Nine-Axis Sensor Fusion Using Direction

Application Report
SLAA518A – February 2012
Nine-Axis Sensor Fusion Using the Direction Cosine
Matrix Algorithm on the MSP430F5xx Family
Erick Macias, Daniel Torres, Sourabh Ravindran
...................................................................................
ABSTRACT
This application report explains the implementation of an Attitude and Heading Reference System
(AHRS), using the ultra-low-power MSP430F5xx microcontroller, a magnetometer, a gyroscope, and an
accelerometer on all three axes. The calibration of the sensors is key to the accuracy of the algorithm,
therefore, the sensors’ output must be calibrated before being input to the Direction Cosine Matrix (DCM)
algorithm. The algorithm is applied to the calibrated sensor readings to calculate the Euler angles
describing the orientation of a body; consisting of the yaw, roll, and pitch angles.
Project collateral and source code discussed in this application report can be downloaded from the
following URL: http://www.ti.com/lit/zip/slaa518.
This application report uses the MPU-9150 MotionFit™ Wireless Developer Kit from InvenSense
(http://www.invensense.com).
Document License: This work is licensed under the Creative Commons Attribution-NonCommercialNoDerivs 3.0 Unported License (CC BY-NC-ND 3.0). To view a copy of this license, visit
http://creativecommons.org/licenses/by-nc-nd/3.0/legalcode or send a letter to Creative Commons, 171
Second Street, Suite 300, San Francisco, California, 94105, USA.
1
2
3
4
5
6
7
Contents
Introduction .................................................................................................................. 2
Direction Cosine Matrix Algorithm ........................................................................................ 3
MSP430F5xx Firmware .................................................................................................... 4
Sensors Calibration ......................................................................................................... 7
Conclusion ................................................................................................................... 9
Schematics ................................................................................................................. 11
References ................................................................................................................. 14
List of Figures
....................................................................................................
1
AHRS Circuit Overview
2
Direct Cosine Matrix Algorithm Overview ................................................................................ 4
3
MSP430F5xx AHRS Firmware Overview ................................................................................ 5
4
AHRS GUI
5
5
MSP430F5xx Calibration Firmware Overview
6
6
7
8
9
...................................................................................................................
..........................................................................
AHRS Calibration GUI ......................................................................................................
Magnetometer Hard Iron Calibration .....................................................................................
Rotations for Hard Iron Calibration of the Magnetometer .............................................................
MSP430 Voltage Measurement .........................................................................................
3
7
8
9
10
List of Tables
1
Sensor Data Request Commands ........................................................................................ 6
2
System Current Consumption
...........................................................................................
10
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1
Introduction
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Micro USB Connector
Blue Low Energy
(BLE)
JTAG
MSP430F5528
LEDs
Barometric
Pressure Sensor
Magnetometer
Gyroscope
Accelerometer
1
Introduction
Modeling the orientation of a rigid body, including airplanes, RC toys, sport watches, smart phones,
humans, etc. can be implemented by using the DCM algorithm. When creating an AHRS, also known as
Magnetic, Angular Rate, and Gravity sensor (MARG), a magnetometer, a gyroscope, and an
accelerometer are required. The calibrated sensors readings are fed to the DCM algorithm, which provides
a complete measurement of the orientation, relative to the earth’s magnetic field and the direction of
gravity, expressed by the Euler (roll, yaw, and pitch) angles. In certain applications such as smart phones
the ultra-low-power MSP430F5xx can handle all the communication with the motion sensors via I2C
protocol. This leads to lower power consumption and higher CPU performance in the system, since they
can request raw data or the orientation angles at any given time, meanwhile they can be in sleep mode, or
they can perform other tasks that could have been delayed by the calculation of the orientation.
This document covers the following key points:
• Direction Cosine Matrix Algorithm (Section 2)
• MSP430F5xx Firmware (Section 3)
• Sensor Calibration (Section 4)
Figure 1 contains the AHRS circuit overview. The MSP430F5xx can communicate via the USB Module
CDC class with two GUIs running in the computer:
• AHRS GUI (See Figure 4)
• AHRS Calibration GUI (See Figure 6)
The calibration GUI must be used when the AHRS system is used for the first time and in the case where
the system’s calibration values get corrupted by the presence of a constant magnetic field (hard iron
effects). The AHRS GUI displays the Euler angles, as well as the visual representation of such; a horizon
and a digital compass. These two GUIs require separate firmware to be downloaded to the MSP430F5xx:
• MSP430 AHRS Project AHRS Mode → AHRS GUI
• MSP430 AHRS Project Calibration Mode → Calibration GUI
There are other alternatives to send the Euler angles to the computer or other devices instead of USB;
Bluetooth Low Energy (BLE) is one of them. The MSP430 communicates with BLE (BR-LE4.0) chip via
UART. This application report will not cover the communication with the BR-LE4.0 chip
(http://www.blueradios.com). To find more information about BLE, visit the http://www.ti.com website.
