Collision avoidance/proximity warning system using secondary radar

• US 4,027,307 A
• Filed: 05/09/1975
• Issued: 05/31/1977
• Est. Priority Date: 12/22/1972
• Status: Expired due to Term

• Current Assignee: Litchstreet Company
• Original Assignee: Litchstreet Company
• Inventors: Litchford, George B.
• Primary Examiner(s): Hubler, Malcolm F.
• Application Number:
  US05/576,143
• Time in Patent Office: 753 Days
• Field of Search: 343/6.5 LC, 343/6.5 R, 343/112 CA
• US Class Current: 342/32
• CPC Class Codes: G01S 13/781 Secondary Surveillance Radar [SSR] in general
• CPC Class Codes: G01S 13/933 of aircraft or spacecraft

Abstract

Proximity indication and evaluation of mobile vehicles, using the signals emitted by the hundreds of existing secondary radar ground stations and the nearly 100,000 cooperating transponders on the vehicles, to detect intrusion in a monitored proximity volume and to determine slant range and/or relative bearing to the intruder.

Claims

1. Proximity indicating apparatus situated at an "own" station for use in an azimuthally scanning secondary surveillance radar (SSR) system in which at least one transponder situated at an "other" station in the proximity of said own station is interrogated by the narrow rotating beam of at least one ground station remote from said own and said other station, said apparatus comprising in combination:

a. direction-finding antenna means for receiving transponder replies transmitted by said other transponder station;

b. direction-finding means, connected to said antenna means, for indicating the angle of incidence of said transponder replies on said antenna means;

c. receiver means for detecting interrogations transmitted by a ground station when said beam is directed thereto; and

d. timing means, connected to said receiver means, for enabling said direction-finding means to indicate said angle of incidence of a transponder reply to an interrogation after a predetermined period following the time that said interrogation would be received if said beam were directed at said receiver means;

whereby the bearing to said other transponder station is indicated only if replies from such transponder station are received after said predetermined period.

2. Proximity indicating apparatus situated at an "own" station for use in an azimuthally scanning secondary surveillance radar (SSR) system in which at least one transponder situated at an "other" station in the proximity of said own station is interrogated by the narrow rotating beam of at least one ground station remote from said own and said other station, said apparatus comprising, in combination:

a. direction-finding antenna means for receiving transponder replies transmitted by said other transponder station;

b. direction-finding means, connected to said antenna means, for indicating the angle of incidence of said transponder replies on said antenna means;

c. receiver means for detecting interrogations transmitted by a ground station when said beam is directed thereto; and

d. timing means, connected to said receiver means, for disabling said direction-finding means from indicating said angle of incidence of a transponder reply to an interrogation after a predetermined period following the time that said interrogation would be received if said beam were directed at said receiver means;

whereby the bearing to said other transponder station is indicated only if replies from such transponder station are received before said predetermined period.

3. Proximity indicating apparatus situated at an "own" station for use in an azimuthally scanning secondary surveillance radar (SSR) system in which at least one transponder situated at an "other" station in the proximity of said own station is interrogated by the narrow rotating beam of at least one ground station remote from said own and said other station, said apparatus comprising, in combination:

(a) direction-finding antenna means for receiving transponder replies transmitted by said other transponder station;

(b) direction-finding means, connected to said antenna means, for indicating the angle of incidence of said transponder replies on said antenna means;

(c) receiver means for detecting interrogations transmitted by a ground station when said beam is directed thereto; and

(d) timing means, connected to said receiver means, for enabling said direction-finding means to indicate said angle of incidence of a transponder reply to an interrogation during a predetermined period following the time that said interrogation would be received if said beam were directed at said receiver means;

whereby the bearing to said other transponder station is indicated only if such transponder station is located within a selected region of space.

4. The proximity indicating apparatus defined in claim 3, wherein said timing means includes gating means, connected to said receiver means, for enabling said direction-finding means for said predetermined period following receipt of said interrogation.

5. The proximity indicating apparatus defined in claim 3, wherein said at least one ground station omni-directionally transmits side lobe suppression signals;

wherein said receiver means includes means for detecting said side lobe suppression signals; and

wherein said timing means includes gating means, connected to said receiver means, for enabling said direction-finding means for said predetermined period following receipt of a side lobe suppression signal.

6. The proximity indicating apparatus defined in claim 3, wherein said timing means includes:

(1) generator means, connected to said receiver means, for continuously producing sync pulses in time with the interrogations transmitted by said ground station; and

(2) gating means, connected to said generator means, for enabling said direction-finding means for said predetermined period following a sync pulse.

