Phased array radar systems for small unmanned aerial vehicles

Patent metadata

Field	Value
Publication number	US-10317518-B2
Application number	US-201615215333-A
Country	US
Kind code	B2
Filing date	Jul 20, 2016
Priority date	Jul 20, 2015
Publication date	Jun 11, 2019
Grant date	Jun 11, 2019

Abstract

Phased array radar systems for unmanned aerial vehicles (UAVs) are disclosed. A disclosed example radar apparatus for a small UAVs includes a transmitter to transmit a transmit signal in the X-band, a receive phased array including at least two receive antennas, wherein the receive phased array provides a field-of-view of at least 100 degrees in a first direction and at least 20 degrees in a second direction perpendicular to the first direction, a first processor programmed to determine a location of an object based on an output from each of the at least two antennas, a second processor programmed to perform collision avoidance based on the location of the object, and a mount to mechanically couple the radar apparatus to the UAV.

First claim

What is claimed is:

1. A radar apparatus for a small unmanned aerial vehicle (UAV), the radar apparatus comprising:
a transmitter to transmit a transmit signal in the X-band;
a receive phased array including at least two receive antennas, wherein the receive phased array provides a field-of-view of at least 100 degrees in a first direction and at least 20 degrees in a second direction perpendicular to the first direction;
a first processor programmed to determine a location of an object based on an output from each of the at least two antennas;
a second processor programmed to perform collision avoidance based on the location of the object;
a mount to mechanically couple the radar apparatus to the UAV; and
a clutter reducer programmed to:
receive first samples of a time-domain signal, the time-domain signal received from one of the at least two receive antennas;
form an autocorrelation sequence for the received first samples;
convert the autocorrelation sequence to a set of coefficients using the Levinson algorithm; and
filter second samples of the time-domain signal using the set of coefficients.

2. The radar apparatus of claim 1 , wherein the receive phased array is a digitally-steered receive phased array capable of simultaneously forming a first beam in a first receive direction and a second beam in a second receive direction.

3. The radar apparatus of claim 1 , wherein the receive phased array is a four-channel receive phased array having four receive antennas.

4. The radar apparatus of claim 1 , wherein the first processor and the second processor are implemented by the same integrated circuit.

5. The radar of apparatus claim 1 , wherein the UAV weighs less than 25 kilograms.

6. The radar of apparatus claim 1 , wherein the UAV is a consumer good.

7. The radar of apparatus claim 1 , wherein the transmit signal comprises a frequency modulated continuous wave (FMCW) signal.

8. The radar apparatus of claim 7 , wherein the second processor is programmed to enable a user to change a transmission characteristic of the FMCW signal.

9. The radar apparatus of claim 1 , wherein one of the at least two receive antennas includes a printed circuit board antenna.

10. The radar apparatus of claim 1 , wherein one of the at least two receive antennas includes an endfire Vivaldi antenna.

11. The radar apparatus of claim 1 , wherein one of the at least two receive antennas has an aerodynamic profile.

12. The radar apparatus of claim 1 , wherein the radar apparatus comprises a homodyne system including:
a receive mixer to down convert a received signal; and
a Wilkinson power divider to direct a portion of the transmit signal to the receive mixer, wherein the receive mixer down converts the received signal based on the portion of the transmit signal.

13. The radar apparatus of claim 1 , further comprising a coupling rejection filter comprising a two-pole high-pass filter configured to adjust signals received by the radar apparatus for two targets at different distances to have generally the same received powers.

14. The radar apparatus of claim 1 , wherein the second processor is programmed to perform real-time target tracking, and to perform the collision avoidance in real-time.

15. A radar apparatus for a small unmanned aerial vehicle (UAV), the radar apparatus comprising:
a transmitter to transmit a transmit signal using a carrier signal having a frequency in the X-band;
a digitally-steered receive phased array having four receive antennas, one of the receive antennas having a conductor with a dimension based on at least one-half the wavelength of the carrier signal;
a first processor programmed to determine a location of an object based on outputs of the four receive antennas;
a second processor programmed to perform collision avoidance based on the location of the object;
a mount to mechanically couple the radar apparatus to the UAV; and
a clutter reducer programmed to:
receive first samples of a time-domain signal, the time-domain signal received from one of the four receive antennas;
form an autocorrelation sequence of the received first samples;
convert the autocorrelation sequence to a set of coefficients using the Levinson algorithm; and
filter second sample of the time-domain signal using the set of coefficients.

16. The radar apparatus of claim 15 , wherein the radar apparatus comprises a homodyne system including:
a receive mixer to down convert a received signal; and
a Wilkinson power divider to direct a portion of the transmit signal to the receive mixer, wherein the receive mixer down converts the received signal based on the portion of the transmit signal.

17. The radar apparatus of claim 16 , wherein the one of the receive antennas comprises an endfire Vivaldi antenna, and has a field-of-view of at least 100 degrees in a first direction and at least 20 degrees in a second direction perpendicular to the first direction.

Assignees

• Univ Brigham Young
• Brigham Young Univ Byu

Inventors

• Warnick Karl Foster
• Spencer Jonathan Cullinan

Classifications

• B64U10/13

  Flying platforms · CPC title

• G01S13/42

  Simultaneous measurement of distance and other co-ordinates (indirect measurement G01S13/46) · CPC title

• G01S13/34

  using transmission of continuous, frequency-modulated waves while heterodyning the received signal, or a signal derived therefrom, with a locally-generated signal related to the contemporaneously transmitted signal · CPC title

• G01S7/032

  Constructional details for solid-state radar subsystems · CPC title

• G01S13/933 Primary

  of aircraft or spacecraft · CPC title