Ground station for a round-trip-path distance-measuring system

• US 4,126,859 A
• Filed: 10/28/1977
• Issued: 11/21/1978
• Est. Priority Date: 10/23/1976
• Status: Expired due to Term

• Current Assignee: Alcatel SA (Nokia Corporation)
• Original Assignee: International Standard Electric Corporation (ITT, Inc.)
• Inventors: Bohm, Manfred
• Primary Examiner(s): Tubbesing, T.H.
• Application Number:
  US05/846,432
• Time in Patent Office: 389 Days
• Field of Search: 343/5 LS
• US Class Current: 342/33
• CPC Class Codes: G01S 13/785 Distance Measuring Equipment [DME] systems
• CPC Class Codes: G01S 13/787 co-operating with direction defining beacons
• CPC Class Codes: G01S 13/913 for landing purposes

Abstract

This DME ground station permits the distance from the touchdown point (where no transponder can be installed) to be measured on the aircraft without any change in the airborne equipment. The time difference between the reception of an interrogating signal and the transmission of a reply signal is chosen so that the transmission of reply signals from the DME transponder located on one side of the runway corresponds to a transmission from the touchdown point with respect to the signal transit time.

On the ground, a DME transponder is located on one side of the runway on a level with the touchdown point, and a receiver and a direction finder are provided on the other side.

Claims

1. A ground DME transponder station located to facilitate air-derived determination of distance to a runway touch-down point at a predetermined location along a runway centerline, comprising:

a first ground station subassembly comprising an antenna, a first DME receiver, a transmitter and a duplexer connecting said receiver and transmitter to said antenna for alternate reception and transmission, said first subassembly being located laterally with respect to said runway at a point spaced by a predetermined distance from said touchdown point;

controllable delay means within said first ground subassembly responsive to an externally supplied transmitter delay control signal, said delay means being connected from said first DME receiver to said transmitter to control the time of transmitter reply after reception of an interrogation signal by said receiver;

a second ground station subassembly comprising a second DME receiver and a colocated direction finder, said direction finder being responsive to said interrogation signal for generating a signal representative of the direction of arrival ε

of said interrogation signal, said second subassembly being located laterally of said runway on the side opposite said first subassembly and spaced from said runway centerline by a second predetermined distance from said runway centerline;

and compensation means responsive to said first and second DME receivers and to said signal representative of the direction of arrival of said interrogation signal for controlling the delay provided by said controllable delay means such that said transmitter reply is received at the point of said air-derived determination substantially at the same time as if transmitted from said touchdown point.

2. Apparatus according to claim 1 in which said first and second predetermined distances, each a/2 where a is the total distance between said first and second ground stations, from said runway centerline are substantially equal.

3. Apparatus according to claim 2 in which said touchdown point and said first and second ground station subassemblies lie on a straight line normal to said runway centerline.

4. Apparatus according to claim 3 in which said compensation means includes time-measuring means for determining the time shift Δ

t of the interrogating signal received by said first DME compared to that received by said second DME receiver as a first correction and computer means responsive to the output of said direction finder and said time-measuring means to solve the equation Δ

d = a/2 √

1 + tan² ε

-tan ε

as a second correction, where Δ

d is the incremental range difference between the slant range from said point of air-derived distance determination to one of said ground station subassemblies and the range to touchdown along said runway centerline, and said compensation means applying said first correction signal to set the delay of said controllable delay means whenever the said interrogation signal arrives at a different time at said second versus said first ground station subassembly, and applying said second correction signal whenever said interrogation signal arrives substantially contemporaneously at said first and second ground station subassemblies, corresponding to location of said point of air-derived distance determination located on a line in a vertical plane also containing said runway centerline.

5. Apparatus according to claim 2 in which said compensation means includes time-measuring means for determining the time shift Δ

t of the interrogating signal received by said first DME receiver compared to that received by said second DME receiver as a first correction and computer means responsive to the output of said direction finder and said time-measuring means to solve the equation Δ

d = a/2 √

1 + tan² ε

-tan ε

as a second correction, where Δ

d is the incremental range difference between the slant range from said point of air-derived distance determination to one of said ground station subassemblies and the range to touchdown along said runway centerline, and said compensation means applying said first correction signal to set the delay of said controllable delay means whenever the said interrogation signal arrives at a different time at said second versus said first ground station subassembly, and applying said second correction signal whenever said interrogation signal arrives substantially contemporaneously at said first and second ground station subassemblies, corresponding to location of said point of air-derived distance determination located on a line in a vertical plane also containing said runway centerline.