7. The proximity indicating apparatus defined in claim 3, further comprising:

(e) receiver means for detecting said transponder replies; and

(f) altitude decoder means, connected to said receiver means, for determining the altitude of said other transponder station from its replies,

whereby the bearing to and altitude of said other transponder station may be indicated.

8. The proximity indicating apparatus defined in claim 7, wherein said apparatus is arranged on an aircraft having an altimeter, and wherein said apparatus further comprises comparator means, connected to said altitude decoder means and to said altimeter, for enabling said direction-finding means to indicate said angle of incidence when the altitude of said other transponder station is within predetermined limits of the altitude of said aircraft.

9. the proximity indicating apparatus defined in claim 8, further comprising means for changing said predetermined limits of said comparator means.

10. The proximity indicating apparatus defined in claim 9, wherein said means for changing said predetermined limits includes means for determining the direction of change of altitude of said aircraft.

11. The proximity indicating apparatus defined in claim 9, wherein said means for changing said predetermined limits includes means for determining the rate of change of altitude of said aircraft.

12. The proximity indicating apparatus defined in claim 7, further comprising second receiver means for detecting interrogations transmitted by a ground station when said beam is directed thereto and timing means, connected to said second receiver means, for enabling said direction-finding means to indicate said angle of incidence of a transponder reply to an interrogation during a predetermined period following the time that said interrogation would be received if said beam were directed at said second receiver means,

whereby the bearing to said other transponder station is indicated only if such transponder station is located within a selected region of space.

13. The proximity indicating apparatus defined in claim 3, further comprising:

(e) second timing means, connected to said receiver means, for enabling said direction-finder means to indicate said angle of incidence of a transponder reply to an interrogation when said beam of said ground station is directed within a selected azimuth sector of its full rotation.

14. The proximity indicating apparatus defined in claim 3, further comprising:

(e) transmitter means for sending normal interrogations substantially omni-azimuthally;

(f) second receiver means for detecting transponder replies transmitted by said other transponder station;

(g) timer means, connected to said transmitter means and to said second receiver means, for determining the elapsed time between a transmitted interrogation and a received reply; and

(h) indicator means, connected to said timer means, for indicating the slant range of said other transponder station.

15. The proximity indicating apparatus defined in claim 3, in which said other transponder station is interrogated at a first frequency by said at least one ground station and replies to interrogations at a second frequency, and in which said other transponder station may be triggered by signals at said second frequency to reply at said second frequency, said apparatus further comprising:

(e) transmitter means for sending signals at said second frequency substantially omni-azimuthally;

(f) second receiver means for detecting transponder replies to said signals;

(g) timer means, connected to said transmitter means and to said second receiver means, for determining the elapsed time between a transmitted signal and a received reply; and

(h) indicator means, connected to said timer means, for indicating the slant range of said other transponder station.

16. Proximity indicating apparatus situated at an "own" station for use in an azimuthally scanning secondary surveillance radar (SSR) system in which at least one transponder situated at an "other" station in the proximity of said own station is interrogated by the narrow rotating beam of at least one ground station remote from said own and said other station, said apparatus comprising, in combination:

(a) direction-finding antenna means for receiving transponder replies transmitted by said other transponder station;

(b) direction-finding means, connected to said antenna means, for determining the angle of incidence of said transponder replies on said antenna means;

(c) first receiver means for detecting interrogations transmitted by the ground stations when the beams thereof sweep by said own station;

(d) means, connected to said first receiver means, for determining the angle of incidence on said own station of interrogations received from one of said ground stations;

(e) second receiver means for detecting transponder replies transmitted by said other transponder station;

(f) timer means, connected to said first and said second receiver means, for determining the difference (T_D) between the time that an interrogation would be received if the beam of said one ground station were directed at said first receiver means, and the time of receipt of a transponder reply to that interrogation;

(g) logic means, connected to said angle determining means and to said timer means, for determining the slant range from said own station to said other transponder station without transmission from said own station; and

(h) means, connected to said direction-finding means, said second receiver means and to said logic means, for indicating said angle of incidence of a transponder reply of, and said slant range to, said other transponder station if said transponder reply is received during a predetermined period following the time that the interrogation which elicited such reply would be received if its beam were directed at said own station.

17. The proximity indicating apparatus defined in claim 16, further comprising means for averaging a succession of time differences (T_D) determined by said timer means, and supplying the average to said logic means.

