STEERABLE DIRECTIONAL ANTENNA SYSTEM FOR AUTONOMOUS AIR VEHICLE COMMUNICATION

• US 20090295635A1
• Filed: 06/03/2008
• Published: 12/03/2009
• Est. Priority Date: 06/03/2008
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Erben, Erik, Smoot, Brad
• Granted Patent: US 7,764,229 B2
• Time in Patent Office: Days
• US Class Current: 342/359
• CPC Class Codes: B64U 2201/20 Remote controls
• CPC Class Codes: H01Q 1/28 Adaptation for use in or on aircraft, missiles, satellites, or balloons
• CPC Class Codes: H01Q 3/24 varying the orientation by switching energy from one active radiating element to another, e.g. for beam switching

Abstract

A system and method for communication with an autonomous air vehicle are provided. The system comprises a steerable antenna array including a plurality of directional antenna elements each selectable to receive a video signal from the air vehicle. An antenna control unit is operatively coupled to the antenna elements and includes a magnetometer for determining an orientation for each of the antenna elements. A ground control station is in operative communication with the antenna array and comprises a ground data terminal in operative communication with the antenna control unit, and an operator control unit in operative communication with the data terminal and the antenna control unit. The operator control unit is configured to obtain positions of the air vehicle and the ground control station from the data terminal. The operator control unit is further configured to determine which of the antenna elements to select by utilizing the positions of the air vehicle and the ground control station, and the orientation of one of the antenna elements.

Claims

1. A system for communication with an autonomous air vehicle, the system comprising:

a steerable antenna array, comprising;

a plurality of directional antenna elements each selectable to receive a video signal from the autonomous air vehicle; and

an antenna control unit operatively coupled to the directional antenna elements, the antenna control unit including a magnetometer for determining an orientation for each of the directional antenna elements;

a ground control station in operative communication with the steerable antenna array, the ground control station comprising;

a ground data terminal in operative communication with the antenna control unit for receiving the video signal; and

an operator control unit in operative communication with the ground data terminal and the antenna control unit, the operator control unit configured to obtain a position of the autonomous air vehicle and a position of the ground control station from the ground data terminal, the operator control unit further configured to determine which of the directional antenna elements to select by utilizing the position of the autonomous air vehicle, the position of the ground control station, and the orientation of one of the directional antenna elements;

wherein the steerable antenna array is configured for automatic selection and manual selection of one or more of the directional antenna elements.

2. The system of claim 1, wherein the control unit includes an antenna controller, and a radio frequency (RF) switch.

3. The system of claim 2, wherein the ground data terminal is configured to receive the video signal from the RF switch.

4. The system of claim 2, wherein the operator control unit is in operative communication with the antenna controller to transmit and receive command signals, control signals, and data signals.

5. The system of claim 1, wherein the directional antenna elements are positioned at an angle with respect to each other from about 45 degrees to about 90 degrees.

6. The system of claim 1, wherein the steerable antenna array comprises at least four directional antenna elements.

7. The system of claim 1, wherein the steerable antenna array comprises at least eight directional antenna elements.

8. The system of claim 1, wherein the steerable antenna array is disposed in an antenna housing that provides environmental protection to the steerable antenna array.

9. The system of claim 8, further comprising a global positioning system antenna operatively coupled to the antenna housing.

10. The system of claim 8, further comprising a command and control antenna operatively coupled to the antenna housing.

11. A method for communication with an autonomous air vehicle, the method comprising:

(a) obtaining a position for a ground control station from telemetry data;

(b) obtaining a position for the autonomous air vehicle from telemetry data;

(c) determining whether the positions of a ground control station and the autonomous air vehicle are valid;

(d) setting an antenna mode to manual and disabling an automatic antenna mode input for a steerable antenna array when the positions of the ground control station and autonomous air vehicle are not valid, and repeating steps (a) to (c) after a preset time period;

(e) determining whether the automatic antenna mode is disabled when the positions of the ground control station and autonomous air vehicle are valid;

(f) enabling the automatic antenna mode input when the automatic mode is disabled, and repeating steps (a) to (e) after the preset time period;

(g) when the automatic antenna mode is not disabled, determining whether an antenna mode is set to automatic;

(h) when the antenna mode is not set to automatic, repeating steps (a) to (g) after the preset time period;

(i) when the antenna mode is set to automatic, calculating a direction and distance to the autonomous air vehicle;

(j) obtaining direction data for a first antenna element of the steerable antenna array;

(k) determining whether the first antenna element or another antenna element is pointed at the autonomous air vehicle; and

(l) switching the antenna array to the antenna element that is pointed at the autonomous air vehicle.

12. The method of claim 11, wherein the autonomous air vehicle is a micro air vehicle.

13. The method of claim 11, wherein the ground control station and steerable antenna array are implemented in a mobile ground vehicle.

14. The method of claim 11, wherein the direction and distance to the autonomous air vehicle is calculated using an inverse Sodano algorithm.

15. The method of claim 11, wherein the direction data for the first antenna element is obtained from an antenna array magnetometer.

16. A computer program product, comprising:

a computer readable medium having instructions stored thereon for a method of communication with an autonomous air vehicle according to claim 11.

17. The computer program product of claim 16, wherein the computer readable medium has further instructions for generating a graphical user interface on a touch screen display.

18. The computer program product of claim 17, wherein the graphical user interface comprises:

an automatic mode selector button;

a manual mode selector button;

a steerable antenna array visual indicator including antenna element icons;

an air vehicle position visual indicator;

an antenna element selection visual indicator; and

a received signal strength visual indicator.

19. A computer comprising:

a computer readable medium having instructions stored thereon for a method of communication with an autonomous air vehicle according to claim 11.

20. The computer of claim 19, wherein the computer readable medium has further instructions for generating a graphical user interface on a touch screen display, the graphical user interface comprising:

an automatic mode selector button;

a manual mode selector button;

a steerable antenna array visual indicator including antenna element icons;

an air vehicle position visual indicator;

an antenna element selection visual indicator; and

a received signal strength visual indicator.