LOW POWER INERTIAL NAVIGATION PROCESSING

• US 20090005986A1
• Filed: 06/26/2007
• Published: 01/01/2009
• Est. Priority Date: 06/26/2007
• Status: Abandoned Application

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Soehren, Wayne A.
• Application Number:
  US11/768,549
• Publication Number:
  US 20090005986A1
• Time in Patent Office: Days
• US Class Current: 701/220
• CPC Class Codes: G01C 21/188 for accumulated errors, e.g. by coupling inertial systems with absolute positioning systems

Abstract

A method and system for processing inertial navigation data are disclosed. The method comprises accumulating measurement data in a data buffer from a plurality of navigational sensors, and activating a processing unit periodically to read and process the accumulated measurement data in the data buffer. The processing unit is deactivated once the accumulated measurement data is processed, such that overall power consumption of the processing unit is reduced.

Claims

1. A method for processing inertial navigation data, the method comprising:

accumulating measurement data in a data buffer from a plurality of navigational sensors;

activating a processing unit periodically to read and process the accumulated measurement data in the data buffer; and

deactivating the processing unit once the accumulated measurement data is processed, such that overall power consumption of the processing unit is reduced.

2. The method of claim 1, further comprising determining a navigational state once the accumulated measurement data is processed.

3. The method of claim 1, wherein accumulating the measurement data further comprises tracking the recorded data with time stamps indicating the time of accumulation.

4. The method of claim 1, wherein activating the processing unit further comprises retrieving data to eliminate compensation for prescribed measurement delays.

5. The method of claim 1, wherein activating the processing unit further comprises operating a measurement filter on the processed measurement data at substantially the same time as new measurement data is collected.

6. A computer program product comprising program instructions, embodied on a machine-readable medium, the program instructions causing at least one programmable processor in an inertial navigation system to:

periodically receive an activation signal from the inertial navigation system;

once activated, process accumulated measurement data from a plurality of navigational sensors; and

once the accumulated measurement data are processed, acknowledge a deactivation signal and enter a non-active state, wherein overall power consumption of the inertial navigation system is reduced by a factor of at least two.

7. The program product of claim 6, further comprising determining a navigational state of the inertial navigation system once the accumulated measurement data is processed.

8. The program product of claim 6, wherein the program instructions cause the at least one programmable processor to retrieve the measurement data based on a programmable measurement processing rate.

9. The program product of claim 6, wherein the program instructions cause the at least one programmable processor to read the accumulated measurement data from a data buffer, the accumulated measurement data tracked with time stamps indicating the time of accumulation.

10. The program product of claim 6, wherein the program instructions cause the at least one programmable processor to operate a measurement filter on the processed measurement data while collecting new measurement data.

11. An inertial navigation system, comprising:

a navigation processing assembly comprising;

a data buffer; and

a navigation processing unit in communication with the data buffer;

a plurality of navigational sensors in communication with the data buffer; and

a system interface in communication with the navigation processing unit;

wherein the plurality of sensors take data measurements that are accumulated in the data buffer to predict movements of the inertial navigation system;

wherein the navigation processing unit is activated periodically to read and process the accumulated data measurements in the data buffer; and

wherein the navigation processing unit is deactivated once the accumulated data measurements are processed, such that overall power consumption of the navigation processing unit is reduced by a factor of at least two.

12. The system of claim 11, wherein the navigation processing unit comprises:

a Kalman filter; and

a plurality of processing blocks in communication with the Kalman filter, each of the processing blocks corresponding to at least one of the sensors.

13. The system of claim 12, wherein the Kalman filter receives raw accumulated sensor measurements directly from the data buffer.

14. The system of claim 12, wherein the Kalman filter estimates present and previous locations of a target being measured with the plurality of navigational sensors.

15. The system of claim 12, wherein the plurality of processing blocks comprise a navigation processing block, an altitude processing block, a heading computation block, a satellite navigation block, an image processing block, a range image processing block, a radio-frequency range processing block, or combinations thereof.

16. The system of claim 11, wherein the navigation processing unit provides the processed measurement data to the system interface that is coupled to a high latency navigational aid.

17. The system of claim 11, wherein the plurality of sensors comprise an inertial sensor, an altimeter, a magnetic sensor, a global navigation satellite system sensor, an electro-optical sensor, a light detecting and ranging sensor, a radio-frequency beacon, or combinations thereof.

18. The system of claim 11, wherein the navigation processing unit comprises a microprocessor, a microcontroller, a field-programmable gate array, a field-programmable object array, a programmable logic device, or an application-specific integrated circuit.

19. The system of claim 11, wherein the data buffer is a memory unit with a first-in, first-out memory configuration.

20. The system of claim 19, wherein the data buffer is one of a random access memory device, a field-programmable gate array, a programmable logic device, or an application-specific integrated circuit.