Narrow band antenna harmonics for guidance in multiple frequency bands

Patent metadata

Field	Value
Publication number	US-11435165-B2
Application number	US-202017112012-A
Country	US
Kind code	B2
Filing date	Dec 4, 2020
Priority date	Dec 4, 2020
Publication date	Sep 6, 2022
Grant date	Sep 6, 2022

Abstract

A narrow band antenna is configured to guide a munition toward a target location during a flight of the munition from a launch location toward the target location. The antenna has a first mode of operation operable during a first portion of the flight at a first bandwidth, and a second mode of operation operable during a second portion of the flight at a second bandwidth, the second bandwidth being a harmonic of the first bandwidth, and may be a third harmonic of the first bandwidth. The method includes transmitting a target location information to the munition in the first bandwidth during the first portion of the flight and then transmitting the target location information to the munition in the second bandwidth during the second portion of the flight. The first band may be X-band and the second band may be Ka-band.

First claim

What is claimed:

1. A narrow band antenna configured to guide a munition toward a target location during a flight of the munition from a launch location toward the target location, the narrow band antenna comprising:
a first mode of operation operable during a first portion of the flight, the first mode of operation being at a first bandwidth; and
a second mode of operation operable during a second portion of the flight, after the first portion of the flight, and the second mode of operation being at a second bandwidth that is a harmonic of the first bandwidth.

2. The narrow band antenna of claim 1 , wherein the second bandwidth is a third harmonic of the first bandwidth.

3. The narrow band antenna of claim 1 , wherein the first mode of operation has a lower accuracy than the second mode of operation.

4. The narrow band antenna of claim 1 , wherein:
the first bandwidth comprises the X-band such that the antenna transmits at a frequency of approximately 8-12 Gigahertz (GHz) in the first mode of operation; and
the second bandwidth comprises the Ka-band such that the antenna transmits at a frequency of approximately 27-40 GHz in the second mode of operation.

5. The narrow band antenna of claim 1 , wherein the antenna bandwidth has a frequency of approximately 8-40 GHz for both the first mode of operation and the second mode of operation.

6. The narrow band antenna of claim 1 , wherein the first portion comprises a first distance, and the second portion comprises a second distance.

7. The narrow band antenna of claim 1 , wherein the first portion comprises a first amount of time and the second portion comprises a second amount of time.

8. The narrow band antenna of claim 1 , wherein the first mode and the second mode transmit and receive using a same transmitter and receiver.

9. A method for guiding a munition during a flight of the munition from a launch location toward a target location, the method comprising:
transmitting, by an antenna, a target location information to the munition in a first bandwidth during a first portion of the flight in a first mode of operation of the antenna; and
transmitting, by the antenna, the target location information to the munition in a second bandwidth during a second portion of the flight, subsequent to the first portion, in a second mode of operation of the antenna, the second bandwidth being a harmonic of the first bandwidth.

10. The method of claim 9 , further comprising determining when the first portion is complete and upon determining the first portion is complete, transmitting in the second band.

11. The method of claim 10 , wherein determining when the first portion is complete is based upon a distance from the launch location.

12. The method of claim 10 , wherein determining when the first portion is complete is based upon an amount of time since the munition left the launch location.

13. The method of claim 9 , wherein the first bandwidth comprises the X-band of approximately 8-12 Gigahertz (GHz) and the second bandwidth comprises the Ka-band of approximately 27-40 GHz.

14. The method of claim 9 , wherein transmitting in the first bandwidth and transmitting in the second bandwidth is performed by a same transmitting element of the antenna.

15. A self-guiding munition system comprising:
a narrow-band antenna having a first mode of operation operable at a first bandwidth during a first portion of a flight of the munition, and a second mode of operation operable at a second bandwidth that is a harmonic of the first bandwidth, the second mode of operation operable during a second portion of the flight of the munition; and
a processor coupled to the narrow-band antenna and coupled to a memory having instructions for carrying out the first mode of operation and the second mode of operation for the narrow-band antenna.

16. The munition system of claim 15 , wherein the second bandwidth is a third harmonic of the first bandwidth.

17. The munition system of claim 15 , wherein the first mode of operation has a lower accuracy than the second mode of operation.

18. The munition system of claim 15 , wherein the first bandwidth comprises the X-band of approximately 8-12 Gigahertz (GHz) and the second bandwidth comprises the Ka-band of approximately 27-40 GHz.

19. The munition system of claim 15 , wherein the antenna bandwidth has a bandwidth of approximately 8-40 GHz for both the first mode of operation and the second mode of operation.

20. The munition system of claim 15 , wherein the first portion comprises a first distance or a first amount of time, and the second portion comprises a second distance or a second amount of time.

Assignees

• Bae Sys Inf & Elect Sys Integ

Inventors

• Smith Brian J
• Chrobak Matthew F
• Dusaitis Peter
• Zemany Paul D

Classifications

• F41G7/2286 Primary

  using radio waves · CPC title

• F41G7/2246

  Active homing systems, i.e. comprising both a transmitter and a receiver · CPC title

• G01S13/58

  Velocity or trajectory determination systems; Sense-of-movement determination systems · CPC title

• G08C17/02 Primary

  using a radio link · CPC title

• G01S13/883

  for missile homing, autodirectors (missile guidance systems F41G7/22) · CPC title