tom dunigan
/
mpu9250
MPU9250 test with polling or ISR
Revision 1:0158e4d78423, committed 2018-11-19
- Comitter:
- manitou
- Date:
- Mon Nov 19 11:58:46 2018 +0000
- Parent:
- 0:31cc139b7d1e
- Commit message:
- format
Changed in this revision
MPU9250.h | Show annotated file Show diff for this revision Revisions of this file |
main.cpp | Show annotated file Show diff for this revision Revisions of this file |
diff -r 31cc139b7d1e -r 0158e4d78423 MPU9250.h --- a/MPU9250.h Sat Sep 10 14:15:19 2016 +0000 +++ b/MPU9250.h Mon Nov 19 11:58:46 2018 +0000 @@ -4,7 +4,7 @@ #include "mbed.h" #include "math.h" -#define USE_ISR 1 // poll or data ready interrupt +#define USE_ISR 0 // poll or data ready interrupt // See also MPU-9250 Register Map and Descriptions, Revision 4.0, RM-MPU-9250A-00, Rev. 1.4, 9/9/2013 for registers not listed in // above document; the MPU9250 and MPU9150 are virtually identical but the latter has a different register map
diff -r 31cc139b7d1e -r 0158e4d78423 main.cpp --- a/main.cpp Sat Sep 10 14:15:19 2016 +0000 +++ b/main.cpp Mon Nov 19 11:58:46 2018 +0000 @@ -1,17 +1,17 @@ /* MPU9250 Basic Example Code by: Kris Winer date: April 1, 2014 - license: Beerware - Use this code however you'd like. If you + license: Beerware - Use this code however you'd like. If you find it useful you can buy me a beer some time. - - Demonstrate basic MPU-9250 functionality including parameterizing the register addresses, initializing the sensor, - getting properly scaled accelerometer, gyroscope, and magnetometer data out. Added display functions to - allow display to on breadboard monitor. Addition of 9 DoF sensor fusion using open source Madgwick and + + Demonstrate basic MPU-9250 functionality including parameterizing the register addresses, initializing the sensor, + getting properly scaled accelerometer, gyroscope, and magnetometer data out. Added display functions to + allow display to on breadboard monitor. Addition of 9 DoF sensor fusion using open source Madgwick and Mahony filter algorithms. Sketch runs on the 3.3 V 8 MHz Pro Mini and the Teensy 3.1. - + SDA and SCL should have external pull-up resistors (to 3.3V). 10k resistors are on the EMSENSR-9250 breakout board. - + Hardware setup: MPU9250 Breakout --------- Arduino VDD ---------------------- 3.3V @@ -19,14 +19,14 @@ SDA ----------------------- A4 SCL ----------------------- A5 GND ---------------------- GND - - Note: The MPU9250 is an I2C sensor and uses the Arduino Wire library. + + Note: The MPU9250 is an I2C sensor and uses the Arduino Wire library. Because the sensor is not 5V tolerant, we are using a 3.3 V 8 MHz Pro Mini or a 3.3 V Teensy 3.1. We have disabled the internal pull-ups used by the Wire library in the Wire.h/twi.c utility file. We are also using the 400 kHz fast I2C mode by setting the TWI_FREQ to 400000L /twi.h utility file. */ - -//#include "ST_F401_84MHZ.h" + +//#include "ST_F401_84MHZ.h" //F401_init84 myinit(0); #include "mbed.h" #include "MPU9250.h" @@ -35,70 +35,69 @@ float sum = 0; uint32_t sumCount = 0; - MPU9250 mpu9250; - - Timer t; +MPU9250 mpu9250; - Serial pc(USBTX, USBRX); // tx, rx +Timer t; + +Serial pc(USBTX, USBRX); // tx, rx volatile bool newData = false; InterruptIn isrPin(D12); //k64 D12 dragon PD_0 -void mpuisr() { +void mpuisr() +{ newData=true; } - + int