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Direction Cosine Matrix Algorithm
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+3.3 V
MSP430F5528
Accelerometer
3.3k W
Magnetometer
Computer
3.3k W
SDA
I2C Module
Calibration
GUI
SCL
Gyroscope
Barometric
Pressure
AHRS
GUI
TX
UART Module
Bluetooth Low
Energy
RX
HANDOVER EULER ANGLES AND SENSOR DATA
USB Module
USB Module
REQUEST SENSOR DATA
Legend:
DCM Sensors
Figure 1. AHRS Circuit Overview
2
Direction Cosine Matrix Algorithm
The DCM algorithm calculates the orientation of a rigid body, in respect to the rotation of the earth by
using rotation matrices. For a visual representation of the Direction Cosine Matrix Algorithm, see Figure 2.
The rotation matrices are related to the Euler angles, which describe the three consecutive rotations
needed to describe the orientation. The three sensors used in the algorithm are:
• The accelerometer measures earth’s gravity field minus acceleration.
• The magnetometer measures earth’s magnetic field.
• The gyroscope sensor measures angular velocity.
The gyroscope sensor is the primary sensor used to calculate the orientation of the system. Since the
gyroscope is not affected by the gravitational or magnetic field, it requires the readings from the
accelerometer and magnetometer to calculate a reference vector. Gyroscopes’ readings have different
offsets depending on which direction the gyroscope is facing; when these readings are integrated over
time it causes the integral result to drift. The accelerometer is not affected by drift, therefore, it can be
used as an orientation reference in the X and Z axis of the rigid body to compensate the roll-pitch error
(gyro’s offset error). The magnetometer’s readings are used to calculate the heading of the rigid body. The
magnetometer must be three axes to be able to calculate the heading of the system in any position of the
sensor platform; to compensate yaw error. The heading of the system used as the reference vector in the
Y axis (yaw error), in addition to the roll-pitch error calculated by the accelerometer, it allows the system to
calculate the rotation correction matrix. Afterwards, the algorithm uses a proportional plus integral
feedback controller on the correction matrix to the remove the drift from the gyro’s readings.
The compensated gyroscope readings denoted as ω (omega), are then fed to the “Normalization &
Kinematics” block as it can be seen in Figure 2. The rotation matrix’s columns are unit vectors. Thus,
before calculating the kinematics portion it must be normalized. (See Renormalization section in [2]). Once
normalized, the gyroscope along with the previous rotation matrix are used to calculate the current rotation
matrix (R Matrix) by using Equation 17 in the Computing Direction Cosines From Gyro Signals section in
[2]. Finally, the Euler angles are calculated from the updated rotation matrix.
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MSP430F5xx Firmware
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Accelerometer
X*, Y*, Z*
Accelerometer
X, Y, Z
Magnetometer
X, Y, Z
R Matrix
R Matrix
Heading
Yaw
Drift Detection
Sensors
Calibration
(Section 4)
Magnetometer
X*, Y*, Z*
Heading Error
Roll-Pitch Error
Gyroscope
X*, Y*, Z*
Gyroscope
X, Y, Z
Error
Adjustment
PI Controller
+ Drift Adjustment
Euler Angles
(roll, pitch, and yaw)
R Matrix
R Matrix
Normalization and
Kinematics
Figure 2. Direct Cosine Matrix Algorithm Overview
3
MSP430F5xx Firmware
This section covers the firmware’s architecture of the AHRS. There are two modes of firmware that can be
downloaded to the MSP430F5xx family: AHRS mode (see Figure 3) or the calibration mode (see
Figure 4). The mode must be defined in device.h, where you must enable either #define AHRS_MODE
or #define CALIBRATION_MODE.
Both modes initialize the MSP430F5xx by following these steps:
1. Set the main clock to 16 MHz.
2. Initialize I2C module (Master mode, Baud Rate ~ 400k Hz, 7-bit Addressing).
3. Initialize background timer (Rate ~20 mS, Disabled).
4. Initialize USB Module (CDC Class).
Afterwards the motion sensors are initialized, and the background timer is enabled. The timer wakes the
MCU from low-power-mode 0 (lowest power consumption mode allowed when using USB module) at a 50
Hz (20 mS) rate. The accelerometer and gyroscope are read and calibrated at a 50 Hz (20 mS) rate. The
magnetometer is read at 10 Hz (100 mS), since the heading of the system does not fluctuate as much as
the gravitational field or angular velocity.
