Ground proximity warning system and method having a reduced set of input parameters

• US 6,785,594 B1
• Filed: 03/24/2000
• Issued: 08/31/2004
• Est. Priority Date: 03/25/1999
• Status: Expired due to Term

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Johnson, Steven C., Bateman, C. Don
• Primary Examiner(s): Nguyen, Tan Q.
• Assistant Examiner(s): Tran, Dalena
• Application Number:
  US09/534,222
• Time in Patent Office: 1,621 Days
• Field of Search: 701/9, 701/4, 701/14, 701/206, 701/301, 340/970, 340/945, 340/963, 340/967, 340/969, 340/977, 731/78.R, 731/78.T, 342/65
• US Class Current: 701/9
• 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 5/005 altimeters for aircraft G01C5/02, G01C5/06 take precedence
• CPC Class Codes: G01S 19/15 Aircraft landing systems
• CPC Class Codes: G01S 19/39 the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
• CPC Class Codes: G01S 19/45 by combining measurements of signals from the satellite radio beacon positioning system with a supplementary measurement
• CPC Class Codes: G08G 5/0086 for monitoring terrain radar or analogous systems specially adapted for terrain avoidance G01S13/935

Abstract

The ground proximity warning system and method provide a number of alerts based upon a substantially reduced list of input parameters relative to a conventional ground proximity warning system and method. The ground proximity warning system and method generally constructs alert envelopes and generates alerts if the upcoming terrain or other obstacles pierce the alert envelopes. The ground proximity warning system and method can also generate alerts if the aircraft has an excessive descent rate at a relatively low altitude and if the aircraft descends immediately following takeoff in a similar fashion to Mode 1 and Mode 3 alerts. Further, the ground proximity warning system and method can provide altitude call outs at predefined altitudes above a target runway and can provide alerts if the aircraft appears to be landing short of a runway. The ground proximity warning system and method are capable of providing the various warnings based upon only a pressure altitude, GPS signals and, in some embodiments, the external air temperature. Thus, the ground proximity warning system and method can be independent of a radio altimeter, an ADC, a glideslope receiver and signals indicative of the configuration of the landing gear and flaps.

Claims

1. A ground proximity warning system comprising:

a processor, responsive to a global position system (GPS) receiver, for determining a positional relationship between an aircraft and upcoming terrain;

a warning mechanism, responsive to said processor, for providing an alert if said processor determines that the positional relationship between the aircraft and the upcoming terrain fails to meet an alert criteria; and

a memory device for storing a terrain database defining the elevational data for the upcoming terrain, wherein said processor determines a geometric altitude of the aircraft and a difference between the geometric altitude and an elevation of local terrain, and wherein said warning mechanism provides an alert if the difference between the geometric altitude and the elevation of the local terrain is less than a predetermined altitude;

wherein said processor is capable of determining the positional relationship between the aircraft and the upcoming terrain based only upon a pressure altitude, signals provided by the GPS receiver and elevational data associated with the upcoming terrain.

2. A ground proximity warning system according to claim 1 wherein said processor is capable of determining the positional relationship between the aircraft and the upcoming terrain in a manner independent of at least one signal selected from the group consisting of signals indicative of radio altitude, indicated airspeed, roll angle, respective positions of landing gear and flaps and a glideslope.

3. A ground proximity warning system according to claim 2 wherein said processor is capable of determining the positional relationship between the aircraft and the upcoming terrain in a manner independent of each of the signals indicative of radio altitude, indicated airspeed, roll angle, respective positions of landing gear and flaps and the glideslope.

4. A ground proximity warning system according to claim 1 wherein said processor defines the alert criteria at least partially based upon data associated with a runway.

5. A ground proximity warning system according to claim 1 wherein said processor is also capable of determining a positional relationship between the aircraft and a runway based only upon the pressure altitude, signals provided by the GPS receiver and data associated with the runway, and wherein said warning mechanism is also capable of providing an alert if said processor determines that the positional relationship between the aircraft and the runway fails to meet a predetermined criteria.

6. A ground proximity warning system according to claim 1 further comprising a memory device for storing a terrain database defining the elevational data for the upcoming terrain, wherein said processor constructs a warning envelope extending in advance of the aircraft and compares the warning envelope to the upcoming terrain based on the elevational data associated with the upcoming terrain, and wherein said warning mechanism provides a warning alert if said processor determines that the upcoming terrain will pierce the warning envelope.