18. The proximity indicating apparatus defined in claim 17, wherein said average is taken over a time of approximately one dwell period of said beam of a ground station.

19. The proximity indicating apparatus defined in claim 16, further comprising means for averaging a plurality of slant ranges.

20. The proximity indicating apparatus defined in claim 19, wherein said averaging means includes a plurality of memory means for storing a plurality of slant ranges and second logic means connected to said memory means, for determining the average of the slant ranges stored in said memory means.

21. The proximity indicating apparatus defined in claim 19, wherein said averaging means includes discriminator means for eliminating inconsistent slant ranges from the computed average of slant ranges.

22. The proximity indicating apparatus defined in claim 19, wherein said average is taken over a time of approximately one rotation period of said beam of a ground station.

23. The apparatus defined in claim 16, wherein said direction-finding antenna means is operative to receive interrogations transmitted by said at least one ground station and means (d) includes direction-finding means, connected to said antenna means, for determining the angle of incidence of said interrogations.

24. The apparatus defined in claim 16, wherein said ground stations omni-azimuthally transmit a reference signal as the respective beams thereof sweep through a standardized reference direction, such as magnetic North;

wherein said first receiver means is operative to detect said reference signals and to select the interrogations and reference signals received from said one ground station; and

wherein means (d) includes means, connected to said first receiver means, for determining the elapsed time between the receipt of a selected reference signal and said selected interrogations for a given beam rotation of said one ground station, said time being proportional to the azimuth of said beam of said one ground station when it is directed at said first receiver means.

25. The apparatus defined in claim 16, wherein said apparatus is arranged on an aircraft having a altimeter, and wherein said apparatus further comprises altitude decoder means, connected to said second receiver means, for determining the altitude of said other transponder station from its replies;

comparator means, connected to said altitude decoder means and to said altimeter, for producing a signal representative of the periods when the altitude of said other transponder station is within predetermined limits of the altitude of said aircraft; and

means, connected to said direction-finding means, said logic means and said comparator means for indicating said angle of incidence of said transponder replies of, and said slant range to, said other transponder station when said other transponder station is within predetermined limits of the altitude of said aircraft.

26. The apparatus defined in claim 16, further comprising means, connected to said first receiver means, for generating a signal synchronized with the interrogations transmitted by said one ground station and indicative of the time that said interrogations would be received if the beam of said one ground station were directed at said first receiver means although said beam may be directed away therefrom;

and wherein said timer means is connected to said signal generating means.

27. Proximity indicating apparatus situated at an "own" station for use in an azimuthally scanning secondary surveillance radar (SSR) system in which at least one transponder situated at an "other" station in the proximity of said own station is interrogated by the narrow rotating beam of at least one ground station remote from said own and said other station, said ground stations omni-directionally transmitting a reference signal as the respective beams thereof sweep through a standardized reference direction, such as magnetic North, said apparatus comprising, in combination:

(a) direction-finding antenna means for receiving transponder replies transmitted by said other transponder station;

(b) direction-finding means, connected to said antenna means, for determining the angle of incidence of said transponder replies on said antenna means;

(c) first receiver means for receiving said reference signals and said interrogations transmitted by said ground stations and producing an output responsive only to the reference signal and interrogations of a selected one of said ground stations; and

(d) first timer means, connected to said first receiver means, for determining the elapsed time between the receipt of said reference signal and said interrogations for a given beam rotation of said selected ground station;

whereby said time is proportional to the azimuth of said beam of said selected ground station when it is directed at said first receiver means.

28. The proximity indicating apparatus defined in claim 27, further comprising:

(e) second receiver means for detecting transponder replies transmitted by said other transponder station; and

(f) second timer means, connected to said first and second receiver means, for determining the difference (T_D) between the time that an interrogation would be received if said beam were directed at said first receiver means, and the time of receipt of a transponder reply to said interrogation.

29. The proximity indicating apparatus defined in claim 27, further comprising first logic means, connected to said direction-finding means and said first timer means, for determining the angle (D) between the directions of incidence of an interrogation and a transponder reply.