3.1
AHRS Mode
The magnetometer’s three axes readings are soft and hard iron compensated (see Section 4), and the
sensor platform’s heading is calculated. The calibrated sensor readings are fed to the Direction Cosine
Matrix algorithm (see Section 2) to calculate the Euler angles (roll, pitch, and yaw). The orientation angles
are sent via USB to the AHRS GUI in the computer, at a 20 Hz (50 mS) rate. The GUI displays the Euler
angles in a horizon (pitch & roll) and a digital compass (yaw) (see Figure 4).
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MSP430F5xx Firmware
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Legend:
Initialize MCU
AHRS_ENABLED
Initialize Sensors
Read Accelerometer
and Gyroscope
100 ms
elapsed?
Yes
No
Magnetometer
Calibration
DCM Algorithm
50 ms
elapsed?
Read Magnetometer
Calculate Heading
Yes
Send Euler Angles
to GUI
No
Blink LED
Yes
Enter Low Power
Mode 0
20 ms
elapsed?
No
Figure 3. MSP430F5xx AHRS Firmware Overview
Figure 4. AHRS GUI
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MSP430F5xx Firmware
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The background timer and the reading of the sensors can run at a faster frequency to increase the
resolution of the algorithm’s integration; therefore, gaining better accuracy of the orientation angles. On
the other hand, when running the algorithm at a higher frequency it causes the power consumption and
CPU usage to increase. Running the background timer at 50 Hz is the sweet spot for low-power
consumption and orientation accuracy.
3.2
Calibration Mode
When the calibration mode (see Figure 5) is enabled instead of calculating the Euler angles, the firmware
checks if a request for sensor raw data has been received or not. When the request (see Table 1) is
received, the MSP430F5xx sends the GUI 500 samples of sensor data in all 3 axes via USB; this results
in a 10 second calibration for the accelerometer and gyroscope, and a 50 second calibration for the
magnetometer. When calibrating the magnetometer, it is very important to read the max and min value for
each axis; sending more samples from the MSP430 to the GUI allows you to move the board in all the
angles necessary for calibration.
Table 1. Sensor Data Request Commands
Command ID
Sensor Data Requested
0x31
Accelerometer
0x32
Gyroscope
0x33
Magnetometer
Legend:
Initialize MCU
CALIBRATION_ENABLED
Initialize Sensors
Read Accelerometer
and Gyroscope
100 ms
elapsed?
Yes
Read Magnetometer
No
Request
received?
Yes
Send Raw Sensor
Data
No
Yes
Blink LED
Enter Low Power
Mode 0
20 ms
elapsed?
No
Figure 5. MSP430F5xx Calibration Firmware Overview
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Sensors Calibration
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4
Sensors Calibration
This section covers how to calibrate the DCM sensors using the 9-Axis Sensor Fusion Calibration GUI
(see Figure 6). The X, Y, and Z offsets calculated for each sensor must be updated inside
calibrationSensors() in AppRoutines.c.
Figure 6. AHRS Calibration GUI
Follow these steps to calibrate your sensor platform:
1. Download the firmware with CALIBRATION_MODE enabled to the MSP430F5xx.
2. Install the USB drivers in the PC.
3. Open the 9-Axis Sensor Fusion Calibration GUI.
4. Click “Auto Connect”.
Now the Accelerometer, Gyroscope and Magnetometer buttons should be enabled.
4.1
Accelerometer
When calibrating the accelerometer, the GUI requests for the AHRS board to be placed in the three
different positions. When the board is placed on a flat surface (parallel to earth), the only axis that should
be non zero is the perpendicular axis to the surface; therefore, the readings on the two other axes will be
offsets (using Equation 1). with a three axes accelerometer, readings can be taken from the accelerometer
having the axis perpendicular to the flat surface and pointing to the sky being X, Y, and Z. For example,
when X is pointing upwards to the sky, the offsets are calculated for Y and Z. Then when Y is pointing
upwards to the sky, the offsets are calculated for X and Z. Therefore, when having gone through all three
positions there are 2 offsets values for each axis, which are averaged and displayed as the X, Y, and Z
offsets.
dataoffset =
4.2
datamin + datamax
2
(1)
Gyroscope
When calibrating the gyroscope, the AHRS board must be stationary on a flat surface where the angular
velocity for all three axes should be 0. The offsets are calculated by using Equation 1 on all three axes.