7. A ground proximity warning system according to claim 6 wherein said processor further constructs a caution envelope extending further in advance of the aircraft than the warning envelope and compares the caution envelope to the upcoming terrain based on the elevational data associated with the upcoming terrain, and wherein said warning mechanism provides a cautionary alert if said processor determines that the upcoming terrain will pierce the caution envelope.

8. A ground proximity warning system according to claim 1 wherein said processor is also responsive to a temperature probe such that said processor is capable of determining the positional relationship between the aircraft and the upcoming terrain based upon a temperature in addition to the pressure altitude, the signals provided by the GPS receiver and elevational data associated with the upcoming terrain.

9. A ground proximity warning system according to claim 1 wherein said processor is responsive to at least one GPS signal selected from the group consisting of GPS signals indicative of a latitude, longitude, ground speed, ground track, GPS altitude and a quality parameter.

10. A method for providing ground proximity warnings comprising:

determining a positional relationship between an aircraft and upcoming terrain, wherein the positional relationship is capable of being determined based only upon a pressure altitude, signals provided by a global position system (GPS) receiver and elevational data associated with the upcoming terrain;

providing an alert if the positional relationship between the aircraft and the upcoming terrain fails to meet an alert criteria;

accessing a terrain database defining the elevational data for the upcoming terrain,

wherein said determining step comprises determining a geometric altitude of the aircraft and a difference between the geometric altitude and an elevation of local terrain, and wherein said providing step comprises providing an alert if the difference between the geometric altitude and the elevation of the local terrain is less than a predetermined altitude.

11. A method according to claim 10 wherein said determining step comprises determining the positional relationship between the aircraft and the upcoming terrain in a manner independent of at least one signal selected from the group consisting of signals indicative of radio altitude, indicated airspeed, roll angle, respective positions of landing gear and flaps and a glideslope.

12. A method according to claim 11 wherein said determining step comprises determining the positional relationship between the aircraft and the upcoming terrain in a manner independent of each of the signals indicative of radio altitude, indicated airspeed, roll angle, respective positions of landing gear and flaps and the glideslope.

13. A method according to claim 10 further comprising determining the alert criteria at least partially based upon data associated with a runway.

14. A method according to claim 10 further comprising:

determining a positional relationship between an aircraft and a runway based only upon the pressure altitude, signals provided by a global position system (GPS) receiver and data associated with the runway; and

providing an alert if the positional relationship between the aircraft and the runway fails to meet a predetermined criteria.

15. A method according to claim 10 further comprising accessing a terrain database defining the elevational data for the upcoming terrain, wherein said determining step comprises constructing a warning envelope extending in advance of the aircraft and comparing the warning envelope to the upcoming terrain based on the elevational data associated with the upcoming terrain, and wherein said providing step comprises providing a warning alert if the upcoming terrain will pierce the warning envelope.

16. A method according to claim 15 wherein said determining step further comprises constructing a caution envelope extending further in advance of the aircraft than the warning envelope and comparing the caution envelope to the upcoming terrain based on the elevational data associated with the upcoming terrain, and wherein said providing step further comprises providing a cautionary alert if the upcoming terrain will pierce the caution envelope.

17. A method according to claim 10 wherein said determining step comprises determining the positional relationship between the aircraft and the upcoming terrain based upon a temperature in addition to the pressure altitude, the signals provided by the GPS receiver and elevational data associated with the upcoming terrain.

18. A ground proximity warning system providing Mode 1, Mode 3 and Mode 6 alert modes comprising:

a processor, responsive to a global position system (GPS) receiver, for determining a positional relationship between an aircraft and upcoming terrain and for selecting one of the alert modes; and

a warning mechanism, responsive to said processor, for providing an alert if said processor determines that the positional relationship between the aircraft and the upcoming terrain fails to meet an alert criteria associated with said selected alert mode, wherein said processor determines the positional relationship and selects the alert mode in a manner independent of signals indicative of radio altitude, respective positions of landing gear and flaps and a glideslope.

19. A ground proximity warning system according to claim 18 wherein said processor defines the alert criteria at least partially based upon data associated with a runway.

20. A ground proximity warning system according to claim 18 wherein said processor is capable of determining the positional relationship between the aircraft and the upcoming terrain in a manner that is also independent of signals indicative of indicated airspeed and roll angle.

21. A ground proximity warning system according to claim 18 wherein said processor is capable of determining the positional relationship between the aircraft and the upcoming terrain based only upon a pressure altitude, signals provided by the GPS receiver and elevational data associated with the upcoming terrain.

