System for monitoring aircraft position

• US 5,262,784 A
• Filed: 06/15/1992
• Issued: 11/16/1993
• Est. Priority Date: 06/15/1992
• Status: Expired due to Fees

• Current Assignee: Cardion Newco Incorporated (Thales SA)
• Original Assignee: Cardion, Inc.
• Inventors: Drobnicki, Paul F., Schwab, Carl E., Goodrich, Fred N. S.
• Primary Examiner(s): Pihulic, Daniel T.
• Application Number:
  US07/898,654
• Time in Patent Office: 519 Days
• Field of Search: 342/45, 342/46
• US Class Current: 342/45
• CPC Class Codes: G01S 13/78 discriminating between different kinds of targets, e.g. IFF-radar, i.e. identification of friend or foe G01S13/75, G01S13/79 take precedence
• CPC Class Codes: G01S 13/91 for traffic control G01S13/93 takes precedence

Abstract

A system for locating and identifying aircraft while on an airport. Each aircraft has an IFF transponder which is interrogated from on board the aircraft to produce replies at a slower rate than normal interrogation rates. A plurality of receiving stations at different locations about the airport measure the time of arrival of the replies and decode the replies. The time of arrival information is forwarded to a central receiving station along with the decode reply data. Using conventional correlation techniques, the location of each aircraft is established through the time of arrival information as well as the identity of the aircraft from the decoded reply data.

Claims

1. A system for generating signals which identify aircraft which are on the ground comprising:

an IFF transponder on board said aircraft, having an antenna input for receiving ground initiated interrogation pulse, and issuing a reply transmission in response thereto;

a directional coupler means having one port connected to said transponder antenna input, and two additional ports one of which is connected to an antenna of said aircraft for receiving said interrogation pulses;

a DME suppression circuit for supplying a signal to said IFF transponder for inhibiting replies of said transponder;

landing gear detection means for providing a signal indicating that said aircraft is on the ground; and

,

circuit means connected to receive said landing gear detection means signal and said DME suppression circuit signal, said circuit means supplying a DME inhibit signal to said IFF transponder and a suppression signal to a remaining port of said directional coupler means to suppress interrogation of said transponder by ground-initiated interrogation pulses, and for introducing interrogation pulses to said IFF transponder at a rate less than the rate of said ground interrogation pulses.

2. The system of claim 1 wherein said landing gear detection means is a weight on wheels switch which changes state when said aircraft is on the ground.

3. The system of claim 1 wherein said circuit means produces interrogation pulses which are at a pseudo randomly varying rate.

4. The system of claim 1 wherein said circuit means produces interrogation pulses for generating a reply which identifies said aircraft.

5. A system for identifying the location of an aircraft which is on the ground, having an IFF transponder, comprising:

means for detecting that said aircraft is on the ground;

means on said aircraft for suppressing interrogation of said IFF transponder from ground interrogation equipment; and

,

means for generating on board interrogation signals for interrogating said IFF transponder at a rate less than interrogation signals produced by said ground interrogation equipment when said aircraft is on the ground.

6. The system according to claim 5 wherein said on board interrogation signals produce a reply from said aircraft transponder identifying said aircraft.

7. The system according to claim 6 wherein said on board interrogation signals produce an additional reply containing data.

8. The system of claim 5 further comprising a plurality of ground receiving stations for detecting the time of arrival of said reply and for decoding each reply whereby said aircraft'"'"'s position and identity are determined.

9. The system of claim 5 wherein said reply includes position data generated on board said aircraft.

10. The system of claim 8 further comprising a acceleration detector for increasing the rate of on-board interrogation pulse sets in response to acceleration of said aircraft.

11. The system of claim 10 further comprising means at said receiving stations for detecting the change in the rate of replies produced by said aircraft.