Multilateration auto-calibration and position error correction

• US 6,094,169 A
• Filed: 12/11/1998
• Issued: 07/25/2000
• Est. Priority Date: 12/11/1998
• Status: Expired due to Term

• Current Assignee: SRA International, Inc. (General Dynamics Corporation)
• Original Assignee: Rannoch Corporation (General Dynamics Corporation)
• Inventors: Lee, Derrick D., Smith, Alexander E.
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): Mull, Fred H.
• Application Number:
  US09/209,008
• Time in Patent Office: 592 Days
• Field of Search: 342/365, 342/457, 342/455, 342/456, 342/463, 342/465, 342/458, 342/450, 342/37, 342/39, 342/165, 340/991
• US Class Current: 342/465
• 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 5/06 Position of source determined by co-ordinating a plurality of position lines defined by path-difference measurements G01S5/12 takes precedence
• CPC Class Codes: G01S 7/4021 of receivers
• CPC Class Codes: G08G 5/0013 with a ground station
• CPC Class Codes: G08G 5/0082 for monitoring traffic from a ground station radar or analogous systems specially adapted for traffic control G01S13/91

Abstract

The accuracy of multilateration systems can be greatly improved by using a correction method based on the SLS (Sideband Lobe Suppression) signal produced by a Secondary Surveillance Radar (SSR). Multilateration is a cooperative surveillance technique for aircraft equipped with Air Traffic Control Radar Beacon System (ATCRBS), Mode S, or Automatic Dependent Surveillance Broadcast (ADS-B) transponders. When one of these transponders aboard a vehicle is interrogated, it responds by broadcasting a message based on what the interrogation requests. These reply messages may be multilaterated to determine the source position of the transmission. Multilateration is a Time Difference of Arrival (TDOA) technique similar to triangulation. Multilateration can be performed to locate the transmission source of any SSR signal. Error detection and correction may be performed on the system by conducting a comparison of a known TDOA for the receiver/transmitter geometry, to the measured TDOA from a Side Lobe Suppression (SLS) pulse emanating from a primary radar.

Claims

1. A method for calibrating a multilateration system, comprising the steps of:

receiving, at a plurality of first radio receivers having known position values, a first radio signal from a first transmitter having a known position value;

measuring a first time value when the first radio signal is received at one of the plurality of first radio receivers;

measuring first time difference values between when the first radio signal is received at the one of the plurality of first radio receivers and when the first radio signal is received at others of the plurality of first radio receivers;

calculating a first theoretical time difference values for each of the others of the plurality of first radio receivers based upon the known position value of the first transmitter and the known position values of the first radio receivers; and

generating first error correction values, for each of the others of the plurality of first radio receivers, proportional to the difference between the first time difference values and the first theoretical time difference values.

2. The method of claim 1, wherein said step of measuring first time difference values comprises the steps of:

measuring a second time value from a calibrated time source when the first radio signal is received at one of the others of the plurality of first radio receivers;

transmitting the second time value via a data link to a central station; and

subtracting the second time value from the first time value to produce a time difference value for the one of the others of the plurality of first radio receivers.

3. The method of claim 2, wherein said step of generating first error correction values comprises the step of:

generating, for each of the others of the plurality of first radio receivers, a time difference correction error value representing a difference between measured time difference for the first radio signal to travel from the first transmitter to the one of the plurality of first radio receivers and a corresponding each of the others of the plurality of first radio receivers and the calculated theoretical time difference for the first radio signal to travel from the first transmitter to the one of the plurality f first radio receivers and a corresponding each of the others of the plurality of first radio receivers.

4. The method of claim 3, further comprising the step of:

adding the time difference correction error value for a corresponding other of the plurality of first radio receivers to subsequent measured time difference values for a corresponding other of the plurality of first radio receivers when a transponder signal is received at the corresponding other of the plurality of first radio receivers.

5. The method of claim 4, further comprising the step of:

generating a time difference correction error value for a second radio receiver of known position not receiving the first radio signal from the first transmitter, but receiving a second radio signal from a second transmitter of initial unknown position, comprising the steps of;

receiving, in the plurality of first radio receivers, a second radio signal from the second transmitter;

measuring a third time value when the second radio signal from the second transmitter is received at one of the plurality of first radio receivers;

measuring second time difference values between when the second radio signal from the second transmitter is received at the one of the plurality of first radio receivers and others of the plurality of first radio receivers;

correcting each of the second time difference values by adding the corresponding time difference correction value to a corresponding second time difference value;

multilaterating a position for the second transmitter to produce an accurate position value for the second transmitter;

measuring a third time difference value between when the second radio signal from the second transmitter is received at the second radio receiver and another of the plurality of first radio receivers;

calculating a second theoretical time difference value for the second radio receiver, based upon the accurate position value of the second transmitter and the known position value of the second radio receiver; and

generating a second error correction value, for the second radio receiver, proportional to the difference between the measured third time difference value and the second theoretical time difference value.

