ADF bearing and location for use with ASR and ASDE displays

• US 4,688,046 A
• Filed: 09/13/1982
• Issued: 08/18/1987
• Est. Priority Date: 09/13/1982
• Status: Expired due to Term

• Current Assignee: Cardion Newco Incorporated (Thales SA)
• Original Assignee: ISC Cardion Electronics Corporation
• Inventors: Schwab, Carl E.
• Primary Examiner(s): Blum, Theodore M.
• Assistant Examiner(s): Sotomayor, John B.
• Application Number:
  US06/417,251
• Time in Patent Office: 1,800 Days
• Field of Search: 343/5 LS, 343/5 GC, 343/5 SC, 343/6 TV, 343/456, 343/454, 343/463, 343/464, 343/465, 343/450, 343/453, 343/455, 343/6.5 R, 342/456, 342/454, 342/463, 342/464, 342/465, 342/450, 342/453, 342/455, 342/33, 342/36, 342/176, 342/182, 342/183
• US Class Current: 342/456
• CPC Class Codes: G01S 11/04 using angle measurements
• CPC Class Codes: G01S 3/046 Displays or indicators
• CPC Class Codes: G01S 5/04 Position of source determined by a plurality of spaced direction-finders

Abstract

An aircraft locating system identifies on a TV format radar display the position of a specific aircraft based on an RF transmission from the aircraft on an RF channel. The locating system includes at least a pair of receive stations located within several miles of an airport and separated by a base line which is in near proximity to at least one runway at the airport or a theoretical extension thereof. Each receive station includes a passive receiver for determining a bearing angle to a source of RF on the RF channel for generating a signal representative of the bearing angle.

The locating system further includes a processor which is responsive to bearing angle signals derived from the receive stations for generating line count and line delay information. The line count and line delay information correlate a position determined by the bearing angle signals from at least a pair of receive stations with a frame of reference of the TV display.

The system further includes a video mixer which responds to two different input signals. A first input signal to the video mixer is a scan converted radar return signal. The second input signal to the video mixer is the line count and line delay information. The output of the video mixer is used to drive a video display. The video display, subjected to the two identified inputs can highlight a location identified by the line count and line delay information so that for example a person viewing the display would be able to identify which of perhaps plural radar returns shown on the display is associated with an aircraft which is actively transmitting on the RF channel.

Claims

1. An aircraft locating system identifying, on a TV format radar display, position of a specific aircraft based on an RF transmission from said aircraft on an RF channel comprising:

at least a pair of receive stations located within several miles of an airport and separated by a base line which is in near proximity to at least one runway at said airport or a theoretical extension thereof,

each said receive station comprising passive receiver means for determining a bearing angle to a source of RF on said RF channel and for generating a signal representative of said bearing angle,

processing means responsive to said signals representative of bearing angle from said receive stations for generating line count and line delay data correlating a position determined by bearing angle signals from at least said pair of receive stations with a frame of reference of said TV display,

video mixer means responsive to a scan converted radar return signal and said line count and line delay data for producting a combined video signal with the ability to highlight a location identified by said line count and line delay data.

2. The apparatus of claim 1 wherein each said passive receiver means of each said receive station is tuned to an approach control frequency.

3. The appartus of claim 1 wherein each said passive receiver means at each said receive station is tuned to a ground control frequency.

4. The apparatus of claim 1 wherein each said passive receiver means is tunable between approach control frequency and ground control frequency, and means for controlling said passive receiver means to tune to approach control frequency or ground control frequency.

5. The apparatus of claim 1 which includes at least three receive stations,

wherein said processing means includes:

position determining means responsive to bearing angle representing signals from each pair of said receive stations for determining line count and line delay data for each of said pair of said receive stations, and to thereby generate line count and line delay data for each transmitting aircraft for each said pair of receiver stations,

combining means for statistically combining all line count and line delay data for each transmitting aircraft.

6. The apparatus of claim 1 which further includes, at each of said receive stations,

a TCAS receiver and time base means for maintaining a time base,

means at each station to record a received TCAS signal from TCAS equipped aircraft, as well as a state of said time base, at the time said TCAS signal is received, means for transmitting information recorded at said station to said processing means,

said processing means including means for identifying a hyperbolic location line corresponding to a position of said aircraft based on said recorded information.

7. The apparatus of claim 1 in which said receive station includes:

a first receiver, comprising said passive receiver means, tuned to an RF voice frequency corresponding to an aircraft carried VF transmitter, and

a second receiver tuned to a RF TCAS frequency corresponding to an aircraft carried TCAS transmitter,

recording means responsive to said second receiver for capturing TCAS transmissions and time of arrival of said TCAS transmission, and

means coupling signals from said recording means and signals representative of said bearing angle to said processing means,

said processing means further including;

means responsive to said signals from said recording means for generating a hyperbolic line of position along which is a transmitting aircraft, and

combining means for determining said line count and line delay data from pairs of said bearing angle signals and said hyperbolic line of position.

11. The system of claim 1 wherein said RF channel is used for an additional function not associated with said system.

12. The system of claim 5 wherein said RF channel is used for an additional function not associated with said system.

13. The system of claim 6 wherein said RF channel is used for an additional function not associated with said system.

14. The system of claim 7 wherein said RF channel is used for an additional function not associated with said system.

8. A receive station useful in generating an enhanced ASR display comprising:

a VF receiver tuned to an approach or ground control frequency,

bearing means responsive to said VF receiver for determining a bearing angle from an aircraft transmitting on said approach or ground control frequency to said station,

a TCAS receiver coupled to a TCAS decoder,

a register,

time base means for maintaining a time base,

a gate with an input from said time base means,

said gate with an output coupled to said register, and said gate with a control input from said TCAS receiver,

means connecting an output of said TCAS decoder to said register, and

control means for sampling and transmitting outputs of said bearing means and said register.

9. The station of claim 8 in which said VF receiver is tunable to either said approach or ground control frequency and in which said control means tunes said VF receiver.

10. The station of claim 8 in which said bearing means is responsive to said TCAS receiver for determining a bearing angle from an aircraft transmitting a TCAS signal to said station and said control means controls said bearing means to respond to either said TCAS receiver or said VF receiver.