main() { - pc.baud(9600); + pc.baud(9600); + + //Set up I2C + i2c.frequency(400000); // use fast (400 kHz) I2C + + pc.printf("CPU SystemCoreClock is %d Hz\r\n", SystemCoreClock); + + t.start(); + isrPin.rise(&mpuisr); - //Set up I2C - i2c.frequency(400000); // use fast (400 kHz) I2C - - pc.printf("CPU SystemCoreClock is %d Hz\r\n", SystemCoreClock); - - t.start(); - isrPin.rise(&mpuisr); - - // Read the WHO_AM_I register, this is a good test of communication - uint8_t whoami = mpu9250.readByte(MPU9250_ADDRESS, WHO_AM_I_MPU9250); // Read WHO_AM_I register for MPU-9250 - pc.printf("I AM 0x%x\n\r", whoami); pc.printf("I SHOULD BE 0x71\n\r"); - - if (whoami == 0x71) // WHO_AM_I should always be 0x68 - { - pc.printf("MPU9250 is online...\n\r"); - wait(1); + // Read the WHO_AM_I register, this is a good test of communication + uint8_t whoami = mpu9250.readByte(MPU9250_ADDRESS, WHO_AM_I_MPU9250); // Read WHO_AM_I register for MPU-9250 + pc.printf("I AM 0x%x\n\r", whoami); + pc.printf("I SHOULD BE 0x71\n\r"); + + if (whoami == 0x71) { // WHO_AM_I should always be 0x68 + pc.printf("MPU9250 is online...\n\r"); + wait(1); + - - mpu9250.resetMPU9250(); // Reset registers to default in preparation for device calibration - mpu9250.calibrateMPU9250(gyroBias, accelBias); // Calibrate gyro and accelerometers, load biases in bias registers - pc.printf("x gyro bias = %f\n\r", gyroBias[0]); - pc.printf("y gyro bias = %f\n\r", gyroBias[1]); - pc.printf("z gyro bias = %f\n\r", gyroBias[2]); - pc.printf("x accel bias = %f\n\r", accelBias[0]); - pc.printf("y accel bias = %f\n\r", accelBias[1]); - pc.printf("z accel bias = %f\n\r", accelBias[2]); - wait(2); - mpu9250.initMPU9250(); - pc.printf("MPU9250 initialized for active data mode....\n\r"); // Initialize device for active mode read of acclerometer, gyroscope, and temperature - mpu9250.initAK8963(magCalibration); - pc.printf("AK8963 initialized for active data mode....\n\r"); // Initialize device for active mode read of magnetometer - pc.printf("Accelerometer full-scale range = %f g\n\r", 2.0f*(float)(1<<Ascale)); - pc.printf("Gyroscope full-scale range = %f deg/s\n\r", 250.0f*(float)(1<<Gscale)); - if(Mscale == 0) pc.printf("Magnetometer resolution = 14 bits\n\r"); - if(Mscale == 1) pc.printf("Magnetometer resolution = 16 bits\n\r"); - if(Mmode == 2) pc.printf("Magnetometer ODR = 8 Hz\n\r"); - if(Mmode == 6) pc.printf("Magnetometer ODR = 100 Hz\n\r"); - wait(2); - } - else - { - pc.printf("Could not connect to MPU9250: \n\r"); - pc.printf("%#x \n", whoami); + mpu9250.resetMPU9250(); // Reset registers to default in preparation for device calibration + mpu9250.calibrateMPU9250(gyroBias, accelBias); // Calibrate gyro and accelerometers, load biases in bias registers + pc.printf("x gyro bias = %f\n\r", gyroBias[0]); + pc.printf("y gyro bias = %f\n\r", gyroBias[1]); + pc.printf("z gyro bias = %f\n\r", gyroBias[2]); + pc.printf("x accel bias = %f\n\r", accelBias[0]); + pc.printf("y accel bias = %f\n\r", accelBias[1]); + pc.printf("z accel bias = %f\n\r", accelBias[2]); + wait(2); + mpu9250.initMPU9250(); + pc.printf("MPU9250 initialized for active data mode....\n\r"); // Initialize device for active mode read of acclerometer, gyroscope, and temperature + mpu9250.initAK8963(magCalibration); + pc.printf("AK8963 initialized for active data mode....