In-situ downhole measurement correction and control
A method includes providing a Bottom Hole Assembly (BHA) in a wellbore. The BHA includes a rotary steerable system and a downhole attitude correction and control system. The downhole correction and control system includes a first sensor set, the sensors of the first sensor set positioned near ferromagnetic components of a drill string and a second sensor set, the sensors of the second sensor set positioned further from the ferromagnetic components of the drill string than the sensors of the first sensor set. Corrupted data from the first sensor set and reference data from the second sensor set is obtained, the corrupted data including cross-axis magnetometer and accelerometer measurements. The method additionally includes correcting the corrupted sensor data to form corrected sensor measurements and calculating an estimated azimuth from the corrected sensor measurements. The method further includes steering the rotary steerable system based on the estimated azimuth.
1. A method comprising:
providing a Bottom Hole Assembly (BHA) positioned in a wellbore, the BHA comprising:
a rotary steerable system; and
a RSS controller for controlling the rotary steerable system, the RSS controller having a target hold mode, the target hold mode comprising:
determining the cross-borehole plane of the rotary steerable system;
projecting a target attitude vector onto a cross-borehole plane of the rotary steerable system wherein the cross-borehole plane is separated into orthogonal components, and separate controllers each employing a Proportional Integral Derivative control operates on their respective components of a projected target vector to determine the orthogonal components of a correcting steering force applied to the rotary steerable system to maintain a target attitude; and
using the projected target attitude vector to determine a desired steering direction.
2. The method of claim 1 , wherein the RSS controller further includes a target plane control mode.
3. The method of claim 2 , wherein the RSS controller transitions from a target plane control mode into target hold mode when the rotary steerable attitude is detected to be within a defined angle of the target attitude.