System and method for assisting the prevention of controlled flight into terrain accidents

• US 6,122,570 A
• Filed: 06/19/1998
• Issued: 09/19/2000
• Est. Priority Date: 07/31/1995
• Status: Expired due to Term

• Current Assignee: Alliedsignal Inc.
• Original Assignee: Alliedsignal Inc.
• Inventors: Johnson, Steven C., Conner, Kevin J., Muller, Hans R.
• Primary Examiner(s): Cuchlinski, Jr., William A.
• Assistant Examiner(s): PIPALA, EDWARD J
• Application Number:
  US09/099,822
• Time in Patent Office: 823 Days
• Field of Search: 701/4, 701/5, 701/6, 701/7, 701/8, 701/9, 701/120, 701/300, 701/301, 701/302, 340/945, 340/963, 340/970, 340/977, 244/180, 244/181, 73/178 R, 73/178 T
• US Class Current: 701/9
• CPC Class Codes: G01C 5/005 altimeters for aircraft G01C5/02, G01C5/06 take precedence
• CPC Class Codes: G05D 1/0676 specially adapted for landing

Abstract

A terrain awareness system (TAS) provides LOOK-AHEAD/LOOK-DOWN as well as LOOK-UP terrain advisory and warning indications to the pilot of an aircraft of a hazardous flight condition. The TAS includes an airport data base as well as a terrain data base that is structured to provide various resolutions depending on the topography of the particular geographic area of interest. Navigational data from a satellite-based navigational system, such as a global positioning system (GPS), is used to provide a LOOK-AHEAD/LOOK-DOWN and LOOK-UP terrain advisory and terrain warning indications based upon the current position and projected flight path of the aircraft. Since the terrain advisory and the warning signals are a function of the flight path of the aircraft, nuisance warnings are minimized.

Claims

1. A system for assisting in the prevention of controlled flight into terrain accidents comprising:

(a) a database of stored terrain information;

(b) a signal processing device, coupled to receive signals representative of a position of the aircraft, a flight path of an aircraft and a speed of the aircraft, and coupled to said database, for;

(i) defining a look ahead distance as a function of the speed of the aircraft;

(ii) defining a first alert envelope, indicative of a first severity of terrain threat, wherein boundaries of said first alert envelope are determined as a first function of the flight path angle, said look ahead distance, and a terrain floor boundary;

(iii) defining a second alert envelope, indicative of a second severity of terrain threat, wherein boundaries of said second alert envelope are determined as a second function of the flight path angle, said look ahead distance and said terrain floor boundary; and

(iv) outputting an alert signal when a subset of the stored terrain information is located with in the boundaries of at least one of said first and said second alert envelopes; and

(c) a display, coupled to receive a subset of said terrain information, for displaying terrain in a vicinity of the aircraft.

2. The system of claim 1 wherein said display comprises an EFIS display.

3. The system of claim 1 wherein said display comprises a weather radar display.

4. The system of claim 1 wherein said display comprises a flight management system (FMS) display.

5. The system of claim 1 wherein said signal processing device comprises a microprocessor.

6. A system for assisting in the prevention of controlled flight into terrain accidents comprising:

(a) a database of stored terrain information;

(b) a signal processing device, coupled to receive signals representative of a position of the aircraft;

a flight path of an aircraft and a speed of the aircraft, and coupled to said database for;

(i) defining a look ahead distance as a function of the speed of the aircraft;

(ii) defining a first alert envelope, indicative of a first severity of terrain threat, wherein boundaries of said first alert envelope are determined as a first function of the flight path angle, said look ahead distance, and a terrain floor boundary;

(iii) defining a second alert envelope, indicative of a second severity of terrain threat, wherein boundaries of said second alert envelope are determined as a second function of the flight path angle, said look ahead distance and said terrain floor boundary;

(c) a display, coupled to said signal processing device for displaying at least a subset of said stored terrain information located within the boundaries of at least one of said first and said second alert envelopes.

7. The system of claim 6 wherein said display comprises an EFIS display.

8. The system of claim 6 wherein said display comprises a weather radar display.

9. The system of claim 6 wherein said display comprises a flight management system (FMS) display.

10. The system of claim 6 wherein said signal processing device comprises a microprocessor.

11. The system of claim 6 wherein said display depicts said subset of terrain using a plurality of colors, each one of said colors representative of a different severity of terrain threat.

12. The system of claim 6 wherein said display depicts said subset of terrain using a variable density dot pattern and wherein said density varies as a function of a severity of terrain threat.

13. The system of claim 6 wherein said display depicts said subset of terrain using a variable density dot pattern that varies as a function of the aircraft altitude relative to said terrain.

14. A method for assisting in the prevention of controlled flight into terrain accidents comprising the steps of:

receiveing signals representative of a position of an aircraft, a flight path of the aircraft and a speed of the aircraft, and terrain data;

defining a look ahead distance as a function of the speed of the aircraft;

defining a first alert envelope, indicative of a first severity of terrain threat, wherein boundaries of said first alert envelope are determined as a first function of the flight path angle, said look ahead distance, and a terrain floor boundary;

defining a second alert envelope, indicative of a second severity of terrain threat, wherein boundaries of said second alert envelope are determined as a second function of the flight path angle, said look ahead distance and said terrain floor boundary;

outputting an alert signal when a subset of the stored terrain information is located with in the boundaries of at least one of said first and said second alert envelopes; and

displaying at least a portion of said terrain data.

15. A method for assisting in the prevention of controlled flight into terrain accidents compromising the steps of:

receiveing signals representative of a position of an aircraft;

a flight path of the aircraft and a speed of the aircraft, and terrain data;

defining a look ahead distance as a function of the speed of the aircraft;

defining a first alert envelope, indicative of a first severity of terrain threat, wherein boundaries of said first alert envelope are determined as a first function of the flight path angle, said look ahead distance, and a terrain floor boundary;

defining a second alert envelope, indicative of a second severity of terrain threat, wherein boundaries of said second alert envelope are determined as a second function of the flight path angle, said look ahead distance and said terrain floor boundary; and

displaying at least a subset of said stored terrain information located within the boundaries of at least one of said first and said second alert envelopes.

16. The method of claim 15 wherein said step of displaying further comprises the step of using a plurality of colors, each one of said colors representative of a different severity of terrain threat.

17. The method of claim 15 wherein said step of displaying further comprises the step of depicting said subset of terrain using a variable density dot pattern and wherein said density varies as a function of a severity of terrain threat.

18. The method of claim 15 wherein said step of displaying further comprises the step of depicting said subset of terrain using a variable density dot pattern that varies as a function of the aircraft altitude relative to said terrain.