Apparatus for multilateration and method

• US 7,830,308 B2
• Filed: 05/23/2007
• Issued: 11/09/2010
• Est. Priority Date: 07/03/2006
• Status: Expired due to Fees

• Current Assignee: ROKE Manor Research Limited (Chemring Group PLC)
• Original Assignee: ROKE Manor Research Limited (Chemring Group PLC)
• Inventors: Brandwood, David Herbert, Quilter, Timothy John
• Primary Examiner(s): Tarcza; Thomas H
• Assistant Examiner(s): GALT, CASSI J
• Application Number:
  US11/802,551
• Publication Number:
  US 20080042902A1
• Time in Patent Office: 1,266 Days
• Field of Search: 342/450, 342/465
• US Class Current: 342/465
• CPC Class Codes: G01S 13/781 Secondary Surveillance Radar [SSR] in general
• CPC Class Codes: G01S 5/0081 Transmission between base stations
• 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

Abstract

To cater for the positioning of an aircraft in a boundary zone between two adjacent multilateration systems, the controller (14) in one system receives Time Difference of Arrival data provided by the controller (15) in the second system. The controller (15) derives the TDoA data from time of arrival data provided by its receiver stations (9-13). By furnishing TDoA data the timings of the two systems do not need to be synchronised. The controller (14) uses the TDoA data and also time of arrival data from its local receiver stations (4-8) to perform a multilateration to determine the location of the aircraft (16).

Claims

1. A system for determining the position of an aircraft, comprising:

a multilateration system controller;

a plurality of receiving stations for receiving an identifying signal from an object that is to be located within a zone of coverage of said multilateration system, said receiving stations being coupled in communication with said controller and sending to said controller time of arrival data for said identifying signal;

wherein;

said multilateration system controller has an input for receiving information from a second controller which is part of an adjacent multilateration system;

when said object is in proximity to a boundary between said zone of coverage of said multilateration system and a zone of coverage of said adjacent multilateration system, said first controller uses said time of arrival information received from said receiving stations, together with said information received from said second controller, to determine the position of said object; and

said information received from said second controller is time difference of arrival data determined based on information received by said second controller concerning arrival of said identifying signal at respective receiving stations of said adjacent multilateration system.

2. A method for determining the position of an aircraft that is within a zone of coverage of a first multilateration system having a plurality of receiving stations for receiving an identifying signal from said object, and sending time of arrival information regarding said identifying signal to a controller of said first multilateration system for position determination, said method comprising:

when said object is in a portion of said zone of coverage of said first multilateration system that is in proximity to a zone of coverage of an adjacent multilateration system, said controller of said first multilateration system receiving from a controller of said adjacent multilateration system time difference of arrival data for said identifying signal at receiving stations of said adjacent multilateration system;

said controller of said first multilateration system determining the position of said object based on said time of arrival information of said first multilateration system and said time difference of arrival information of said second multilateration system.