Mechanically steered and horizontally polarized antenna for aerial vehicles, and associated systems and methods

Patent metadata

Field	Value
Publication number	US-11101557-B2
Application number	US-202016859648-A
Country	US
Kind code	B2
Filing date	Apr 27, 2020
Priority date	Mar 19, 2014
Publication date	Aug 24, 2021
Grant date	Aug 24, 2021

Abstract

A mechanically steered, horizontally polarized, directional antennae for aerial vehicles, such as UAVs. The antenna system can include a planar substrate with a horizontally polarized antenna embedded therein. A rotation member, on one end, can be attached to the planar substrate, and can extend from an external surface of the aerial vehicle. An actuator can be coupled to the rotation member to rotate the rotation member. A communication controller of the aerial vehicle can control the actuator to beam horizontally polarized radiofrequency (RF) waves to a target receiver or receive a wave front from a target transmitter.

First claim

We claim:

1. An aerial vehicle antenna system, comprising:
a rotationally symmetric planar substrate with an antenna embedded therein;
a communication controller electrically coupled to the antenna;
a signal detector coupled to the communication controller and to the antenna, the signal detector to detect signal quality of a signal received by the antenna;
a rotation member coupled to the rotationally symmetric planar substrate;
a servo, electrically coupled to the communication controller, and coupled to the rotation member to rotate the rotation member and the rotationally symmetric planar substrate in response to a command from the communication controller; and
a memory coupled to the signal detector and to the communication controller to store at least one of an azimuthal angle or an elevation angle of the antenna corresponding to a selected detected signal quality.

2. The aerial vehicle antenna system of claim 1 , wherein the selected detected signal quality is the highest of multiple detected signal strengths.

3. The aerial vehicle antenna system of claim 1 , wherein the communication controller is to provide at least one of air-to-air communication or air-to-ground communication by actuating the servo to rotate the antenna to orient a dominant radiating direction of the antenna generally toward a direction corresponding to the selected detected signal quality.

4. The aerial vehicle antenna system of claim 3 , wherein the communication controller is coupled to a flight controller and is to request the flight controller to tilt or bank an aerial vehicle that carries the aerial vehicle antenna system toward the direction corresponding to the selected detected signal quality.

5. The aerial vehicle antenna system of claim 4 , wherein the communication controller is to determine a tilt or bank angle to request from the flight controller based on at least one of the stored azimuthal angle or elevation angle.

6. The aerial vehicle antenna system of claim 4 , wherein the communication controller is to further receive a signal quality indication from the signal detector as the aerial vehicle banks or tilts, and request the flight controller to adjust the tilt or bank angle based on the received signal quality indication.

7. The aerial vehicle antenna system of claim 1 , wherein the rotation member is to rotate the symmetric planar substrate about a center of gravity of the rotationally symmetric planar substrate.

8. The aerial vehicle antenna system of claim 1 , wherein the rotationally symmetric planar substrate exhibits a disk shape, and wherein the rotationally symmetric planar substrate includes conductive elements embedded within, the conductive elements having an angular tilt relative to a flat surface of the disk shape of the substrate.

9. The aerial vehicle antenna system of claim 8 , wherein the conductive elements are completely enclosed in the rotationally symmetric planar substrate.

10. A method of operating an aerial vehicle communication system, comprising:
rotating a planar substrate, carried by an aerial vehicle and having an antenna embedded therein;
periodically measuring, via a signal detector coupled to the antenna, a signal quality of a signal received by the antenna as the planar substrate is rotated; and
identifying at least one of an azimuthal angle or an elevation angle of the signal received by the antenna corresponding to a selected detected signal quality.

11. The method of claim 10 , wherein the selected detected signal quality corresponds to a maximum measured signal quality.

12. The method of claim 10 , wherein the antenna is horizontally polarized.

13. The method of claim 10 , wherein the received signal is transmitted by an antenna of a ground communication station.

14. The method of claim 13 , further including identifying a spatial location of the ground communication station using at least one of the identified azimuthal angle or elevation angle.

15. The method of claim 13 , further including:
requesting a flight controller of the aerial vehicle to bank the aerial to aim a dominant radiating direction of the antenna generally toward the ground communication station.

16. The method of claim 13 , further including:
storing the identified azimuthal angle and elevation angle;
identifying additional azimuthal angles and elevation angles of the antenna corresponding to additional measured signal strengths;
storing the additional angles referenced to the additional measured signal strengths; and
requesting a communication controller to rotate the planar substrate to orient the antenna generally towards a stored angle corresponding to a next best measured signal strength when communication with ground communication station degrades.

17. The method of claim 16 , wherein an indication of a spatial location of the aerial vehicle is at least one of a GPS coordinate or an altitude indication.

18. The method of claim 10 , further including:
requesting a flight controller of the aerial vehicle to bank the aerial vehicle to aim a dominant radiating direction of the antenna generally toward a direction of the received signal having a maximum measured signal strength.

19. The method of claim 10 , further including:
requesting a flight controller of the aerial vehicle to bank the aerial vehicle based on at least one of the identified azimuthal angle or an elevation angle.

20. The method of claim 10 , further including:
storing the identified azimuthal angle and elevation angle;
storing an indication of a spatial location of the aerial vehicle corresponding to the stored azimuthal angle and elevation angle; and
requesting a communication controller to rotate the planar substrate to orient the antenna generally towards the stored azimuthal angle or elevation angle when the aerial vehicle returns to the spatial location corresponding to the stored indication of the spatial location.

Assignees

• Insitu Inc

Inventors

• Mack Torsten
• Kunz Peter

Classifications

• B64U2101/20

  for use as communications relays, e.g. high-altitude platforms · CPC title

• B64U2101/31

  for surveillance · CPC title

• B64U10/25

  Fixed-wing aircraft (VTOL aircraft B64U10/20) · CPC title

• B64U2101/35

  for science, e.g. meteorology · CPC title

• H01Q1/282

  Modifying the aerodynamic properties of the vehicle, e.g. projecting type aerials · CPC title