Sampling and control circuit board for an inertial measurement unit

• US 9,423,426 B1
• Filed: 08/03/2012
• Issued: 08/23/2016
• Est. Priority Date: 08/03/2012
• Status: Active Grant

• Current Assignee: United States Administrator of National Aeronautics and Space Administration
• Original Assignee: United States Administrator of National Aeronautics and Space Administration
• Inventors: Chelmins, David T, Powis, Richard T. Jr., Sands, Obed
• Primary Examiner(s): Desta, Elias
• Application Number:
  US13/565,890
• Time in Patent Office: 1,481 Days
• US Class Current: 1/1
• CPC Class Codes: G01C 21/265 constructional aspects of navigation devices, e.g. housings, mountings, displays G01C21/3688 takes precedence
• CPC Class Codes: G01R 13/0254 for triggering, synchronisation

Abstract

A circuit board that serves as a control and sampling interface to an inertial measurement unit (“IMU”) is provided. The circuit board is also configured to interface with a local oscillator and an external trigger pulse. The circuit board is further configured to receive the external trigger pulse from an external source that time aligns the local oscillator and initiates sampling of the inertial measurement device for data at precise time intervals based on pulses from the local oscillator. The sampled data may be synchronized by the circuit board with other sensors of a navigation system via the trigger pulse.

Claims

1. An apparatus, comprising:

a circuit board configured to serve as a control and sampling interface between an inertial measurement device, a local oscillator, and an external trigger pulse, the circuit board configured to;

receive the external trigger pulse and time align the local oscillator to initiate sampling of the inertial measurement device for data at precise time intervals based on pulses from the local oscillator, wherein

the sampled data is synchronized by the circuit board with a navigation system via the external trigger pulse.

2. The apparatus of claim 1, wherein the circuit board is further configured to collect a plurality of inertial measurements from the inertial measurement device between external trigger pulses.

3. The apparatus of claim 1, wherein the circuit board is further configured to receive a radiometric trigger pulse from a radiometric device and synchronize sampling of the inertial measurement device with the radiometric device.

4. The apparatus of claim 3, wherein the circuit board is further configured to sample the inertial measurement device based on the external trigger pulse when the radiometric trigger pulse from the radiometric device is not received.

5. The apparatus of claim 1, wherein the data sampled from the inertial measurement device comprises delta angle along an X, Y, and Z axis measured by a gyroscope and delta velocity along the X, Y, and Z axis measured by an accelerometer.

6. The apparatus of claim 1, wherein the external trigger pulse is generated externally to the circuit board and transmitted wirelessly to the circuit board.

7. The apparatus of claim 1, wherein the circuit board is further configured to minimally process the sampled data onboard and to provide the minimally processed data to the navigation system for inclusion in the overall system.

8. The apparatus of claim 1, wherein the circuit board is further configured to cause normal time stamping overhead associated with data collection by the inertial measurement device to be performed outside of a main processor of the navigation system, freeing up processing resources to run more intensive algorithms in parallel.

9. An apparatus, comprising:

a circuit board configured to serve as a control and sampling interface between with an inertial measurement device, a local oscillator, and an external trigger pulse, the circuit board configured to;

receive the external trigger pulse and time align the local oscillator, and

sample the inertial measurement device for data at time intervals based on pulses from the oscillator.

10. The apparatus of claim 9, wherein the circuit board is further configured to collect a plurality of inertial measurements from the inertial measurement device between external trigger pulses.

11. The apparatus of claim 9, wherein the circuit board is further configured to receive a radiometric trigger pulse from a radiometric device and synchronize sampling of the inertial measurement device with the radiometric device.

12. The apparatus of claim 11, wherein the circuit board is further configured to sample the inertial measurement device based on the external trigger pulse when the radiometric trigger pulse from the radiometric device is not received.

13. The apparatus of claim 9, wherein the data sampled from the inertial measurement device comprises delta angle along an X, Y, and Z axis measured by a gyroscope and delta velocity along the X, Y, and Z axis measured by an accelerometer.

14. The apparatus of claim 9, wherein the circuit board is further configured to minimally process the sampled data onboard and to provide the minimally processed data to a navigation system for inclusion in the overall system.

15. The apparatus of claim 9, wherein the circuit board is further configured to cause normal time stamping overhead associated with data collection by the inertial measurement device to be performed outside of a main processor of a navigation system, freeing up processing resources to run more intensive algorithms in parallel.

16. A system, comprising:

an inertial measurement unit;

a local oscillator;

a main processor; and

a circuit board configured to serve as a control and sampling interface between with the inertial measurement unit, the local oscillator, an external trigger pulse, and the main processor, the circuit board configured to;

receive the external trigger pulse and time aligns the local oscillator, and

sample the inertial measurement device for data at time intervals based on pulses from the oscillator, wherein

the sampled data is synchronized by the circuit board with a navigation system via the trigger pulse, and

the main processor is configured to perform intensive processing for the navigation system.

17. The system of claim 16, wherein the circuit board is further configured to collect a plurality of inertial measurements from the inertial measurement device between external trigger pulses.

18. The system of claim 16, wherein the circuit board is further configured to receive a radiometric trigger pulse from a radiometric device and synchronize sampling of the inertial measurement device with the radiometric device.

19. The system of claim 16, wherein the circuit board is configured to minimally process the sampled data onboard and to provide the minimally processed data to the navigation system for inclusion in the overall system.

20. The system of claim 16, wherein the circuit board is further configured to cause normal time stamping overhead associated with data collection by the inertial measurement device to be performed outside of the main processor of the navigation system, freeing up processing resources to run more intensive algorithms in parallel.