IP Library Granted Patent US 7,068,187
Granted Patent B2
US 7,068,187 · App. 09/775,455 · Granted Jun 27, 2006

Method, apparatus and computer program product for unstabilized approach alerting

Assignee: Honeywell International Inc.
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Quick Facts
Patent No.
US 7,068,187
App. No.
09/775,455
Granted
Jun 27, 2006
Kind
B2
Abstract

A method, apparatus and computer program product for assisting the pilot of an aircraft in making a go-around decision. Various aircraft parameters are monitored during the approach to land and a risk level assessed. When the risk level exceeds a specified threshold, an alert is provided.

Claims (26)

1. A method for alerting the pilot of an aircraft to a potential go-around condition comprising the steps of:

monitoring a plurality of parameters indicative of an unstabilized approach;

assigning a risk of go-around value to each of said parameters;

summing the assigned risk values; and

asserting an alert signal when said summation exceeds a predetermined threshold amount, asserting further comprises:

asserting a go-around caution alert signal when said value exceeds a first threshold amount and is less than a second threshold amount; and

asserting a go-around warning signal when said value exceeds said second threshold amount.

2. The method of claim 1 wherein said step of monitoring a plurality of parameters includes the step of monitoring a change in a speed of the aircraft.

3. The method of claim 1 wherein said step of monitoring a plurality of parameters includes the step of monitoring a runway wind condition.

4. The method of claim 1 wherein said step of monitoring a plurality of parameters includes the step of monitoring a flight path angle of the aircraft.

5. The method of claim 1 wherein said step of monitoring a plurality of parameters includes the step of monitoring a position of the aircraft.

6. The method of claim 1 wherein said step of monitoring a plurality of parameters includes the step of monitoring a track of the aircraft.

7. The method of claim 1 wherein said step of asserting an alert signal comprises the step of commanding an autopilot go-around maneuver.

8. A method of alerting the pilot of an aircraft to a potential go-around condition comprising the steps of:

monitoring a plurality of parameters indicative of a runway landing length required;

assigning a risk of runway overrun value for each of said plurality of parameters;

summing the assigned risk values; and

asserting an alert signal when said summation exceeds a predetermined threshold value,

wherein the plurality of parameters include runway length,

wherein said step of asserting an alert signal further comprises the steps of:

asserting a go-around caution alert signal when said value exceeds a first threshold amount and is less than a second threshold amount; and

asserting a go-around warning signal when said value exceeds said second threshold amount.

9. The method of claim 8 wherein said step of monitoring a plurality of parameters includes the step of monitoring a deceleration required to stop the aircraft.

10. The method of claim 8 wherein said step of monitoring a plurality of parameters includes the step of monitoring a runway surface condition.

11. The method of claim 8 wherein said step of monitoring a plurality of parameters includes the step of monitoring at least one atmospheric condition.

12. The method of claim 8 wherein said step of asserting an alert signal comprises the step of commanding an autopilot go-around maneuver.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 9, 2001
From: ISHIHARA, YASUO; GREMMERT, SCOTT; JOHNSON, STEVEN C.
To: HONEYWELL INTERNATIONAL INC.
Reel/Frame 011702/0760 →
Continuity (2)
Provisional Application 6017993800 · Feb 3, 2000
Related Publication 20010052562A1 · Dec 20, 2001