SYSTEMS AND METHODS FOR DETERMINING A POSITIONAL STATE OF AN AIRBORNE ARRAY ANTENNA USING DISTRIBUTED ACCELEROMETERS

• US 20130009818A1
• Filed: 07/07/2011
• Published: 01/10/2013
• Est. Priority Date: 07/07/2011
• Status: Active Grant

• Current Assignee: Raytheon Company (Rtx Corporation)
• Original Assignee: Raytheon Company (Rtx Corporation)
• Inventors: Quan, Clifton, Hui, Leo H., Robinson, Brendan H., Steele, John H. II
• Granted Patent: US 8,930,047 B2
• Time in Patent Office: Days
• US Class Current: 342/359
• CPC Class Codes: H01Q 1/125 Means for positioning
• CPC Class Codes: H01Q 1/28 Adaptation for use in or on aircraft, missiles, satellites, or balloons
• CPC Class Codes: H01Q 21/06 Arrays of individually energised antenna units similarly polarised and spaced apart
• CPC Class Codes: H01Q 23/00 Antennas with active circuits or circuit elements integrated within them or attached to them
• CPC Class Codes: H01Q 3/00 Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system means for positioning H01Q1/125

Abstract

Systems and methods for determining a positional state of an airborne array antenna using distributed accelerometers are described. One such method includes receiving and formatting acceleration data from each of a plurality of accelerometers mounted at different locations along the array antenna, receiving position and orientation data from an inertial navigation service (INS) mounted on the array antenna, generating an INS estimated position for each accelerometer based on the position and orientation data from the INS, generating an accelerometer estimated position for each accelerometer based on the acceleration data, determining a position and orientation of each accelerometer based on the respective INS estimated position and the respective accelerometer estimated position, determining an estimated position of a center and an orientation of the array antenna based on the determined position and orientation of each accelerometer, and adjusting a direction of the array antenna based on the estimated position of the array antenna.

Claims

1. A method for determining a positional state of an airborne array antenna using an array of distributed accelerometers, the method comprising:

receiving and formatting acceleration data from each of a plurality of accelerometers mounted at different locations along the array antenna;

receiving position and orientation data from an inertial navigation service (INS) mounted on the array antenna;

generating an INS estimated position for each accelerometer based on the position and orientation data from the INS;

generating an accelerometer estimated position for each accelerometer based on the acceleration data;

determining a position and orientation of each accelerometer based on the respective INS estimated position and the respective accelerometer estimated position;

determining an estimated position of a center and an orientation of the array antenna based on the determined position and orientation of each accelerometer; and

adjusting a direction of the array antenna based on the estimated position of the array antenna.

2. The method of claim 1, wherein the plurality of accelerometers are uniformly positioned along the array antenna.

3. The method of claim 1, wherein the plurality of accelerometers are tri-axial micro-electro-mechanical systems (MEMS) accelerometers.

4. The method of claim 1, wherein the determining the position and orientation of each accelerometer based on the respective INS estimated position and the respective accelerometer estimated position comprises:

comparing the INS estimated position and the accelerometer estimated position;

generating a residual based on the comparison of the INS estimated position and the accelerometer estimated position;

determining an updated accelerometer estimated position based on the residual; and

using the updated accelerometer estimated position in determining the position and orientation of each accelerometer based on the respective INS estimated position and the respective accelerometer estimated position.

5. The method of claim 1, wherein the generating the accelerometer estimated position for each accelerometer based on the acceleration data comprises compensating for instrument bias.

6. The method of claim 1, wherein the generating the accelerometer estimated position for each accelerometer based on the acceleration data comprises compensating for gravity.

7. The method of claim 1, wherein the generating the accelerometer estimated position for each accelerometer based on the acceleration data comprises:

generating coriolis and centripetal accelerations based on accelerometer data; and

compensating for the coriolis and centripetal accelerations.

8. A system for determining a positional state of an airborne array antenna using an array of distributed accelerometers, the system comprising:

an array antenna;

a plurality of accelerometers mounted at different locations along the array antenna;

an inertial navigation service (INS) mounted on the array antenna;

a processing circuitry configured to;

receive and format acceleration data from each of the plurality of accelerometers;

receiving position and orientation data from the inertial navigation service (INS);

generate an INS estimated position for each accelerometer based on the position and orientation data from the INS;

generate an accelerometer estimated position for each accelerometer based on the acceleration data;

determine a position and orientation of each accelerometer based on the respective INS estimated position and the respective accelerometer estimated position; and

determine an estimated position of a center and an orientation of the array antenna based on the determined position and orientation of each accelerometer.

9. The system of claim 8, further comprising a steering controller configured to adjust a direction of the array antenna based on the estimated position of the array antenna.

10. The system of claim 8, wherein the plurality of accelerometers are uniformly positioned along the array antenna.

11. The system of claim 8, wherein the plurality of accelerometers are tri-axial micro-electro-mechanical systems (MEMS) accelerometers.

12. The system of claim 8, wherein the processing circuitry is further configured to:

compare the INS estimated position and the accelerometer estimated position;

generate a residual based on the comparison of the INS estimated position and the accelerometer estimated position;

determine an updated accelerometer estimated position based on the residual; and

use the updated accelerometer estimated position to determine the position and orientation of each accelerometer based on the respective INS estimated position and the respective accelerometer estimated position.

13. The system of claim 8, wherein the processing circuitry is further configured to compensate for instrument bias.

14. The system of claim 8, wherein the processing circuitry is further configured to compensate for gravity.

15. The system of claim 8, wherein the processing circuitry is further configured to:

generate coriolis and centripetal accelerations based on accelerometer data; and

compensate for the coriolis and centripetal accelerations.