Method of determining radio frequency link reliability in an aircraft tracking system

• US 6,617,997 B2
• Filed: 01/03/2002
• Issued: 09/09/2003
• Est. Priority Date: 01/03/2002
• Status: Expired due to Term

• Current Assignee: L-3 Communications Corporation (L3Harris Technologies, Inc.)
• Original Assignee: Aviation Communication and Surveillance Systems LLC (L3Harris Technologies, Inc.)
• Inventors: Johnson, David J., Ybarra, Kathryn W.
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): ALSOMIRI, ISAM A
• Application Number:
  US10/038,134
• Publication Number:
  US 20030128151A1
• Time in Patent Office: 614 Days
• Field of Search: 342/29, 342/30, 342/31-32, 342/38, 342/36, 342/40, 342/361
• US Class Current: 342/29
• CPC Class Codes: G01S 13/767 Responders; Transponders teaching or practice apparatus for gun-aiming or gun-laying using reflecting targets or active targets F41G3/26
• CPC Class Codes: G01S 13/784 Coders or decoders therefor; Degarbling systems; Defruiting systems
• CPC Class Codes: G01S 13/933 of aircraft or spacecraft
• CPC Class Codes: G08G 5/0008 with other aircraft
• CPC Class Codes: G08G 5/0078 for monitoring traffic from the aircraft radar or analogous systems specially adapted for traffic control G01S13/91

Abstract

An aircraft system and method for determining when to attempt acquisition of an intruder for active tracking. A link reliability score associated with the intruder is adjusted based upon the signal strength of transmissions, the frequency of the transmissions, and the number of previous attempts to acquire the intruder for active tracking.

Claims

1. A system in a first aircraft for avoiding collision with a second aircraft, the system comprising:

a. means for receiving first and second signals each identifiable to the second aircraft;

b. means for adjusting a score toward a threshold value with a first value for the first signal and with a second value for the second signal, the first value being determined in accordance with signal strength of the first signal and the second value being determined in accordance with signal strength of the second signal;

c. means for adjusting the score away from the threshold value with a third value determined in accordance with a time interval between the first and the second signals;

d. means for maintaining a track of the second aircraft after the score has crossed the threshold; and

e. means for providing a traffic advisory in accordance with the track, the traffic advisory for alerting a pilot of the first aircraft to avoid collision with the second aircraft.

2. The system of claim 1 wherein the first and second signals are identifiable to the second aircraft by virtue of indicia contained in the first and second signals comprising an identification of the second aircraft.

3. The system of claim 1 wherein at least one of the first and second signals comprise radar transmission of a Mode S type.

4. The system of claim 1 wherein at least one of the first and second signals comprise at least one of a reply, a squitter, an Automatic Dependent Surveillance Broadcast (ADS-B) squitter, and a Frequency Replies Unsynchronized In Time (FRUIT) transmission.

5. The system of claim 1 wherein signal strength corresponds to at least one of amplitude at a particular time, power at a particular time, amplitude during a duration of measurement, power during a duration of measurement, an integral of amplitude, an integral of power, an average of a plurality of amplitude measurements, and an average of a plurality of power measurements.

6. The system of claim 1 wherein the time interval corresponds to an integer quantity of squitter transmission intervals.

7. The system of claim 1 wherein the first value is in a range from 0% to 40% of the threshold value.

8. The system of claim 1 wherein the third value is in a range from 0% to 10% of the threshold value.

9. The system of claim 1 wherein the track comprises indicia of identification of the second aircraft in association with at least one of estimated position, velocity, range, range rate, altitude, and bearing.

10. The system of claim 9 wherein at least one of estimated position, velocity, range, range rate, altitude, and bearing is obtained in response to interrogation by the means for maintaining the track.

11. A method performed in a first aircraft for avoiding collision with a second aircraft, the method comprising:

receiving first and second signals each identifiable to the second aircraft;

adjusting a score toward a threshold value with a first value for the first signal and with a second value for the second signal, the first value being determined in accordance with signal strength of the first signal and the second value being determined in accordance with signal strength of the second signal;

adjusting the score away from the threshold value with a third value determined in accordance with a time interval between the first and the second signals;

acquiring a track of the second aircraft after the score has crossed the threshold; and

providing a traffic advisory in accordance with the track, the traffic advisory for alerting a pilot of the first aircraft to avoid collision with the second aircraft.

12. A memory comprising indicia of the method of claim 11.

13. A traffic alert and collision avoidance system comprising the memory of claim 12.