Once the GUI receives the requested raw gyroscope readings from the AHRS, it will display the offsets as
the X, Y, and z offsets.
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Sensors Calibration
4.3
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Magnetometer
There are two types of calibrations required for magnetometers: soft iron and hard iron calibration. Hard
iron calibration is considered to remove constant magnetic field affecting the sensor platform. When
graphing the output of a magnetometer in an ideal case, the output should be a perfect sphere in 3D
centered at (0,0,0), but this is usually not the case. Instead, it is centered in another x,y,z location. For
example, in Figure 7 the center lies in (34.5, -140.5, 46.5). These offsets were calculated by using
Equation 1 on the readings of the magnetometer on all three axes after moving the board in all different
angles.
Figure 7. Magnetometer Hard Iron Calibration
When calibrating the magnetometer, it is best to rotate the board in three different rotations as displayed in
Figure 8. While calibrating the magnetometer, the three graphs displayed in Figure 7 should be graphing a
circle, which allows for the minimum and maximum of each axis to be taken into account when calculating
the offsets. Soft iron calibration is required to eliminate the effects of electromagnetic fields, which causes
the ideal sphere to become an oval shape figure. Soft iron calibration is performed in the firmware after
the magnetometer values have been read and hard iron calibration has been applied.
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Figure 8. Rotations for Hard Iron Calibration of the Magnetometer
5
Conclusion
This section covers the power consumption of the sensor platform and the MSP430 requirements. The
voltage across a shunt resistor (26.63 Ω) connected to the VCC of the MSP430F5xx can be seen in
Figure 9. The voltage measurements were taken with the USB module disabled and low-power-mode 3
enabled when the MSP430F5xx was neither reading the sensors nor calculating the DCM algorithm. The
MSP430F5xx consumes ~ 5 µA in low-power-mode 3 and ~ 5.6 mA in active mode. The AHRS board
requires being battery powered when the transmission of the Euler angles is via BLE. The cycle area of
the voltage is 685.3 µVs, where each cycle is 20 ms. Therefore, the average voltage is 685.3 µVs / 20ms
= 34.265 mV. Using Equation 2, the average current consumption of the MSP430F5xx is 34.265 mV/
26.63 Ω ~ 1.28 mA.
D
Vavg
Vavg = Iavg * R ® Iavg =
R
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Conclusion
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Figure 9. MSP430 Voltage Measurement
Figure 9 shows the reading the motion sensors at different frequencies; the magnetometer (M) is read at a
10 Hz rate, while the accelerometer (A) and gyroscope (G) are read at 50 Hz. This figure shows the
MSP430F5xx using ~30% of the CPU. The accuracy of the MSP430 AHRS board is TBD. Table 2
includes the current consumption measurements for the different ICs in the AHRS board.
Table 2. System Current Consumption
Integrated Circuits (ICs)
Average Current Measurement
MSP430F5xx
1.06 mA
Accelerometer
(1)
(1)
0.14 mA
Gyroscope
6.5 mA
Barometric Pressure Sensor
0.65 mA
(1)
(1)
Magnetometer
0.1 mA
BLE Radio
30-mA worst case peak at 4 dBm
The current measurement values were obtained from the sensors’ datasheet.
MSP430 Requirements:
• RAM ~ 0.75 kB
• Flash ~ 11.7 kB
• CPU Usage ~ 21.34%
• SMCLK = 16 MHz, MCLK = 16 MHz, ACLK = REFO ~ 32.6 kHz
NOTE: The memory requirements include the DCM algorithm and exclude the USB Stack. IAR
Embedded Workbench 5.20.1 was the IDE used to benchmark.
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Schematics
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Schematics
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References
7
References
1.
2.
3.
4.
5.
14
www.ti.com
MSP430x5xx/MSP430x6xx Family User's Guide (SLAU208)
Direction Cosine Matrix IMU: Theory (http://gentlenav.googlecode.com/files/DCMDraft2.pdf)
CkDevices Open Source Firmware (http://www.ckdevices.com)
CkDevices Open Source Mongoose Visualizer (http://www.ckdevices.com)
Compensating for Tilt, Hard-Iron, and Soft-Iron Effects (http://www.sensorsmag.com/sensors/motionvelocity-displacement/compensating-tilt-hard-iron-and-soft-iron-effects-6475)
Nine-Axis Sensor Fusion Using the Direction Cosine Matrix Algorithm on the
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