Warning system having low intensity wind shear enhancements

• US 5,153,588 A
• Filed: 10/16/1990
• Issued: 10/06/1992
• Est. Priority Date: 08/29/1985
• Status: Expired due to Term

• Current Assignee: Alliedsignal Inc.
• Original Assignee: Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Muller, Hans R.
• Primary Examiner(s): Ng, Jin F.
• Assistant Examiner(s): SWARTHOUT, BRENT
• Application Number:
  US07/598,140
• Time in Patent Office: 721 Days
• Field of Search: 340/963, 340/967, 340/974, 340/976, 340/970, 340/968, 73/178 T, 364/433
• US Class Current: 340/968
• CPC Class Codes: G01C 5/005 altimeters for aircraft G01C5/02, G01C5/06 take precedence
• CPC Class Codes: G01C 5/06 by using barometric means
• CPC Class Codes: G01S 13/933 of aircraft or spacecraft
• CPC Class Codes: G05D 1/0615 to counteract a perturbation, e.g. gust of wind

Abstract

A ground proximity warning system for aircraft having flight path angle based warning criteria generates a warning in the event of an excessively steep flight path angle during an approach to a landing. The warning criteria are altered to provide an earlier warning upon the occurrence of a low intensity wind shear or a below glideslope condition. A below glideslope warning system that is biased as a function of decreasing performance shear is also provided. A descent rate based warning system usable above a predetermined altitude may also be provided to supplement the flight path angle warning system.

Claims

1. A ground proximity warning system for warning the pilot of an aircraft of a dangerous flight condition during an approach to a landing, comprising:

means for providing a signal representative of the flight path angle of the aircraft;

means for providing a signal representative of the altitude above ground of the aircraft;

means responsive to said flight path angle and altitude above ground representative signals for generating the warning according to a predetermined set of criteria if the flight path angle is too steep for the altitude above ground at which the aircraft is flying;

first means for detecting a wind shear condition;

second means responsive to said first detecting means for detecting a decreasing performance wind shear condition; and

means responsive to the first and second detecting means for altering said predetermined set of criteria to cause said warning to be generated at less steep flight path angles in the presence of decreasing performance wind shear.

2. A ground proximity warning system as recited in claim 1, wherein said altering means is responsive to a decreasing performance wind shear for altering said predetermined set of criteria.

3. A ground proximity warning system as recited in claim 1 further including:

means for receiving a glideslope signal and providing a glideslope deviation signal representative of the deviation of the aircraft from the glideslope; and

means responsive to the glideslope deviation signal for altering said predetermined set of criteria to cause said warning to be generated at less steep flight path angles in the presence of a below the glideslope condition.

4. A ground proximity warning system as recited in claim 1 further including:

means for receiving a signal representative of the vertical velocity of the aircraft;

means for receiving a signal representative of the horizontal velocity of the aircraft;

means for receiving a signal representative of the altitude above ground of the aircraft; and

means responsive to said vertical and horizontal velocity representative signals for generating said signal representative of the flight path angle of the aircraft.

5. A ground proximity warning system for warning the pilot of an aircraft of a dangerous flight condition during an approach to a landing, comprising:

means for providing a signal representative of the flight path angle of the aircraft;

means for providing a signal representative of the altitude above ground of the aircraft;

means responsive to said flight path angle and altitude above ground representative signals for generating a warning according to a predetermined set of criteria if the flight path angle is too steep for the altitude above ground at which the aircraft is flying;

means for receiving a glide slope signal and providing a glide slope deviation signal representative of the deviation of the aircraft from the glide slope; and

means responsive to the glide slope deviation signal for altering said predetermined set of criteria to cause said warning to be generated at less steep flight path angles in the presence of a below the glide slope condition.

6. A ground proximity warning system as recited in claim 5 further including:

means for receiving a signal representative of the vertical velocity of the aircraft;

means for receiving a signal representative of the horizontal velocity of the aircraft;

means for receiving a signal representative of the altitude above ground of the aircraft; and

means responsive to said vertical and horizontal velocity representative signals for generating said signal representative of the flight path angle of the aircraft.

7. A ground proximity warning system for warning the pilot of an aircraft of a dangerous flight condition during an approach to a landing, comprising:

means for receiving a signal representative of the vertical velocity of the aircraft;

means for receiving a signal representative of the horizontal velocity of the aircraft;

means for receiving a signal representative of the altitude above ground of the aircraft;

means responsive to said vertical and horizontal velocity representative signals for generating a signal representative of the flight path angle of the aircraft;

means operative above a predetermined altitude and responsive to said vertical velocity and altitude above ground representative signals for generating a warning according to a predetermined set of criteria if the vertical velocity is excessive in a negative direction for the altitude at which the aircraft is flying; and

means operative below said predetermined altitude and responsive to said flight path angle representative signal and said altitude above ground signal for generating a warning according to a second predetermined set of criteria if the flight path angle is too steep for the altitude at which the aircraft is flying.

8. A ground proximity warning system as recited in claim 7 further including:

means for receiving a glideslope signal and providing a glideslope deviation signal representative of the deviation of the aircraft from the glideslope; and

means responsive to the glideslope deviation signal for altering said second predetermined set of criteria to cause said warning to be generated at less steep flight path angles in the presence of a below the glideslope condition.

9. A ground proximity warning system as recited in claim 7 further including:

first means for providing a wind shear signal representative of wind shear;

second means responsive to said first detecting means for detecting a decreasing performance wind shear condition; and

means responsive to the wind shear signal for altering said second predetermined set of criteria to cause said warning to be generated at less steep flight path angles in the presence of a wind shear condition.

10. A ground proximity warning system as recited in claim 9, wherein said wind shear responsive means is responsive to a decreasing performance wind shear for altering said second predetermined set of criteria.