Method of correcting measurement errors caused by clock deviations in a secondary radar system

• US 5,363,109 A
• Filed: 07/23/1993
• Issued: 11/08/1994
• Est. Priority Date: 03/27/1991
• Status: Expired due to Term

• Current Assignee: Alcatel Sel AG (Nokia Corporation)
• Original Assignee: Alcatel Sel AG (Nokia Corporation)
• Inventors: Hofgen, Gunter, Zeitz, Rudiger
• Primary Examiner(s): Barron, Jr., Gilberto
• Application Number:
  US08/097,595
• Time in Patent Office: 473 Days
• Field of Search: 342/31, 342/32, 342/37, 342/38
• US Class Current: 342/31
• CPC Class Codes: G01S 13/765 with exchange of information between interrogator and responder
• CPC Class Codes: G01S 13/781 Secondary Surveillance Radar [SSR] in general
• CPC Class Codes: G01S 13/878 Combination of several spaced transmitters or receivers of known location for determining the position of a transponder or a reflector G01S13/874 takes precedence
• CPC Class Codes: G01S 7/40 Means for monitoring or calibrating
• CPC Class Codes: G01S 7/4008 of transmitters
• CPC Class Codes: G01S 7/4017 of HF systems

Abstract

Conventional secondary radar systems use mechanically rotating antennas to radiate a concentrated beam that rotates in a horizontal plane. Data exchange between ground stations and airborne transponders can only take place if the aircraft is struck by the antenna lobe. The distance from the aircraft to the ground station is determined from the signal transit time. Directional information is derived from the antenna position. The secondary radar system according to the invention uses an omnidirectional antenna, so that data can be exchanged between ground station and aircraft at any time. To determine the position of the aircraft, interrogation signals are transmitted by a single active ground station such that the reply signal from a transponder falls within the common system time frame of the ground station. The times of arrival of the reply signals at different ground stations are then directly proportional to the distances from the aircraft to these ground stations.

Measurement errors caused by clock deviations are corrected by determining any deviation of the clocks of two ground stations from each other. To correct clock deviations, two interrogation/reply cycles are used in direct succession in opposite directions over a common transmission path. The two transmission periods will differ by twice the deviation of the clocks in the two ground stations. The measured deviation is used to correct the measured transit time values and/or to synchronize the clocks. Synchronization of several ground stations with a master station can be achieved by using successive interrogation/reply cycles between the master station and all other stations.

Claims

1. A secondary radar system for Mode S operation, comprising:

a plurality of ground stations, each ground station including a ground-based interrogator which transmits a plurality of interrogation signals and receives a plurality of reply signals;

a plurality of antennas respectively connected to said interrogators;

at least one airborne station that transmits a reply signal in response to a received interrogation signal;

measuring means, connected to each of the interrogators, for measuring a time interval between a transmission of an interrogation signal and a reception of a reply signal;

synchronizing means for synchronizing the interrogator in each ground station to a system time within a fixed time frame;

said measuring means, including computing means for computing a signal transmit time from a respective one of said interrogators to which a respective measuring means is connected, to the at least one airborne station, and return; and

means provided in each of said interrogators, and responsive to the signal transit time computed by said computing means, for adjusting a time of transmission of a further interrogation signal from said respective one of said interrogators such that a further reply signal transmitted by the at least one airborne station, responsive to the further interrogation signal, will be received by said interrogators within the fixed time frame;

the further reply signals from the at least one airborne station, responsive to said further interrogation signal, being transmitted at a common time back to said interrogators.

2. A secondary radar system as claimed in claim 1, further comprising:

a plurality of cells formed into a cellular network, each of said plurality of cells having a respective one of said interrogators positioned therein;

said respective one of said interrogators in a respective cell in which the airborne station is located and said computing means of said measuring means connected to said respective one of said interrogators, computing said signal transit time from said respective cell to said at least one airborne station, and return.

3. A secondary radar system as claimed in claim 1, wherein:

the plurality of antennas are positioned at the interrogators; and

each antenna comprises a plurality of radiating elements fed through at least one network in such a way that a fan of overlapping radiation patterns is produced in a horizontal plane.