\n\r"); // Initialize device for active mode read of magnetometer + pc.printf("Accelerometer full-scale range = %f g\n\r", 2.0f*(float)(1<<Ascale)); + pc.printf("Gyroscope full-scale range = %f deg/s\n\r", 250.0f*(float)(1<<Gscale)); + if(Mscale == 0) pc.printf("Magnetometer resolution = 14 bits\n\r"); + if(Mscale == 1) pc.printf("Magnetometer resolution = 16 bits\n\r"); + if(Mmode == 2) pc.printf("Magnetometer ODR = 8 Hz\n\r"); + if(Mmode == 6) pc.printf("Magnetometer ODR = 100 Hz\n\r"); + wait(2); + } else { + pc.printf("Could not connect to MPU9250: \n\r"); + pc.printf("%#x \n", whoami); - - while(1) ; // Loop forever if communication doesn't happen + + while(1) ; // Loop forever if communication doesn't happen } mpu9250.getAres(); // Get accelerometer sensitivity @@ -111,109 +110,109 @@ magbias[1] = +120.; // User environmental x-axis correction in milliGauss magbias[2] = +125.; // User environmental x-axis correction in milliGauss - while(1) { - static int readycnt=0; - // If intPin goes high, all data registers have new data - + while(1) { + static int readycnt=0; + // If intPin goes high, all data registers have new data + #if USE_ISR - if(newData) { - newData=false; - mpu9250.readByte(MPU9250_ADDRESS, INT_STATUS); //? need this with ISR + if(newData) { + newData=false; + mpu9250.readByte(MPU9250_ADDRESS, INT_STATUS); //? need this with ISR #else - if(mpu9250.readByte(MPU9250_ADDRESS, INT_STATUS) & 0x01) { // On interrupt, check if data ready interrupt + if(mpu9250.readByte(MPU9250_ADDRESS, INT_STATUS) & 0x01) { // On interrupt, check if data ready interrupt #endif - readycnt++; - mpu9250.readAccelData(accelCount); // Read the x/y/z adc values - // Now we'll calculate the accleration value into actual g's - ax = (float)accelCount[0]*aRes - accelBias[0]; // get actual g value, this depends on scale being set - ay = (float)accelCount[1]*aRes - accelBias[1]; - az = (float)accelCount[2]*aRes - accelBias[2]; - - mpu9250.readGyroData(gyroCount); // Read the x/y/z adc values - // Calculate the gyro value into actual degrees per second - gx = (float)gyroCount[0]*gRes - gyroBias[0]; // get actual gyro value, this depends on scale being set - gy = (float)gyroCount[1]*gRes - gyroBias[1]; - gz = (float)gyroCount[2]*gRes - gyroBias[2]; - - mpu9250.readMagData(magCount); // Read the x/y/z adc values - // Calculate the magnetometer values in milliGauss - // Include factory calibration per data sheet and user environmental corrections - mx = (float)magCount[0]*mRes*magCalibration[0] - magbias[0]; // get actual magnetometer value, this depends on scale being set - my = (float)magCount[1]*mRes*magCalibration[1] - magbias[1]; - mz = (float)magCount[2]*mRes*magCalibration[2] - magbias[2]; - } - - Now = t.read_us(); - deltat = (float)((Now - lastUpdate)/1000000.0f) ; // set integration time by time elapsed since last filter update - lastUpdate = Now; - - sum += deltat; - sumCount++; - + readycnt++; + mpu9250.readAccelData(accelCount); // Read the x/y/z adc values + // Now we'll calculate the accleration value into actual g's + ax = (float)accelCount[0]*aRes - accelBias[0]; // get actual g value, this depends on scale being set + ay = (float)accelCount[1]*aRes - accelBias[1]; + az = (float)accelCount[2]*aRes - accelBias[2]; + + mpu9250.readGyroData(gyroCount); // Read the x/y/z