Utilizing multipath to determine down and reduce dispersion in projectiles

Patent metadata

Field	Value
Publication number	US-11435430-B2
Application number	US-202017112118-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 method for launching a round from an airborne platform, receiving a plurality of RF signals at the round, determining an amount of time between a first and second received RF signal, where the second signal is a multi-path signal and the first signal is a direct path signal. An altitude of the round is determined based on the delay between the first and second received signal and aligning the round's flight path with an initial velocity vector of the aircraft platform to reduce dispersion. The round can include a plurality of sensors for detecting the RF signals. The second received RF signal may be a multi-path signal having been reflected off of the earth's surface or another object on the earth's surface. The altitude of the round can be determined using the known altitude of the airborne platform, the delay of time between the first and second received signals, and the speed of light.

First claim

What is claimed:

1. A method comprising:
receiving, via at least one RF sensor on a round, a plurality of inherent RF signals transmitted by an airborne platform;
determining, via a processor of the round, a time delay between a first received signal of the plurality of inherent RF signals and at least one second received signal, wherein the second received signal is at least one multi-path signal;
determining, via the processor of the round, an altitude of the round based on the time delay between the first received signal and the second received signal; and
aligning a flight path of the round, via the processor of the round, with an initial velocity vector of the airborne platform relative to ground to reduce initial dispersion.

2. The method of claim 1 , wherein the round uses Doppler to determine the initial velocity vector.

3. The method of claim 1 , wherein the inherent RF signals comprises identification friend or foe (IFF) electronic warfare radar, radar warning receiver or other radar-based system emanating from the airborne platform.

4. The method of claim 1 , wherein the multi-path signal is reflected off of a surface of earth.

5. The method of claim 1 , wherein the altitude of the round is determined based on the time delay, and determined by multiplying the time delay by the speed of light, and then subtracting an altitude of the airborne platform.

6. The method of claim 1 , wherein the initial velocity vector is determined by Doppler, multipath timing, or Time Difference of Arrival.

7. The method of claim 1 , wherein the inherent RF signals are transmitted in an L-band frequency range of 0.5-1.5 Gigahertz (GHz) or a C-band frequency range of 4-8 GHz.

8. The method of claim 1 , wherein the plurality of inherent RF signals are received by multiple sensors on the round.

9. A method comprising:
receiving, via at least one sensor on a round, a plurality of RF signals transmitted by an airborne platform;
determining, via a processor of the round, a time delay between at least one first received signal of the plurality of RF signals and at least one second received signal of the plurality of RF signals; and
determining, via the processor of the round, a maximum amplitude comprising the at least one second received signal and the first received signal, the maximum amplitude indicating that the at least one sensor on the round is pointing down toward a ground surface.

10. The method of claim 9 , further comprising:
aligning a flight path of the round, via the processor of the round, with an initial velocity vector of the airborne platform relative to the ground surface using the altitude of the round, to thereby reduce dispersion.

11. The method of claim 9 , wherein the altitude of the round is determined based on the time delay, and determined by multiplying the time delay by speed of light, and then subtracting a known altitude of the airborne platform.

12. The method of claim 9 , wherein the at least one second received signal comprises at least one multi-path signal reflected from the ground surface.

13. A round configured to be launched from an airborne platform, the round comprising:
at least one sensor configured to receive a plurality of inherent RF signals transmitted by the airborne platform; and
a processor configured to determine a delay of time between a first received signal from the airborne platform and a second received signal comprising multi-path signals;
wherein the processor is configured to determine a down position of the at least one sensor based on the delay of time and to cause the round to align its flight path with an initial velocity vector of the airborne platform relative to a ground surface using an altitude of the round that reduces initial dispersion.

14. The round of claim 13 , wherein the round uses Doppler to determine the initial velocity vector of the airborne platform.

15. The round of claim 13 , wherein the second signal is a multi-path signal having signals are reflected off of the ground surface.

16. The round of claim 13 , wherein the inherent RF signals are transmitted in an L-band frequency range of 0.5-1.5 Gigahertz (GHz) or a C-band frequency range of 4-8 GHz.

17. The round of claim 13 , wherein the plurality of inherent RF signals are received by multiple sensors on the round.

18. The round of claim 13 , wherein the round comprises a weapon, a projectile, a ballistic, a bullet, a munition, a guided weapon, an unmanned aerial vehicle (UAV), or an unmanned aerial system (UAS).

19. The round of claim 13 , wherein the round uses other guidance information to direct the round to a target once the initial dispersion has been reduced.

Assignees

• Bae Sys Inf & Elect Sys Integ

Inventors

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

Classifications

• F41G7/34

  based on predetermined target position data · CPC title

• G01S2013/462

  using multipath signals · CPC title

• G01S13/883

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

• G01S7/003

  Transmission of data between radar, sonar or lidar systems and remote stations · CPC title

• G01S13/46

  Indirect determination of position data · CPC title