Near-bit tool attitude measurement while drilling apparatus and method

• US 10,202,841 B2
• Filed: 08/29/2017
• Issued: 02/12/2019
• Est. Priority Date: 08/29/2016
• Status: Active Grant

• Current Assignee: institute of geology and geophysics, chinese academy of sciences
• Original Assignee: institute of geology and geophysics, chinese academy of sciences
• Inventors: Zhang, Wenxiu, Di, Qingyun, Chen, Wenxuan, Yang, Yongyou, Sun, Yuntao, Zheng, Jian, Liu, Jianguang
• Primary Examiner(s): Ngon, Ricky
• Application Number:
  US15/689,879
• Publication Number:
  US 20180058192A1
• Time in Patent Office: 532 Days
• Field of Search: 702 9
• CPC Class Codes: E21B 17/16 Drill collars
• CPC Class Codes: E21B 47/024 of devices in the borehole determining slope or direction of the borehole E21B47/022
• CPC Class Codes: E21B 47/07 Temperature
• CPC Class Codes: E21B 7/04 Directional drilling
• CPC Class Codes: G01V 11/002 Details, e.g. power supply systems for logging instruments, transmitting or recording data, specially adapted for well logging, also if the prospecting method is irrelevant means for transmitting well survey signals E21B47/12; signal transmission systems in general G08C; transmission in general H04B

Abstract

A near-bit tool attitude MWD apparatus includes measurement sensors and a measurement circuit. The measurement sensors transmit measured signals to the measurement circuit, and the measurement circuit processes and calculates the signals to obtain attitude data. The measurement sensors include a triaxial accelerometer, a triaxial gyroscope, a triaxial magnetic sensor and a temperature sensor, the measured data of the triaxial accelerometer, the triaxial gyroscope and the triaxial magnetic sensor are respectively corrected using the measured data of the temperature sensor, a first attitude angle is calculated using the corrected measured data of the triaxial accelerometer and the triaxial magnetic sensor. Quaternions are initialized using the first attitude angle, and the initialized quaternions are subjected to time updating according to the measured data of the triaxial gyroscope, and further an attitude angle is calculated utilizing the updated quaternions. The quaternions are periodically initialized to eliminate cumulative errors of the triaxial gyroscope, so as to improve the near-bit tool attitude MWD accuracy.

Claims

1. A near-bit tool attitude measurement while drilling method, comprising:

(1) installing a measurement-while-drilling (MWD) apparatus in a bottomhole assembly near a bottom of a drill string above a near-bit stablizer,

wherein the MWD apparatus comprises a plurality of measurement sensors coupled to a measurement circuit, wherein the plurality of measurement sensors include a triaxial accelerometer, a triaxial gyroscope, a triaxial magnetic sensor, and a temperature sensor,

wherein the measurement circuit comprises a plurality of low-pass filters coupled to an analog-to-digital converter, a field programmable gate array coupled to the analog-to-digital convertor, a processor coupled to the field programmable gate array, a memory coupled to the processor, and

wherein each of the triaxial accelerometer, the triaxial gyroscope, the triaxial magnetic sensor, and the temperature sensor is coupled to one of the plurality of low-pass filters;

(2) measuring data of the triaxial accelerometer, the triaxial gyroscope, the triaxial magnetic sensor, and the temperature sensor using the MWD apparatus;

correcting measured data of the triaxial accelerometer and the triaxial magnetic sensor by utilizing measured data of the temperature sensor, respectively; and

calculating a first attitude angle by utilizing corrected measured data of the triaxial accelerometer and the triaxial magnetic sensor;

(3) initializing quaternions by utilizing the first attitude angle;

(4) correcting measured data of the triaxial gyroscope by utilizing the measured data of the temperature sensor;

performing time updating on initialized quaternions according to the measured data of the triaxial gyroscope; and

further calculating a second attitude angle by utilizing the updated quaternions;

(5) measuring data of the triaxial gyroscope, and repeating the step (4) to calculate a third attitude angle; and

(6) after 1 s to 10 s, going to the step (2), calculating the first attitude angle by reusing the data of the triaxial accelerometer and the triaxial magnetic sensor, initializing the quaternions by using the first attitude angle, and periodically initializing the quaternions to eliminate cumulative errors of the triaxial MEMS gyroscope.

2. The method according to claim 1, further comprising:

correcting calibration coefficients and installation errors of the accelerometer, the magnetic sensor, and the gyroscope by utilizing stored calibration coefficients of the accelerometer, the magnetic sensor, and the gyroscope.

3. The method according to claim 1, wherein the triaxial accelerometer, the triaxial gyroscope and the triaxial magnetic sensor are arranged in an X axis, a Y axis, or a Z axis that are orthogonally to each other, and in each axial direction, directions of sensitive axes of the accelerometer, the gyroscope and the magnetic sensor are parallel.

4. The method according to claim 1, wherein high-frequency interferences in analog signals outputted by measurement sensors are filtered out by the low-pass filters, the filtered output signals of the measurement sensors are subjected to acquisition by the analog-to-digital converter, and the timing control of the analog-to-digital converter is realized by a field programmable gate array, while the field programmable gate array performs digital filtering on acquired original data, and sends the filtered data to the processor according to a communication protocol after packetizing, the processor stores original time series data in the memory, while the attitude angle is solved, and the processor comprises an attitude angle calculation module, a quaternion initialization module and a quaternion updating module.

5. The method according to claim 1, wherein the accelerometer is a micro electromechanical system (MEMS) accelerometer, the gyroscope is a MEMS gyroscope, and the magnetic sensor is a magnetoresistive sensor.

6. The method according to claim 1, wherein the memory stores calibration coefficients of the accelerometer, the magnetic sensor and the gyroscope.

7. The method according to claim 1, wherein the attitude angle comprises an inclination angle, an azimuth angle, and a toolface angle.

8. The method according to claim 1, wherein the MWD apparatus is disposed less than 6 meters from a drill bit.

9. The method according to claim 8, wherein the MWD apparatus is disposed less than 4 meters from the drill bit.

10. The method according to claim 9, wherein the MWD apparatus is disposed less than 3 meters from the drill bit.