System and method for determining the orientation of an inertial measurement unit (IMU)

Patent metadata

Field	Value
Publication number	US-9846040-B2
Application number	US-201514873946-A
Country	US
Kind code	B2
Filing date	Oct 2, 2015
Priority date	May 8, 2015
Publication date	Dec 19, 2017
Grant date	Dec 19, 2017

Abstract

A system and method are provided for determining the orientation of an inertial measurement unit (IMU). The method calculates a gyroscopic quaternion, and when the IMU accelerometer reading is about equal to gravity (1 G), a field quaternion is calculated using IMU accelerometer readings. Estimates are made of angular orientation errors due to IMU angular velocity and linear acceleration, and these angular orientation errors are used to selectively mix the gyroscopic quaternion and field quaternion to supply a current sample quaternion. Alternatively, if the accelerometer reading is not about equal to 1 G, the gyroscopic quaternion is used as the current sample quaternion. In one aspect, IMU gyroscope readings and IMU accelerometer readings are calibrated in response to determining a lack of IMU movement. Near-zero gyroscope reading jitter is removed by setting the IMU gyroscopic reading to zero, when the gyroscopic reading is near zero.

First claim

I claim:

1. An inertial measurement unit (IMU) comprising:
a gyroscope having an output to supply gyroscopic readings;
an accelerometer having an output to supply accelerometer readings;
a processor,
a non-transitory memory;
an IMU application residing in the non-transitory memory, comprising a sequence of processor executable instructions for calculating a gyroscopic quaternion in response to gyroscopic readings, calculating a field quaternion using accelerometer readings when an accelerometer reading is about equal to gravity (1 G), estimating angular orientation errors due to IMU angular velocity and linear acceleration, and using the angular orientation errors to selectively mix the gyroscopic quaternion and field quaternion to supply a current sample quaternion: and,
an IMU interface to supply a current IMU orientation in space, responsive to the current sample quaternion.

2. The IMU of claim 1 further comprising:
a magnetometer having an output to supply magnetometer readings; and,
wherein the IMU application estimates magnetometer jitter errors in response to magnetometer readings, calculates the field quaternion using the accelerometer readings and magnetometer readings, and selectively mixes the gyroscopic quaternion and field quaternion includes in response to the angular orientation errors and the estimated magnetometer jitter errors.

3. The IMU of claim 2 wherein the IMU application estimates the IMU magnetometer jitters errors, and calibrates the gyroscope readings and accelerometer readings in response to determining a lack of IMU movement.

4. The IMU of claim 1 wherein the IMU application uses the gyroscopic quaternion as the current sample quaternion when the accelerometer reading is not about equal to 1 G.

5. The IMU of claim 1 wherein the IMU application, prior to calculating the field quaternion, calculates a total angular orientation error by combining an orientation angular error due to centripetal acceleration, an orientation angular error due to linear acceleration, and an orientation angular error due to estimated magnetometer jitter.

6. The IMU of claim 5 wherein the IMU application calculates an angular difference between the gyroscopic quaternion and field quaternion, compares the angular difference to the total angular orientation error, and selectively mixes the gyroscopic quaternion and field quaternion in response to the comparison.

7. The IMU of claim 1 wherein the IMU application calculates the field quaternion by:
calculating a gravitational quaternion able to rotate an accelerometer reading so that a normalized Z-axis component of the accelerometer reading is equal to 1;
using the gravitational quaternion to rotate a magnetometer reading;
setting the rotated magnetometer reading's Z-axis component to zero, creating an adjusted magnetometer reading;
calculating a magnetometer quaternion able to further rotate the adjusted magnetometer reading so that a normalized X-axis component is equal to −1; and,
combining the gravitational quaternion and the magnetometer quaternion.

8. The IMU of claim 7 wherein the IMU application calculates the field quaternion by combining a plurality of accelerometer readings to create an average accelerometer reading, and using the average accelerometer reading to calculate an accelerometer quaternion.

9. The IMU of claim 7 wherein the IMU application calculates the field quaternion by combining a plurality of magnetometer readings to create an average magnetometer reading, and using the average magnetometer reading to calculate a magnetometer quaternion.

10. The IMU of claim 9 wherein the IMU application selects a number of readings in the plurality of magnetometers readings in response to a distance between a current reading and past readings, and an estimated magnetometer jitter.

11. The IMU of claim 1 wherein the IMU application low-pass filters four vector elements of the current sample quaternion to provide an output quaternion.

12. The IMU of claim 1 wherein the IMU application compares a sum of angular commonalties between each current sample quaternion in a group of current sample quaternions, with other current sample quaternions from the group, and selects the current sample quaternion associated with the largest sum as an output quaternion.

13. An inertial measurement unit (IMU) comprising:
a gyroscope having an output to supply gyroscopic readings;
an accelerometer having an output to supply accelerometer readings;
a processor,
a non-transitory memory;
an IMU application residing in the non-transitory memory, comprising a sequence of processor executable instructions for calculating a gyroscopic quaternion in response to gyroscopic readings, calculating a field quaternion using accelerometer readings when an accelerometer reading is about equal to gravity (1 G), estimating angular orientation errors due to IMU angular velocity and linear acceleration, and using a field quaternion estimate error and the angular distance between the gyroscope quaternion and field quaternion to relatively weight the gyroscope quaternion and field quaternion used to form a current sample quaternion; and,
an IMU interface to supply a current IMU orientation in space, responsive to the current sample quaternion.

Assignees

• Sharp Laboratories Of America (Sla) Inc
• Sharp Laboratories America Inc

Inventors

• Hallberg Bryan

Classifications

• G01C21/188 Primary

  for accumulated errors, e.g. by coupling inertial systems with absolute positioning systems · CPC title

• G01C21/165 Primary

  combined with non-inertial navigation instruments · CPC title

• G01C21/16

  by integrating acceleration or speed, i.e. inertial navigation · CPC title