30. Proximity indicating apparatus situated at an "own" station for use in an azimuthally scanning secondary surveillance radar (SSR) system in which at least one transponder situated at an "other" station in the proximity of said own station is interrogated by the narrow rotating beam of at least one ground station remote from said own and said other station, said ground stations omni-directionally transmitting a reference signal as the respective beams thereof sweep through a standardized reference direction, such as magnetic North, said apparatus comprising, in combination:

(a) direction-finding antenna means for receiving transponder replies transmitted by said other transponder station;

(b) direction-finding means, connected to said antenna means, for determining the angle of incidence of said transponder replies on said antenna means;

(c) first receiver means for receiving said reference signals and said interrogations transmitted by said ground stations and producing an output responsive only to the reference signal and interrogations of a selected one of said ground stations;

(d) first timer means, connected to said first receiver means, for determining the elapsed time between the receipt of said reference signal and said interrogations for a given beam rotation of said selected ground station;

(e) second receiver means for detecting transponder replies transmitted by said other transponder station;

(f) second timer means, connected to said first and second receiver means, for determining the difference (T_D) between the time that a interrogation would be received if said beam were directed at said first receiver means, and the time of receipt of a transponder reply to said interrogation;

(g) logic means, connected to said direction-finding means and to said second timer means, for determining the slant range from said own station to said other transponder station without transmission from said own station.

31. The proximity indicating apparatus defined in claim 30, wherein said logic means includes:

(1) first logic means, connected to said direction-finding means and said first timer means, for determining the angle (D) between the directions of incidence of an interrogation and a transponder reply;

(2) second logic means, connected to said first logic means, for determining the valve (1- cos D) of one minus the cosine of said angle (D) between said directions of incidence; and

(3) third logic means, connected to said second timer means and to said second logic means, for determining the value T_D /(1 - cos D) of the quotient of said time difference (T_D) divided by said value of one minus the cosine of said angle (D) between said directions of incidence.

32. The proximity indicating apparatus defined in claim 31, further comprising means for averaging a succession of angles (D) determined by said first logic means, and supplying the average to said second logic means.

33. The proximity indicating apparatus defined in claim 32, wherein said average is taken over a time of approximately one dwell period of said beam of a ground station.

34. The proximity indicating apparatus defined in claim 30, further comprising means for averaging a succession of time differences (T_D) determined by said second timer means, and supplying the average to said logic means.

35. The proximity indicating apparatus defined in claim 34, wherein said average is taken over a time of approximately one dwell period of said beam of a ground station.

36. The proximity indicating apparatus defined in claim 30, further comprising means for averaging a plurality of slant ranges.

37. The proximity indicating apparatus defined in claim 36, wherein said averaging means includes a plurality of memory means for storing a plurality of slant ranges and second logic means connected to said memory means, for determining the average of the slant ranges stored in said memory means.

38. The proximity indicating apparatus defined in claim 36, wherein said averaging means includes discriminator means for eliminating inconsistent slant ranges from the computed average of slant ranges.

39. The proximity indicating apparatus defined in claim 36, wherein said average is taken over a time of approximately one rotation period of said beam of a ground station.

40. A process for detecting at an "own" station the proximity of mobile, transponder-carrying vehicles in an azimuthally scanning secondary surveillance radar (SSR) system wherein vehicle transponders in the proximity of said own station reply to interrogations transmitted in a narrow, rotating beam of at least one ground station remote from said own station and said vehicle transponders, said process comprising the steps of:

(a) receiving transponder replies to an interrogation at said own station during a predetermined period following the time that said interrogation would be received if said beam were directed toward said own station; and

(b) determining the angle of incidence of said transponder replies received during said predetermined period.

41. The process defined in claim 40, further comprising the steps of:

(c) receiving interrogations transmitted by a ground station; and

(d) indicating said angle of incidence of transponder replies when the beam of said ground station is directed within a selected azimuth sector of its full rotation.

42. The process defined in claim 40 further comprising the steps of:

(c) transmitting normal interrogations omni-azimuthally to nearby vehicle transponders;

(d) receiving transponder replies to said transmitted interrogations;

(e) determining the angle of incidence of said transponder replies to said transmitted interrogations to obtain the bearing to a nearby vehicle transponder; and

(f) determining the elapsed time between a transmitted interrogation and a received reply thereto to obtain the slant range to a nearby vehicle transponder.

43. The process defined in claim 40, in which said vehicle transponders are successively interrogated at a first frequency by said at least one ground station and reply to interrogations at a second frequency, and in which the vehicle transponders may be triggered by signals at said second frequency to reply at said second frequency, said process further comprising the steps of:

(c) transmitting signals omni-azimuthally to nearby vehicle transponders at said second frequency;

(d) receiving transponder replies to said transmitted signals;

(e) determining the angle of incidence of said transponder replies to said transmitted signals to obtain the bearing to a nearby vehicle transponder;

(g) determining the elapsed time between a transmitted signal and a received reply thereto to obtain the slant range to a nearby vehicle transponder.

