. The system for generating an airborne network for collision avoidance of claim 13 wherein the component for displaying a relative position of each target aircraft to the host aircraft comprises:

a module for determining a down range, cross range and altitude differentials between the host aircraft and each target aircraft;

a module for determining a relative position of each target aircraft from the host aircraft based upon the down range, cross range and altitude differentials between the host aircraft and each target aircraft; and

a module for plotting the relative position of each target aircraft on a multi-dimensional display.

22. The system for generating an airborne network for collision avoidance of claim 21 wherein the component for displaying a relative position of each target aircraft to the host aircraft further comprises a module for plotting at least one target aircraft as a vector wherein the vector represents heading and speed of the at least one target aircraft.

23. The system for generating an airborne network for collision avoidance of claim 13 wherein the module for automatically providing a course deviation for the host aircraft to avoid collision with a target aircraft comprises:

a module for determining if an automatic reaction function is set on the host aircraft;

a module for determining if an autopilot on the host aircraft is coupled to an airborne collision avoidance system;

a module for setting a remaining time to initiate a course correction;

a module for determining a course deviation for the host aircraft relative to the current heading; and

a module for generating a steering command sequence to change the host aircraft'"'"'s heading based on the determined course deviation.

24. The system for generating an airborne network for collision avoidance of claim 23 wherein the module for automatically providing a course deviation for the host aircraft to avoid collision with a target aircraft further comprises:

a module for determining if a collision course conflict with the target aircraft has cleared; and

a module for generating a steering command sequence to change the host aircraft'"'"'s heading to an intended course.

26. The computer program product for generating an airborne network for collision avoidance of claim 24 wherein the received GPS data conforms to a pre-specified serial data protocol format.

27. The computer program product for generating an airborne network for collision avoidance of claim 26 wherein the received GPS location data includes latitude, longitude, height above mean sea level, and height above ground level.

25. A computer program product for generating an airborne network for collision avoidance without ground control, wherein the airborne network includes a plurality of aircraft, comprising a computer readable medium having computer readable code embedded therein, the computer readable medium comprising:

program instructions for establishing a data link for each aircraft to a plurality of navigational satellites for providing global positioning system (GPS) data including location, heading and speed at each time fix for each aircraft;

program instructions for receiving GPS data and converting the location data into a Cartesian coordinate system data for each aircraft;

program instructions for transmitting the converted location, heading, speed and time fix data from a host aircraft to a plurality of target aircraft within a coverage range of the network;

program instructions for receiving the converted location, heading, speed and time fix data from the plurality of target aircraft;

program instructions for displaying a relative position of each target aircraft to the host aircraft;

program instructions for determining if any target aircraft is on a collision course with the host aircraft;

program instructions for providing a warning alert to the host aircraft if any target aircraft is on a collision course with the host aircraft; and

program instructions for automatically providing a course deviation for the host aircraft to avoid collision.

28. The computer program product for generating an airborne network for collision avoidance of claim 25 wherein the Cartesian coordinate system comprises the Earth-centered Earth-Fixed (ECEF) coordinate system.

29. The computer program product for generating an airborne network for collision avoidance of claim 25 further comprising program instructions for determining if any target aircraft projected location will approach within a proximity threshold value of the host aircraft location.

30. The computer program product for generating an airborne network for collision avoidance of claim 29 further comprising program instructions for providing a caution alert to the host aircraft if any target aircraft projected location will approach within a proximity threshold value of the host aircraft location.

31. The computer program product for generating an airborne network for collision avoidance of claim 25 wherein the warning alert comprises a flashing target symbol and an audio warbling tone.

32. The computer program product for generating an airborne network for collision avoidance of claim 30 wherein the caution alert comprises a flashing target symbol and an audio warbling tone.

33. The computer program product for generating an airborne network for collision avoidance of claim 25 wherein the program instructions for displaying a relative position of each target aircraft to the host aircraft comprise:

program instructions for determining a down range, cross range and altitude differentials between the host aircraft and each target aircraft;

program instructions for determining a relative position of each target aircraft from the host aircraft based upon the down range, cross range and altitude differentials between the host aircraft and each target aircraft; and

program instructions for plotting the relative position of each target aircraft on a multi-dimensional display.

34. The computer program product for generating an airborne network for collision avoidance of claim 33 wherein the program instructions for displaying a relative position of each target aircraft to the host aircraft further comprises program instructions for plotting at least one target aircraft as a vector wherein the vector represents heading and speed of the at least one target aircraft.

35. The computer program product for generating an airborne network for collision avoidance of claim 25 wherein the program instructions for automatically providing a course deviation for the host aircraft to avoid collision with a target aircraft comprise:

program instructions for determining if an automatic reaction function is set on the host aircraft;

program instructions for determining if an autopilot on the host aircraft is coupled to an airborne collision avoidance system;

program instructions for setting a remaining time to initiate a course correction;

program instructions for determining a course deviation for the host aircraft relative to the current heading; and

program instructions for generating a steering command sequence to change the host aircraft'"'"'s heading based on the determined course deviation.

36. The computer program product for generating an airborne network for collision avoidance of claim 35 wherein the program instructions for automatically providing a course deviation for the host aircraft to avoid collision with a target aircraft further comprise:

program instructions for determining if a collision course conflict with the target aircraft has cleared; and

program instructions for generating a steering command sequence to change the host aircraft'"'"'s heading to an intended course.