4. A secondary radar system as claimed in claim 1, wherein:

said computing means of said measuring means is connected to at least three interrogators for computing a position of said at least one airborne station from the reply signal transmitted from said at least one airborne station to said at least three interrogators, within the fixed time frame.

5. A secondary radar system as claimed in claim 1, further comprising a cellular network having a plurality of cells, each of said plurality of cells having at least one of said interrogators therein.

6. A secondary radar system as claimed in claim 1, further comprising:

means in each of said plurality of ground stations and each of said at least one airborne stations for exchanging information.

7. A secondary radar system as claimed in claim 1, wherein each airborne station includes a computing means for computing a plurality of distances from the reply and further reply signals radiated within the system time frame.

8. A secondary radar system as claimed in claim 1, wherein:

the plurality of antennas are positioned at the interrogators; and

each antenna comprises a plurality of radiating elements fed through at least one network in such a way that a fan of overlapping radiation patterns is produced in a horizontal plane. station equipped with a means for transmitting reply signals in response to the received interrogation signals.

9. A secondary radar system as claimed in claim 1, further comprising at least one geostationary satellite for synchronizing the interrogators to the system time.

10. A secondary radar system as claimed in claim 1, further comprising:

at least one additional interrogator connected to at least one measuring means having a computing means for computing a distance to an airborne station whose position was previously computed by at least three other computing means; and

said computing means of said at least one measuring means computing a difference between a previously computed distance value to the previously computed position of the airborne station and a distance value calculated from a plurality of coordinates of a present position of the airborne station, and based on the thus computed difference, said computing means of said at least one measuring means computes a temporal correction value which represents a deviation of an elapsed time between receipt of an interrogation signal and transmission of a reply signal from a predetermined value.

11. A secondary radar system as claimed in claim 10, wherein all interrogators but one are pure receiver units or operate as pure receiver units.

12. A secondary radar system as claimed in claim 10, wherein the system includes means for determining an altitude of the airborne station equipped with a means for transmitting reply signals in response to the received interrogation signals.

13. In a secondary radar system for Mode S operation, having:

a plurality of ground stations, each ground station including a clock and a ground-based interrogator which transmits a plurality of interrogation signals and receives a plurality of first reply signals;

a plurality of antennas respectively connected to said interrogators;

at least one airborne station that transmits a first reply signal in response to a received interrogation signal;

measuring means, connected to each of the interrogators, for measuring a time interval between a transmission of an interrogation signal and a reception of a first reply signal;

synchronizing means for synchronizing the interrogator in each ground station to a system time within a fixed time frame;

said measuring means including computing means for computing a signal transit time from a respective one of said interrogators to which a respective measuring means is connected, to the at least one airborne station, and return; and

means provided in each of said interrogators, and responsive to the signal transit time computed by said computing means, for adjusting a time of transmission of a further interrogation signal from said respective one of said interrogators such that a further first reply signal transmitted by the at least one airborne station, responsive to the further interrogation signal, will be received by said interrogators within the fixed time frame;

the further first reply signals from the at least one airborne station, responsive to said further interrogation signal, being transmitted at a common time back to said interrogators;

a method of correcting measurement errors caused by clock deviations in the plurality of ground stations, comprising the steps of;

transmitting toward said at least one airborne station from all the ground stations (S1-S4) which are used to determine a position of the at least one airborne station, a plurality of transmit interrogation signals in a cyclic sequence and at fixed points in time within another time frame that is predetermined by the clock of one of said plurality of ground stations (S1);

receiving second reply signals from said at least one airborne station at all said ground stations, said second reply signals being responsive to said plurality of transmit interrogation signals;

determining at each ground station receiving said second reply signals, a time of reception of said second reply signals;

forming said plurality of ground stations into different respective pairs of ground stations;

each of said different respective pairs of ground stations comprising one of said ground stations and one of a master ground station and another one of said ground stations;

exchanging data between the ground stations of a selected pair of ground stations, said exchanged data representing an elapsed time that is calculated between a transmission of a transmit interrogation signal by one of said selected pair of ground stations and a reception by the other one of said selected pairs of ground stations of a second reply signal from said airborne station that is responsive to said transmit interrogation signal transmitted by said one of said selected pair of ground stations;