44. The process defined in claim 40, further comprising the step of:

decoding the altitude of a replying transponder from its replies.

45. The process defined in claim 44, wherein said process is carried out in an aircraft having an altimeter, and said process further comprises the steps of comparing the decoded altitude of the replying transponder with the altitude of the aircraft determined by the altimeter and indicating said angle of incidence only if the two altitudes are within predetermined limits of each other.

46. A process for detecting at an "own" station the proximity of mobile, transponder-carrying vehicles in an azimuthally scanning secondary surveillance radar (SSR) system wherein vehicle transponders in the proximity of said own station reply to interrogations transmitted in a narrow, rotating beam of at least one ground station remote from said own station and said vehicle transponders, said ground stations omni-directionally transmitting a reference signal as the respective beams thereof sweep through a standardized reference direction, such as magnetic North, said process comprising the steps of:

(a) receiving said reference signals transmitted by said ground stations;

(b) receiving said interrogations transmitted by said ground stations;

(c) selecting the reference signal and interrogations received from one of said ground stations;

(d) determining the elapsed time between the receipt of said selected reference signal and said selected interrogations for a given beam rotation of said one ground station;

(e) determining the angle of incidence of transponder replies,

thereby to obtain the bearing of a nearby vehicle transponder and the azimuth of said beam of said one ground station when it is directed at the place of said own station where said interrogatories are received.

47. The process defined in claim 46 further comprising the steps of:

(f) determining the difference (T_D) between the time that an interrogation would be received if the beam of said ground station were directed toward the place of receipt at said own station of said transponder replies and the time of receipt of a transponder reply to that interrogation; and

(g) determining the slant range from said own station to said vehicle transponder, without transmission from said own station.

48. Proximity indicating apparatus situated at an "own" station for use in an azimuthally scanning secondary surveillance radar (SSR) system in which at least one transponder situated at an "other" station in the proximity of said own station is interrogated by the narrow rotating beam of at least one ground station remote from said own and said other station, said apparatus comprising, in combination:

(a) direction-finding antenna means, for receiving transponder replies transmitted by said other transponder station;

(b) direction-finding means, connected to said antenna means, for determining the angle of incidence of said transponder replies on said antenna means;

(c) first receiver means for detecting interrogations transmitted by a ground station when said beam is directed thereto;

(d) means, connected to said first receiver means, for determining the angle of incidence on said own station of interrogations received from one of said ground stations;

(e) second receiver means for detecting transponder replies transmitted by said other transponder station;

f. timer means connected to said first and said second receiver means, for determining the difference (T_D) between the time that an interrogation would be received if the beam of said one ground station were directed at said first receiver means, and the time of receipt of a transponder reply to that interrogation;

(g) first logic means, connected to said angle determining means, for determining the angle (D) between the directions of incidence of an interrogation and a transponder reply;

(h) second logic means, connected to said first logic means, for determining the value (1 - cos D) of one minus the cosine of said angle (D) between said directions of incidence; and

(i) third logic means, connected to said timer means and to said second logic means, for determining the value T_D /(1 - cos D) of the quotient of said time difference (T_D) divided by said value of one minus the cosine of said angle (D) between said directions of incidence;

whereby said quotient is proportional to the slant range from said own station to said other transponder station.

49. The proximity indicating apparatus defined in claim 48, further comprising means for averaging a succession of angles (D) determined by said first logic means, and supplying the average to said second logic means.

50. The proximity indicating apparatus defined in claim 49, wherein said average is taken over a time of approximately one dwell period of said beam of a ground station.

51. A process for detecting at an "own" station the proximity of mobile, transponder-carrying vehicles in an azimuthally scanning secondary surveillance radar (SSR) system wherein vehicle transponders in the proximity of said own station reply to interrogations transmitted in a narrow, rotating beam of at least one ground station remote from said own station and said vehicle transponders, said process comprising the steps of:

(a) receiving transponder replies to an interrogation at said own station during a predetermined period following the time that said interrogation would be received if said beam were directed toward said own station;

(b) determining the angle of incidence of said transponder replies received during said predetermined period;

(c) determining the angle of incidence of interrogations transmitted by a ground station;

(d) determining the difference (T_D) between the time that an interrogation would be received if the beam of said ground station were directed toward the place of receipt at said own station of said transponder replies and the time of receipt of a transponder reply to that interrogation; and

(e) determining the slant range from said own station to said vehicle transponder, without transmission from said own station.