Terrain awareness system having nuisance alarm filter for use during approach

• US 6,567,728 B1
• Filed: 08/08/2001
• Issued: 05/20/2003
• Est. Priority Date: 08/08/2001
• Status: Expired due to Term

• Current Assignee: Rockwell Collins, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Rockwell Collins, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Uckun, Serdar, Kelly, Wallace E.
• Primary Examiner(s): NGUYEN, TAN QUANG
• Application Number:
  US09/924,821
• Time in Patent Office: 650 Days
• Field of Search: 701/9, 701/8, 701/16, 701/17, 340/947, 340/948, 340/951, 340/954, 340/960, 340/961, 340/976, 340/979
• US Class Current: 701/9
• CPC Class Codes: G01C 5/005 altimeters for aircraft G01C5/02, G01C5/06 take precedence
• CPC Class Codes: G08G 5/0086 for monitoring terrain radar or analogous systems specially adapted for terrain avoidance G01S13/935
• CPC Class Codes: G08G 5/025 Navigation or guidance aids radar or analogous systems specially adapted for landing purposes G01S13/913

Abstract

An approach suppressed TAWS system and method for suppressing nuisance alarms based upon a determination that an aircraft is properly aligned for landing based upon location within a safe zone defined by a glideslope component and a localizer component.

Claims

1. An apparatus for assisting in reducing nuisance ground proximity warning systems alerts, the apparatus comprising:

a ground proximity warning system which is adapted and configured to provide warnings to a pilot of possible controlled flight into terrain situations; and

,

a first algorithm, adapted and configured to cooperate with said ground proximity warning system, said first algorithm adapted and configured to make a determination that the aircraft is in a safe zone having a localizer component and a glideslope component which define a safe zone centrally disposed around a safe zone axis extending in a plane containing an airport runway.

2. An apparatus of claim 1 wherein:

said determination utilizes a predetermined safe zone and a positioning system to provide current position of the aircraft.

3. An apparatus of claim 1 wherein an instrument landing system receiver is coupled to said ground proximity warning system and provides information used to determine whether the aircraft is in said safe zone.

4. An apparatus of claim 3 further comprising:

a second algorithm, adapted and configured to cooperate with said ground proximity warning system, said second algorithm makes a safe heading determination of a plurality of safe headings for said aircraft; and

a display which is responsive to said safe heading determination and provides a visual indication of safe headings to a pilot.

5. An apparatus of claim 4 wherein said first algorithm and said second algorithm are executed by said ground proximity warning system.

6. An apparatus of claim 5 wherein said first algorithm and said second algorithm are portions of an algorithm used by said ground proximity warning system to provide warnings based upon current heading and current vertical speed.

7. A method of reducing nuisance terrain warning alerts, comprising the steps of:

providing a ground proximity warning system which utilizes a positioning system and a terrain database;

making a determination of a location of an aircraft within a safe zone which is defined by a glideslope component and a localizer component; and

,

suppressing an alert from said ground proximity warning system in response to said determination of location.

8. A method of claim 7 wherein said step of making a determination of a location utilizes an instrument landing system receiver.

9. A method of claim 8 further comprising the step of displaying to a pilot safe headings.

10. A method of claim 9 further comprising the step of making a determination of safe negative vertical speeds.

11. A method of claim 10 further comprising the step of displaying a plurality safe negative vertical speeds.

12. A method of claim 11 wherein said safe negative vertical speeds are displayed as a colored line disposed adjacent to a vertical speed.

13. A method of claim 7 wherein said step of making a determination of location utilizes a predetermined safe zone.

14. A system comprising:

a ground proximity warning system which is adapted and configured to generate warnings based upon current speed, current heading and current location of a protected aircraft; and

,

means for suppressing a warning from said ground proximity warning system in response to a determination that an aircraft is disposed within a safe zone defined by a glideslope component and a localizer component.

15. A system of claim 14 wherein said means for suppressing is responsive to an instrument landing system receiver.

16. A system of claim 15 further comprising means for notifying a pilot of safe heading and descent rates.

17. A system of claim 16 wherein said means for notifying is a display providing information relating to safe headings of said protected aircraft, wherein said safe headings are depicted as bars disposed about a compass rose.

18. A system of claim 14 wherein said means for suppressing utilizes a comparison of current position of the aircraft to a predetermined safe zone.