calculating a first elapsed time for said selected pair of ground stations beginning at a first time when said one ground station of said selected pair of ground stations transmits a first transmit interrogation signal and ending at a second time when the other one of said selected pair of ground stations receives a second reply signal responsive to the first transmit interrogation signal transmitted by said one ground station;

calculating a second elapsed beginning at another first time when said other one of said ground stations of said selected pair of ground stations transmits a second transmit interrogation signal and ending when the one ground station of said selected pair of ground stations receives another second reply signal from said airborne station that is responsive to said second transmit interrogation signal transmitted from said other ground station; and

wherein

one-half of an absolute value of a difference between the first and second calculated elapsed times is representative of a deviation between the clocks of the ground stations of said selected pair of ground stations; and

then

adjusting a determination of a position of said at least one airborne station based on said deviation between said clocks.

14. The method of claim 13, wherein:

the step of forming different pairs of ground stations comprises forming each of said pairs so that one (S1) of the ground stations in each different pair of ground stations is the master ground station; and

further comprising determining any deviation of the clocks of any selected pair of ground stations from each other in said master station; and

wherein;

said exchanging step comprises communicating data from the master ground station to said other one of said ground station (S2, S3 or S4) of said selected pair, said exchanged data being used by said other one of said ground stations to correct the clock therewithin.

15. The method of claim 13, further comprising transmitting a clock signal of one of the ground stations over a plurality of data links (V) to all of a remaining plurality of ground stations.

16. The method of claim 14, further comprising transmitting a clock signal of one of the ground stations over a plurality of data links (V) to all of a remaining plurality of ground stations.

17. The method of claim 13, further comprising:

receiving at all of said plurality of ground stations a time standard signal transmitted from a public time standard transmitter; and

adjusting the clock in each ground station to said time standard signal.

18. The method of claim 14, further comprising:

receiving at all of said plurality of ground stations a time standard signal transmitted from a public time standard transmitter; and

adjusting the clock in each ground station to said time standard signal.

19. The method of claim 13, further comprising:

forming each second reply signal to include data identifying the ground station that transmitted a transit interrogation signal to which said second reply signal is responsive.

20. The method of claim 14, further comprising:

forming each second reply signal to include data, identifying the ground station that transmitted a transit interrogation signal to which said second reply signal is responsive.

21. A secondary radar system for Mode S operation, comprising:

a plurality of ground stations, each ground station including a clock and a ground-based interrogator which transmits a plurality of interrogation signals and receives a plurality of first reply signals;

a plurality of antennas respectively connected to said interrogators;

at least one airborne station that transmits a first reply signal in response to a received interrogation signal;

measuring means, connected to each of the interrogators, for measuring a time interval between a transmission of an interrogation signal and a reception of a first reply signal;

synchronizing means for synchronizing the interrogator in each ground station to a system time within a fixed time frame;

said measuring means including computing means for computing a signal transit time from a respective one of said interrogators to which a respective measuring means is connected, to the at least one airborne station, and return;

means provided in each of said interrogators, and responsive to the signal transit time computed by said computing means, for adjusting a time of transmission of a further interrogation signal from said respective one of said interrogators such that a further first reply signal transmitted by the at least one airborne station, responsive to the further interrogation signal, will be received by said interrogators within the fixed time frame;

the further first reply signals from the at least one airborne station, responsive to said further interrogation signal, being transmitted at a common time back to said interrogators; and

correcting means for correcting pairs of clocks of said ground stations, said correcting means including;

deviation determining means for determining any deviation between the clocks of selected pairs of said ground stations; and

means for correcting a determination of a position of said at least one airborne station based on the deviation determined by said deviation determining means.

22. The system of claim 21, further comprising data links (V) for forwarding a clock signal of one of the ground stations to all of a remaining plurality of ground stations.

23. The system of claim 21, wherein said plurality of antennas receive at all of said plurality of ground stations, a time standard signal transmitted from a public time standard transmitter;

and

the clock in each ground station being adjusted to said time standard signal.