Apparatus and method for determining the gravitational orientation of a well logging instrument

• US 5,606,124 A
• Filed: 05/20/1996
• Issued: 02/25/1997
• Est. Priority Date: 05/20/1996
• Status: Expired due to Term

• Current Assignee: Western Atlas International Incorporated (Northrop Grumman Corporation)
• Original Assignee: Western Atlas International Incorporated (Northrop Grumman Corporation)
• Inventors: Bergren, Paul A., Chace, David M., Roessler, Dennis E., Doyle, Mark R., Evans, John T.
• Primary Examiner(s): Williams, Hezron E.
• Assistant Examiner(s): Politzer, Jay L.
• Application Number:
  US08/655,304
• Time in Patent Office: 281 Days
• Field of Search: 73/152.01, 33/304, 33/313
• US Class Current: 73/152.01
• CPC Class Codes: E21B 47/022 of the borehole, e.g. using geomagnetism

Abstract

A method for determining orientation of an instrument with respect to earth'"'"'s gravity. The method includes measuring components of earth'"'"'s gravity along mutually orthogonal axes. One of the axes is substantially parallel to an axis of the instrument. Tilt of the instrument along two orthogonal axes is measured. One of the tilt axes is substantially parallel to the instrument axis. The instrument is rotated about its axis, and biases of the sensors used to measure the components of earth'"'"'s gravity perpendicular to the instrument axis are calculated by averaging measurements made by these sensors during rotation. The ratio of gains of these sensors is determined from the range of amplitudes of the output of these sensors during rotation. A roll angle is determined from the bias corrected measurements of components of the earth'"'"'s gravity perpendicular to the axis. The tilt measurement with respect to the two orthogonal axes is then calibrated by using the calculated roll angle. Gain and offset calibration of all the sensors used to measure the components of the earth'"'"'s gravity is performed using the calibrated tilt measurements and the orientation is calculated from the gravity measurements after correction for gain and offset of the sensors.

Claims

1. An apparatus for determining the gravimetric orientation of an instrument, comprising:

gravity sensors responsive to components of the earth'"'"'s gravity along mutually orthogonal axes, one of said axes substantially parallel to an axis of said instrument;

a tilt sensor responsive to two orthogonal angles of tilt, one of said orthogonal angles referenced to a line substantially parallel to said axis of said instrument, wherein outputs of said tilt sensor are multiplexed into a single signal processing channel; and

a processor, operatively connected to said gravity sensors and said tilt sensor, said processor including means for calculating relative gains and bias errors of said gravity sensors from a peak-to-peak amplitude of signals from said gravity sensors obtained through rotation of said instrument about said axis, said processor including means for calibrating said tilt sensor from said relative gains and bias errors of said gravity sensors, said processor including means for calculating absolute gains of said gravity sensors from calibrated signals from said tilt sensor said processor including means for calculating an orientation of said instrument from signals generated by said gravity sensors calibrated for said bias and said absolute gain.

2. The apparatus as defined in claim 1 wherein said gravity sensors comprise three mutually orthogonal accelerometers.

3. The apparatus as defined in claim 1 wherein said tilt sensor comprises an electrolytic bubble level sensor.

4. The apparatus as defined in claim 1 wherein outputs of said tilt sensor are multiplexed into a single signal processing channel.

5. The apparatus as defined in claim 1 further comprising means for rotating said instrument about said axis of said instrument.

6. The apparatus as defined in claim 5 further comprising means for selectively controlling said orientation of said instrument in response to determination of a direction of the earth'"'"'s gravity.

7. A method for determining the orientation of an instrument with respect to gravity, comprising:

measuring components of said gravity along mutually orthogonal axes, one of said axes substantially parallel to an axis of said instrument;

measuring output of a tilt sensor disposed in said instrument along two orthogonal axes, one of said tilt axes substantially parallel to said instrument axis;

rotating said instrument about said instrument axis;

calculating a roll angle from said measurements of said components of said gravity perpendicular to said instrument axis, said step of calculating said roll angle comprising calculating biases of sensors used to measure said components of said gravity perpendicular to said instrument axis by averaging measurements made by said sensors during said rotating, said step of calculating said roll angle comprising calculating a ratio of gains of said sensors from peak amplitudes of said measurements made during said rotating;

calibrating said output of said tilt sensor perpendicular to said instrument axis by characterizing said output with respect to said roll angle;

calibrating said output of said tilt sensor perpendicular to said axis by multiplexing said outputs from said tilt sensor along and perpendicular to said axis into a signal processing unit, whereby said outputs of said tilt sensor along and parallel to said axis are assumed to be calibrated by substantially identical gain and offset calibration constants;

calibrating gain and offset of all of said sensors used to measure said components of said gravity by scaling said measurements of gravity previously corrected for bias of said sensors with respect to said calibrated tilt sensor outputs; and

calculating said orientation from said gravity measurements after correction for gain and offset of said gravity sensors.

8. The method as defined in claim 7 further comprising selectively controlling said orientation of said instrument about said instrument axis in response to determination of a direction of said gravity with respect to said instrument.

9. An apparatus for determining the gravimetric orientation of an instrument, comprising:

gravity sensors responsive to components of the earth'"'"'s gravity along mutually orthogonal axes, one of said axes substantially parallel to an axis of said instrument;

a gravity-referenced tilt sensor responsive to two orthogonal angles of tilt, one of said orthogonal angles referenced to a line substantially parallel to said axis of said instrument; and

a processor, operatively connected to said gravity sensors and said tilt sensor, said processor including means for calibrating signals generated by said gravity sensors and said tilt sensor, said processor including means for calculating an orientation of said instrument from said calibrated signals generated by said sensors and said gravity-referenced tilt sensor.

10. The apparatus as defined in claim 9 wherein said gravity sensors comprise three mutually orthogonal accelerometers.

11. The apparatus as defined in claim 9 wherein said gravity-referenced tilt sensor comprises an electrolytic bubble level sensor.

12. The apparatus as defined in claim 9 wherein outputs of said tilt sensor are multiplexed into a single signal processing channel.

13. The apparatus as defined in claim 9 further comprising means for rotating said instrument about said axis of said instrument.

14. The apparatus as defined in claim 13 further comprising means for selectively controlling said orientation of said instrument in response to determination of a direction of the earth'"'"'s gravity.