Apparatus for determining the position of an aircraft with respect to the runway

• US 4,316,252 A
• Filed: 08/10/1979
• Issued: 02/16/1982
• Est. Priority Date: 08/10/1979
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Cooper, Michael G.
• Primary Examiner(s): Gruber, Felix D.
• Application Number:
  US06/065,404
• Time in Patent Office: 921 Days
• Field of Search: 364/426, 364/428, 364/430, 364/433, 364/443, 340/27 NA, 244/183, 244/184, 244/186
• US Class Current: 701/16
• CPC Class Codes: G05D 1/0083 to help an aircraft pilot in the rolling phase

Abstract

Upon landing approach to a runway, glideslope and altitude information is processed to produce an indication of ground distance to the touchdown point. Actual aircraft position is then determined by integrating the aircraft'"'"'s ground speed. A display of distance from the beginning and end of the runway is provided. An alert is produced if the aircraft approaches the end of the runway at excessive speed. Further, the system may be coupled to the aircraft'"'"'s autobrake system to automatically control the rate of deceleration.

Claims

1. Apparatus for determining the position of an airplane, having a groundspeed indicator, with respect to a runway comprising:

means for determining the glidescope angle φ

of the plane with respect to the runway;

means for determining that the plane is a specified altitude A above the runway on said glideslope;

processing means including means for;

calculating the ground distance d of the airplane from the intersection of the glideslope with the runway from the equation d=A/tan φ

;

calculating the ground distance S_o of the airplane from the beginning of the runway during the instance of the airplane being at the altitude A from the equation S_o =d-D, where D is the predetermined distance from the beginning of the runway to the intersection of the glideslope with the runway;

integrating airplane ground speed to produce an indication of airplane relative position; and

updating said distance S_o by said relative position to produce a continuous indication S of the distance of the airplane from the beginning of the runway.

2. The apparatus of claim 1, wherein the runway has a predetermined length L, wherein the processing means further includes means for calculating the distance R of the airplane from the end of the runway from the equation R=L-S.

3. The apparatus of either of claims 1 or 2 wherein the airplane has a desired deceleration factor defining the optimum instantaneous ground speed of the airplane as a function of position on the runway, the apparatus further comprising:

braking means responsive to a control signal to affect braking of the airplane, and

the processing means further includes means for monitoring airplane position and instantaneous ground speed, comparing these values with the desired values and generating and applying a control signal to said braking means causing said braking means to correct airplane deceleration to said desired factor.

4. The apparatus of claim 3 further comprising:

alerting means for monitoring airplane ground speed, decelerating factor and the distance R and producing an alert signal if the instantaneous values of said monitored parameters indicates that without additional braking the airplane'"'"'s speed at the end of the runway would be excessive.

5. A method for determining the position of an airplane, having a groundspeed indicator, with respect to a runway comprising the steps of:

determining the glideslope angle φ

of the plane with respect to the runway;

determining that the plane is a specified altitude A above the runway on said glideslope;

calculating the ground distance d of the airplane from the intersection of the glideslope with the runway from the equation d=A/tan φ

;

calculating the ground distance S_o of the airplane from the beginning of the runway during the instance of the airplane being at the altitude A from the equation S_o =d-D, where D is the predetermined distance from the beginning of the runway to the intersection of the glideslope with the runway;

integrating airplane ground speed to produce an indication of airplane relative position; and

updating said distance S_o by said relative position to produce a continuous indication S of the distance of the airplane from the beginning of the runway.

6. The method of claim 5 wherein the runway has a predetermined length L, comprising the further step of:

calculating the distance R of the airplane from the end of the runway from the equation R=L-S.

7. The method of either of claims 5 or 6 wherein the airplane has a desired deceleration factor defining the optimum instantaneous ground speed of the airplane as a function of position on the runway, the method comprising the further steps of:

providing braking means responsive to a control signal to affect braking of the airplane; and

monitoring airplane position and instantaneous ground speed, comparing these values with the desired values and generating and applying a control signal to said braking means causing said braking means to correct airplane deceleration to said desired factor.

8. The method of claim 7 comprising the further step of:

monitoring airplane ground speed, decelerating factor and the distance R and producing an alert signal if the instantaneous values of said monitored parameters indicates that without additional braking the airplane'"'"'s speed at the end of the runway would be excessive.