US4316252A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Apparatus for determining the position of an aircraft with respect to the runway
Assignee: Boeing Co
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Filing: 1979-08-10
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Granted: 1982-02-16
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Expires: 1999-08-10
Abstract
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.
Inventors
- 👤 Michael G. Cooper
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-02 01:51
CPC Classifications
G; G05; G05D; G05D1/00; G05D1/0083
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
170 words
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.
Claim 2
Dependent Claim
170 words
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.
Claim 3
Dependent Claim
38 words
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.
Claim 4
Independent Claim
96 words
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.
Claim 5
Dependent Claim
50 words
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.
Claim 6
Independent Claim
165 words
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.
Claim 7
Independent Claim
165 words
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.
Claim 8
Dependent Claim
35 words
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.
Claim 9
Independent Claim
93 words
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.
Claim 10
Dependent Claim
50 words
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.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1985-02-15 | 1985-08-17 | 1986-02-16 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1989-02-15 | 1989-08-17 | 1990-02-16 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1993-02-15 | 1993-08-17 | 1994-02-16 | $7700.00 | Window Closed / Lapsed |