22. A ground proximity warning system according to claim 21 wherein said processor is also capable of determining the positional relationship between the aircraft and a runway based only upon the pressure altitude, signals provided by the GPS receiver and data associated with the runway, and wherein said warning mechanism is also capable of providing an alert if said processor determines that the positional relationship between the aircraft and the runway fails to meet a predetermined criteria.

23. A ground proximity warning system according to claim 21 wherein said processor is also responsive to a temperature probe such that said processor is capable of determining the positional relationship between the aircraft and the upcoming terrain based upon a temperature in addition to the pressure altitude, the signals provided by the GPS receiver and the elevational data associated with the upcoming terrain.

24. A ground proximity warning system according to claim 18 further comprising a memory device for storing a terrain database defining the elevational data for the upcoming terrain, wherein said processor constructs a warning envelope extending in advance of the aircraft and compares the warning envelope to the upcoming terrain based on the elevational data associated with the upcoming terrain, and wherein said warning mechanism provides a warning alert if said processor determines that the upcoming terrain will pierce the warning envelope.

25. A ground proximity warning system according to claim 24 wherein said processor further constructs a caution envelope extending further in advance of the aircraft than the warning envelope and compares the caution envelope to the upcoming terrain based on the elevational data associated with the upcoming terrain, and wherein said warning mechanism provides a cautionary alert if said processor determines that the upcoming terrain will pierce the caution envelope.

26. A ground proximity warning system according to claim 18 further comprising a memory device for storing a terrain database defining the elevational data for the upcoming terrain, wherein said processor determines a geometric altitude of the aircraft and a difference between the geometric altitude and an elevation of local terrain, and wherein said warning mechanism provides an alert if the difference between the geometric altitude and the elevation of the local terrain is less than a predetermined altitude.

27. A ground proximity warning system according to claim 18 wherein said processor is responsive to at least one GPS signal selected from the group consisting of GPS signals indicative of a latitude, longitude, ground speed, ground track, GPS altitude and a quality parameter.

28. A method for providing ground proximity warnings for Mode 1, Mode 3 and Mode 6 alert modes comprising:

determining a positional relationship between an aircraft and upcoming terrain based upon signals from a global position system (GPS) receiver and independent of signals indicative of radio altitude, respective positions of landing gear and flaps and a glideslope;

selecting one of the alert modes based upon signals from a global position system (GPS) receiver and independent of signals indicative of radio altitude, respective positions of landing gear and flaps and a glideslope; and

providing an alert if the positional relationship between the aircraft and the upcoming terrain fails to meet an alert criteria associated with said selected alert mode.

29. A method according to claim 28 further comprising determining the alert criteria at least partially based upon data associated with a runway.

30. A method according to claim 28 wherein said determining step comprises determining the positional relationship between the aircraft and the upcoming terrain in a manner that is also independent of signals indicative of indicated airspeed and roll angle.

31. A method according to claim 28 wherein said determining step comprises determining the positional relationship between the aircraft and the upcoming terrain based only upon a pressure altitude, signals provided by the GPS receiver and elevational data associated with the upcoming terrain.

32. A method according to claim 31 further comprising:

determining a positional relationship between the aircraft and a runway based only upon the pressure altitude, signals provided by the GPS receiver and data associated with the runway; and

providing an alert if the positional relationship between the aircraft and the runway fails to meet a predetermined criteria.

33. A method according to claim 31 wherein said determining step further comprises determining the positional relationship between the aircraft and the upcoming terrain based upon a temperature in addition to the pressure altitude, the signals provided by the GPS receiver and the elevational data associated with the upcoming terrain.

34. A method according to claim 28 further comprising accessing a terrain database defining elevational data for the upcoming terrain, wherein said determining step comprises constructing a warning envelope extending in advance of the aircraft and comparing the warning envelope to the upcoming terrain based on the elevational data associated with the upcoming terrain, and wherein said providing step comprises providing a warning alert if the upcoming terrain will pierce the warning envelope.

35. A method according to claim 34 wherein said determining step further comprises constructing a caution envelope extending further in advance of the aircraft than the warning envelope and comparing the caution envelope to the upcoming terrain based on the elevational data associated with the upcoming terrain, and wherein said providing step further comprises providing a cautionary alert if the upcoming terrain will pierce the caution envelope.

36. A method according to claim 28 further comprising accessing a terrain database defining elevational data for the upcoming terrain, wherein said determining step comprises determining a geometric altitude of the aircraft and a difference between the geometric altitude and an elevation of local terrain, and wherein said providing step comprises providing an alert if the difference between the geometric altitude and the elevation of the local terrain is less than a predetermined altitude.