COLLISION ALERTING AND AVOIDANCE SYSTEM

• US 20070252748A1
• Filed: 11/02/2005
• Published: 11/01/2007
• Est. Priority Date: 11/03/2004
• Status: Active Grant

• Current Assignee: Flight Safety Technologies, Inc. (Applied Blockchain, Inc.)
• Original Assignee: Flight Safety Technologies, Inc. (Applied Blockchain, Inc.)
• Inventors: Rees, Frank, Cotton, William
• Granted Patent: US 7,307,579 B2
• Time in Patent Office: Days
• US Class Current: 342/29
• CPC Class Codes: H01Q 1/28 Adaptation for use in or on aircraft, missiles, satellites, or balloons
• CPC Class Codes: H01Q 1/42 Housings not intimately mechanically associated with radiating elements, e.g. radome
• CPC Class Codes: H01Q 13/02 Waveguide horns
• CPC Class Codes: H01Q 21/064 using horn or slot aerials slotted waveguides arrays H01Q21/005
• CPC Class Codes: H01Q 21/205 providing an omnidirectional coverage turnstile aerials H01Q21/26

Abstract

A collision alerting and avoidance system for use in an aerial vehicle is presented herein. The system comprises a one low profile antenna array disposed on the aerial vehicle. The array includes a plurality of horns; a polar horn, 45-degree horns, and equatorial horns. A transmitter/receiver probe is coupled to each horn. The transmitter/receiver probes are configured to transmit electromagnetic waves and to receive an echo signal reflected from a threat obstacle. A plurality of transmitter/receiver modules are coupled to each of the transmitter/receiver probes. The transmitter/receiver modules are configured to produce electromagnetic waves for transmission and to receive the echo signal. A processor coupled to the plurality of transmitter/receiver modules controls the transmission of electromagnetic waves from the horns and processes the echo signal to provide an output signal containing information regarding the obstacle.

Claims

1. A collision alerting and avoidance system for use in an aerial vehicle comprising:

at least one low profile antenna array disposed on the aerial vehicle, said at least one low profile antenna array including a plurality of horns, said plurality of horns including at least one polar horn, a plurality of 45-degree horns, and a plurality of equatorial horns;

at least one transmitter/receiver probe coupled to each of said at least one polar horn, said 45-degree horns, and said equatorial horns, each said transmitter/receiver probe configured to operate in a transmit mode to transmit electromagnetic waves and a receive mode to receive an echo signal reflected from an obstacle in the area of the aerial vehicle;

a plurality of transmitter/receiver modules coupled to each of said transmitter/receiver probes, each said transmitter/receiver module configured to operate in a transmit mode to produce electromagnetic waves for transmission and a receive mode to receive said echo signal; and

a processor coupled to said plurality of transmitter/receiver modules, said processor configured to control transmission of said electromagnetic waves from said horns and to process said echo signal to provide an output signal containing information regarding said obstacle.

3. The collision alerting and avoidance system of claim 1, further comprising:

a flight control system coupled to said processor for processing said information in order to take action to avoid said obstacle.

4. The collision alerting and avoidance system of claim 1, wherein the aerial vehicle is a general aviation aircraft, and the collision alerting and avoidance system acts primarily as an alerting system.

5. The collision alerting and avoidance system of claim 1, wherein the aerial vehicle is an unmanned aerial vehicle, and the collision alerting and avoidance system acts primarily as an avoidance system in coordination with a flight control system.

6. The collision alerting and avoidance system of claim 1, further comprising:

a low-drag radome covering said antenna array.

7. The collision alerting and avoidance system of claim 1, further comprising:

a plurality of communication links selected from the group consisting of TCAS, ADS-B, TIS-B, and FIS-B, coupled to the collision alerting and avoidance system.

8. The collision alerting and avoidance system of claim 1, further comprising:

a second antenna array disposed in electrical communication with said at least one antenna array and said processor, said second antenna array including a plurality of horns, said plurality of horns including at least one polar horn, a plurality of 45-degree horns, and a plurality of equatorial horns.

9. The collision alerting and avoidance system of claim 1, further comprising:

a conductive metal coating disposed on an interior of said horns.

10. The collision alerting and avoidance system of claim 1, wherein said at least one transmitter/receiver probe transmits another said electromagnetic wave upon receipt of said echo signal.

11. The collision alerting and avoidance system of claim 1, wherein said processor is configured to determine a range-rate estimation of said obstacle to the aerial vehicle by varying a pulse-repetition frequency based on said information and to determine a time to closest approach to said obstacle as a ratio of a range to said range-rate estimation.

12. The collision alerting and avoidance system of claim 11, wherein said processor is configured to transmit said electromagnetic waves simultaneously from said horns.

2. The collision alerting and avoidance system of claim 2, further comprising:

a display coupled to said processor for displaying said information to an operator of the aerial vehicle, said information enables said operator to take appropriate action to avoid said obstacle.

13. A method of using a collision alerting and avoidance system on an aerial vehicle comprising:

disposing at least one low profile antenna array on the aerial vehicle, said at least one low profile antenna array including a plurality of horns, said plurality of horns including at least one polar horn, a plurality of 45-degree horns, and a plurality of equatorial horns;

coupling at least one transmitter/receiver probe to each of said at least one polar horn, said 45-degree horns, and said equatorial horns, each said transmitter/receiver probe configured to operate in a transmit mode and a receive mode;

coupling at least one transmitter/receiver module to each of said transmitter/receiver probes, said at least one transmitter/receiver module configured to produce at least one electromagnetic wave in a transmit mode and to receive an echo signal in a receive mode;

transmitting said at least one electromagnetic wave from at least one of said transmitter/receiver probes;

detecting said echo signal reflected from an obstacle in the area of the aerial vehicle in said at least one transmitter/receiver probe and said at least one transmitter/receiver module;

transmitting another electromagnetic wave from said at least one transmitter/receiver probe and said at least one transmitter/receiver module upon receipt of said echo signal; and

processing said echo signal in a processor coupled to said plurality of transmitter/receiver modules to provide an output signal containing information regarding said obstacle.

14. The method of claim 13, further comprising:

determining a range-rate estimation of said obstacle to the aerial vehicle by varying a pulse-repetition frequency based on said information; and

determining a time to closest approach to said obstacle as a ratio of range to said range-rate estimation.

15. The method of claim 13, further comprising:

displaying said information to an operator of the aerial vehicle, wherein said information enables said operator to take action to avoid said obstacle.

16. The method of claim 13, further comprising:

coupling a flight control system to said processor for processing said information to enable the aerial vehicle to take action to avoid said obstacle.

17. The method of claim 13, wherein the aerial vehicle is a general aviation aircraft.

18. The method of claim 13, wherein the aerial vehicle is an unmanned aerial vehicle.

19. The method of claim 13, further comprising:

disposing a low-drag radome over said antenna array.

20. The method of claim 13, further comprising:

electrically coupling a plurality of communication links to the collision alerting and avoidance system, said plurality of communication links selected from the group consisting of TCAS, ADS-B, TIS-B, and FIS-B.

21. The method of claim 13, further comprising:

coupling a second antenna array in electrical communication with said at least one antenna array and said processor, said second antenna array including a plurality of horns, said plurality of horns including at least one polar horn, a plurality of 45-degree horns, and a plurality of equatorial horns.

22. The method of claim 13, further comprising:

disposing a conductive metal coating on an interior of said horns.

23. The method of claim 13, further comprising:

transmitting said electromagnetic waves simultaneously from said horns.