Airport surveillance system

• US 4,418,349 A
• Filed: 03/30/1981
• Issued: 11/29/1983
• Est. Priority Date: 04/01/1980
• Status: Expired due to Fees

• Current Assignee: Alcatel SA (Nokia Corporation)
• Original Assignee: International Standard Electric Corporation (ITT, Inc.)
• Inventors: Hofgen, Gunter, Cohrs, Heinz L.
• Primary Examiner(s): NOT, DEFINED
• Assistant Examiner(s): NOT, DEFINED
• Application Number:
  US06/248,877
• Time in Patent Office: 974 Days
• Field of Search: 343/6.5 R, 343/6.5 LC, 343/18 C, 343/112 R, 343/112 TC, 343/5 LS, 343/6.8 R, 340/24, 340/25, 340/26
• US Class Current: 342/37
• CPC Class Codes: G01S 13/003 Bistatic radar systems; Multistatic radar systems
• CPC Class Codes: G01S 13/762 with special measures concerning the radiation pattern, e.g. S.L.S. aerials or aerial systems providing at least two radiation patterns, e.g. providing sum and difference patterns, H01Q25/00
• CPC Class Codes: G01S 5/10 Position of receiver fixed by co-ordinating a plurality of position lines defined by path-difference measurements , e.g. omega or decca systemsG01S5/12 takes precedence ; beacons and receivers cooperating therewith G01S1/306, G01S1/308
• CPC Class Codes: H01Q 25/002 providing at least two patterns of different beamwidth; Variable beamwidth antennas

Abstract

Located adjacent to runways, taxiways, and approach ramps are secondary radar interrogators which radiate the P1 and P3 pulses and the P2 pulse via different directional patterns into sectors to be monitored which are individually assigned to each interrogator. Direction finders at different locations determine the directions of arrival of SSR reply signals radiated by an airborne SSR transponder in a sector to be monitored. From the directions of arrival and the locations of the direction finders, the respective transponder position is determined. The interrogators require no central control. Alternatively, the arrival times of the SSR reply signals are measured at several points; an evaluating device forms the differences in arrival time, and the intersection of the hyperbolic lines of position determined in the evaluating device is the position of the transponder.

Claims

1. A radar system for airport surface surveillance for identifying the positions on said surface of vehicles including aircraft equipped with SSR transponders responsive to a predetermined P1 and P3 interrogation pulse format providing predetermined P1 to P2 time spacing, and to a P2 pulsed pattern comprising:

first means including a plurality of self-timed, mutually asychronous pulsing interrogators providing generally lobe-shaped horizontal radiation patterns, said interrogators distributed along the sides of a pathway in a substantially symmetrical alternating pattern whereby each interrogator is located on a side of said pathway opposite that of the preceding and the next succeeding interrogator along the length of said pathway;

second means within each of said interrogators for radiating signals corresponding to said P1 and P3 pulses in a generally lobe-shaped pattern within a corresponding sector across said pathway, and signals corresponding to said P2 pulses in a pattern having lower amplitude within said sector than the amplitude of said lobe-shaped pattern but higher amplitude than said lobe-shaped pattern outside said sector;

third means comprising at least two auxiliary equipments spaced from said pathway for receiving the SSR transponder reply signals emitted by said SSR transponders, said auxiliary equipments each being adapted to determine at least one of the discrete parameters consisting of angle of arrival of said SSR reply signals and time of arrival of said SSR reply signals; and

fourth means responsive to at least one of said discrete parameters determined by said third means for identifying the instantaneous position of said SSR transponder along said airport surface.

2. A system according to claim 1 in which said fourth means responds to said discrete parameter from each of said auxiliary equipments corresponding to angles of arrival of said SSR transponder reply signals, for determining the location of said SSR transponder on the basis of intersection of said angles of arrival.

3. A system according to claim 1 in which said fourth means responds to said discrete parameter from each of said auxiliary equipments corresponding to time of arrival of said SSR reply signals, said auxiliary equipments having substantially omni-direction receiving characteristics.

4. A system according to claim 1 in which said auxiliary equipments are defined as direction finders.

5. A system according to claim 1 in which said auxiliary equipments are at least three in number.

6. A system according to claim 2 in which said auxiliary equipments are at least three in number.

7. A system according to claim 3 in which said auxiliary equipments are at least three in number.

8. A system according to claim 4 in which said auxiliary equipments are at least three in number.

9. A system according to claim 1 in which said second means comprises an antenna having first and second spaced radiating elements extending from a conductive counterpoise plane and a reflecting surface generally normal to said counterpoise plane and generally concave toward said first radiating element and said pathway, said first radiating element being energized by signals corresponding to said P1 and P3 pulses and said second radiating element being energized by signals corresponding to said P2 pulse.

10. A system according to claim 1 further including a display device responsive to said fourth means for displaying said SSR transponder instantaneous position along said airport surface.