GPS independent guidance sensor system for gun-launched projectiles

• US 20130001354A1
• Filed: 06/30/2011
• Published: 01/03/2013
• Est. Priority Date: 06/30/2011
• Status: Active Grant

• Current Assignee: Northrop Grumman Guidance & Electronics Co., Inc. (Northrop Grumman Corporation)
• Original Assignee: Northrop Grumman Guidance & Electronics Co., Inc. (Northrop Grumman Corporation)
• Inventors: Meyer, A. Douglas, Karam, Mostafa A., Lee, Charles A., Volk, Charles H.
• Granted Patent: US 8,598,501 B2
• Time in Patent Office: Days
• US Class Current: 244/3.19
• CPC Class Codes: F41G 7/305 for spin-stabilized missiles
• CPC Class Codes: F41G 7/34 based on predetermined target position data
• CPC Class Codes: F42B 15/01 Arrangements thereon for guidance or control steering arrangements F42B10/60; aircraft flight control B64C; guidance systems other than those installed aboard F41G7/00, F41G9/00; locating by use of radio or other waves G01S; flight control in general G05D1/00; computer aspects G06]
• CPC Class Codes: G01S 5/0247 Determining attitude

Abstract

A sensor system uses ground emitters to illuminate a projectile in flight with a polarized RF beam. By monitoring the polarization modulation of RF signals received from antenna elements mounted on the projectile, both angular orientation and angular rate signals can be derived and used in the inertial solution in place of the gyroscope. Depending on the spacing and positional accuracies of the RF ground emitters, position information of the projectile may also be derived, which eliminates the need for accelerometers. When RF signals of ground emitter/s are blocked from the guided projectile, the sensor deploys another plurality of RF antennas mounted on the projectile nose to determine position and velocity vectors and orientation of incoming targets.

Claims

1. A sensor system for measuring parameters used for guiding a gun-launched projectile, comprising:

a plurality of RF antennas mounted to the projectile, each RF antenna being arranged to receive an RF signal of a selected polarization; and

a radar RF emitter/receiver system arranged to direct polarized RF signals toward the plurality of RF antennas, the radar RF emitter/receiver being further arranged to receive polarized RF signals received by another plurality of RF antennas embedded on nose portions of the projectile and process the received polarized RF signals to determine position and velocity vectors of an incoming projectile.

2. The sensor system of claim 1 wherein the plurality of RF antennas includes:

a first pair of antenna elements spaced apart symmetrically with respect to the projectile lengthwise axis along an axis x located in a plane normal to the lengthwise axis; and

a second pair of antenna elements spaced apart symmetrically with respect to the projectile lengthwise axis along an axis y located in a plane normal to the lengthwise axis and perpendicular to the x-axis.

3. The sensor system of claim 2 wherein the first pair of antenna elements are active such that they function as both sending and receiving antennas, and the second pair of antennas are passive so that they function only as receiving antennas.

4. The sensor system of claim 3 wherein two antenna elements on the same axis have the same orientation and phase center to ensure the equality of both magnitude, and direction of electric fields transmitted or received by each one of the two antenna elements.

5. The sensor system of claim 4 wherein the antenna elements on the x-axis are cross-polarized and on the y-axis are like-polarized.

6. The radar RF emitter/receiver system of claim 1, comprising three emitters that emit signals with three different frequencies for measuring position and velocity vectors of the guided projectile, the three emitters are located at coordinates (X₁,Y₁,Z₁), (X₂,Y₂,Z₂) and (X₃,Y₃,Z₃), the system being arranged to record signal travel time between each of the three emitters and a corresponding RF antenna embedded in the projectile, the system being further arranged to use a triangulation process to measure distances between each of the emitters and the corresponding RF antenna to obtain the position vector of the projectile, the system being further arranged to use the measured Doppler frequency associated with each emitter and the derived position vector to obtain the velocity vector of the projectile, the signals from the three emitters each having its own direction and polarization, which provide additional information for extracting angular rate of the projectile.

7. The radar RF emitter/receiver system of claim 1, further comprising a neural network arranged to extract values of angular rotation from measured RF polarized power, the neural network including an input layer that receives measured RF polarized data output from a plurality of RF sensors, a plurality of hidden layers arranged to contain neurons that calculate signals that indicate rotation, and an output layer that outputs roll, pitch and yaw signals.

8. A method for measuring parameters used for guiding a gun-launched projectile, comprising the steps of:

mounting a plurality of RF antennas to the fins of the projectile;

arranging each RF antenna to receive an RF signal of a selected polarization; and

arranging a radar RF emitter/receiver system to direct polarized RF signals toward the plurality of RF antennas; and

arranging the radar RF emitter/receiver to receive polarized RF signals received by the plurality of RF antennas mounted on nose portions of the projectile and process the received polarized RF signals to determine position and velocity vectors for incoming targets.

9. The method of claim 8 further including the steps of:

spacing a first pair of antenna elements apart symmetrically with respect to the projectile lengthwise axis along an axis x located in a plane normal to the lengthwise axis; and

spacing a second pair of antenna elements apart symmetrically with respect to the projectile lengthwise axis along an axis y located in a plane normal to the lengthwise axis and perpendicular to the x-axis.

10. The method of claim 9 further including the steps of:

forming the first pair of antenna elements to be active such that they function as both sending and receiving antennas; and

forming the second pair of antennas to be passive so that they function only as receiving antennas.

11. The method of claim 10 further including the step of arranging the antenna elements such that two antenna elements on the same axis have same orientation and phase center to ensure the equality of both magnitude, and direction of electric fields transmitted or received by each one of the two antenna elements.

12. The method of claim 11 further including the step of arranging the antenna elements such that the antenna elements on the x-axis are like-polarized and the y-axis are cross-polarized.

13. The method of claim 8 further including the steps of:

arranging three emitters to emit signals with three different frequencies for measuring position and velocity vectors of the projectile'"'"'s fins;

placing the three emitters at coordinates (X₁,Y₁,Z₁), (X₂,Y₂,Z₂) and (X₃,Y₃,Z₃);

recording signal travel time between each of the three emitters and a corresponding RF antenna embedded in the projectile;

using a triangulation process to measure distances between each of the emitters and the corresponding RF antenna to obtain the position vector of the projectile;

measuring Doppler frequency associated with each emitter and the derived position vector to obtain the velocity of the projectile; and

arranging the signals from the three emitters so that each has its own direction and polarization to provide additional information for extracting angular rate of the projectile.

14. The method of claim 8 further including the steps of:

arranging a neural network to extract values of angular rotation from measured RF polarized power; and

forming the neural network to include an input layer that receives measured RF polarized data output from a plurality of RF sensors, a plurality of hidden layers arranged to contain neurons that calculate signals that indicate rotation, and an output layer that outputs roll, pitch and yaw signals.