6. A method for accurately determining aircraft position, comprising the steps of:

receiving, at a plurality of first radio receivers having known position values, a sideband lobe suppression pulse from a radar transmitter having a known position value;

measuring a first time value when the sideband lobe suppression pulse is received at one of the plurality of first radio receivers;

measuring first time difference values between when the sideband lobe suppression pulse is received at the one of the plurality of first radio receivers and others of the plurality of first radio receivers;

calculating first theoretical time difference values for each of the others of the plurality of first radio receivers based upon the known position value of the radar transmitter and the known position values of the plurality of first radio receivers;

generating first error correction values, for each of the others of the plurality of first radio receivers, proportional to the difference between the measured first time difference values and the first theoretical time difference values;

receiving, at the plurality of first radio receivers, an aircraft transponder signal from an aircraft transponder responding to a radar signal from the radar transmitter;

measuring a second time value when the aircraft transponder signal is received at one of the plurality of first radio receivers;

measuring second time difference values between when the aircraft transponder signal is received at the one of the plurality of first radio receivers and others of the plurality of first radio receivers;

adding corresponding error correction values for each of the plurality of first radio receivers to each of the second difference values produce corrected second time difference values; and

generating a multilaterated position value of the aircraft from the corrected second time difference values.

7. The method of claim 6, wherein said step of measuring first time difference values comprises the steps of:

measuring a third time value from a calibrated time source when a sideband lobe suppression pulse is received at one of the others of the plurality of first radio receivers using a calibrated time source; and

transmitting the third time value via a data link to a central station; and

subtracting the second time value from the first time value to produce a time difference value for the one of the others of the plurality of first radio receivers.

8. The method of claim 7, wherein said step of generating first error correction values comprises the step of:

generating, for each of the others of the plurality of first radio receivers, a time difference correction error value representing a difference between measured time difference for the first radio signal to travel from the first transmitter to the one of the plurality of first radio receivers and a corresponding each of the others of the plurality of first radio receivers and the calculated theoretical time difference for the first radio signal to travel from the first transmitter to the one of the plurality of first radio receivers and a corresponding each of the others of the plurality of first radio receivers.

9. The method of claim 8, further comprising the step of:

generating a time difference correction error value for a second radio receiver of known position not receiving the first radio signal from the radar transmitter, but receiving a second radio signal from the aircraft transponder, comprising the steps of;

measuring a third time difference value between when the second radio signal from the aircraft transponder is received at the second radio receiver and another of the plurality of first radio receivers;

calculating a second theoretical time difference value for the second radio receiver, based upon the accurate position value of the aircraft transponder and the known position value of the second radio receiver; and

generating a second error correction value, for the second radio receiver, proportional to the difference between the measured third time difference value and the second theoretical time difference value.

10. A multilateration system, comprising:

a plurality of radio receivers of known position, for receiving a radio signal from a transmitter of known position;

means for measuring time values when the radio signal is received at each of the plurality of radio receivers;

means for generating a plurality of time difference values between measured time values for the plurality of radio receivers;

means for calculating theoretical time difference values between measured time values for the plurality of radio receivers based upon the known position value of the transmitter and the known position values of the radio receivers;

means for generating error correction values, for each of the plurality of time difference values, proportional to the difference between the measured time difference values and the theoretical time difference values; and

means for adding the error correction values to subsequently recieved time difference values generated in response to a received radio signal from a transmitter of initial unknown position, to generate corrected time difference values; and

means for generating a multilaterated position value of the transmitter of initial unknown position from the corrected measured time difference values.

11. The multilateration system of claim 10, wherein said means for measuring time values when the radio signal is received at the plurality of radio receivers comprises:

means for measuring a time value from a calibrated time source when the radio signal is received at a radio receiver; and

means for transmitting the time value via a data link to a central station.

12. The multilateration system of claim 11, wherein said means for generating a multilaterated position value of the transmitter from the measured time difference values comprises:

means for receiving, at the central station, over the data link, a corresponding time value from each of the plurality of radio receivers;

means for measuring difference between time values to generate time difference values; and

means for generating a multilaterated position value of the transmitter from the time difference values and the known positions of each of the plurality of radio receivers.

13. The multilateration system of claim 12, further comprising:

means for generating, from error correction values for each of the plurality of radio receivers, an error correction value for a radio receiver of known position not receiving the radio signal using the transmitter of initial unknown position as a source signal, and calculating a time difference correction value based upon theoretical time difference values from the transmitter of initial unknown position, using the multilaterated position, and actual time difference values measured from radio signals from the transmitter of initial unknown position.

14. A method of accurately multilaterating position of a transmitter of unknown position, comprising the steps of:

multilaterating a position of a first transmitter of known position to generate a first multilaterated position value;

comparing the first multilaterated position value with the known position of the first transmitter to generate a difference value;

multilaterating a position of a second transmitter of unknown position to generate a second multilaterated position value; and

correcting the second multilaterated position value by applying the correction value to the second multilaterated position value.