adc values + // Calculate the gyro value into actual degrees per second + gx = (float)gyroCount[0]*gRes - gyroBias[0]; // get actual gyro value, this depends on scale being set + gy = (float)gyroCount[1]*gRes - gyroBias[1]; + gz = (float)gyroCount[2]*gRes - gyroBias[2]; + + mpu9250.readMagData(magCount); // Read the x/y/z adc values + // Calculate the magnetometer values in milliGauss + // Include factory calibration per data sheet and user environmental corrections + mx = (float)magCount[0]*mRes*magCalibration[0] - magbias[0]; // get actual magnetometer value, this depends on scale being set + my = (float)magCount[1]*mRes*magCalibration[1] - magbias[1]; + mz = (float)magCount[2]*mRes*magCalibration[2] - magbias[2]; + } + + Now = t.read_us(); + deltat = (float)((Now - lastUpdate)/1000000.0f) ; // set integration time by time elapsed since last filter update + lastUpdate = Now; + + sum += deltat; + sumCount++; + // if(lastUpdate - firstUpdate > 10000000.0f) { // beta = 0.04; // decrease filter gain after stabilized // zeta = 0.015; // increasey bias drift gain after stabilized - // } - - // Pass gyro rate as rad/s - uint32_t us = t.read_us(); - mpu9250.MadgwickQuaternionUpdate(ax, ay, az, gx*PI/180.0f, gy*PI/180.0f, gz*PI/180.0f, my, mx, mz); - us = t.read_us()-us; - // mpu9250.MahonyQuaternionUpdate(ax, ay, az, gx*PI/180.0f, gy*PI/180.0f, gz*PI/180.0f, my, mx, mz); +// } + + // Pass gyro rate as rad/s + uint32_t us = t.read_us(); + mpu9250.MadgwickQuaternionUpdate(ax, ay, az, gx*PI/180.0f, gy*PI/180.0f, gz*PI/180.0f, my, mx, mz); + us = t.read_us()-us; +// mpu9250.MahonyQuaternionUpdate(ax, ay, az, gx*PI/180.0f, gy*PI/180.0f, gz*PI/180.0f, my, mx, mz); - // Serial print and/or display at 0.5 s rate independent of data rates - delt_t = t.read_ms() - count; - if (delt_t > 500) { // update LCD once per half-second independent of read rate - pc.printf("readycnt %d us %d\n",readycnt,us); - readycnt=0; - pc.printf("ax = %f", 1000*ax); - pc.printf(" ay = %f", 1000*ay); - pc.printf(" az = %f mg\n\r", 1000*az); + // Serial print and/or display at 0.5 s rate independent of data rates + delt_t = t.read_ms() - count; + if (delt_t > 500) { // update LCD once per half-second independent of read rate + pc.printf("readycnt %d us %d\n",readycnt,us); + readycnt=0; + pc.printf("ax = %f", 1000*ax); + pc.printf(" ay = %f", 1000*ay); + pc.printf(" az = %f mg\n\r", 1000*az); + + pc.printf("gx = %f", gx); + pc.printf(" gy = %f", gy); + pc.printf(" gz = %f deg/s\n\r", gz); + + pc.printf("gx = %f", mx); + pc.printf(" gy = %f", my); + pc.printf(" gz = %f mG\n\r", mz); + + tempCount = mpu9250.readTempData(); // Read the adc values + temperature = ((float) tempCount) / 333.87f + 21.0f; // Temperature in degrees Centigrade + pc.printf("temperature = %f C\n\r", temperature); - pc.printf("gx = %f", gx); - pc.printf(" gy = %f", gy); - pc.printf(" gz = %f deg/s\n\r", gz); - - pc.printf("gx = %f", mx); - pc.printf(" gy = %f", my); - pc.printf(" gz = %f mG\n\r", mz); - - tempCount = mpu9250.readTempData(); // Read the adc values - temperature = ((float) tempCount) / 333.87f + 21.0f; // Temperature in degrees Centigrade - pc.printf("temperature = %f C\n\r", temperature); - - pc.printf("q0 = %f\n\r", q[0]); - pc.printf("q1 = %f\n\r", q[1]); - pc.printf("q2 = %f\n\r", q[2]); - pc.printf("q3 = %f\n\r", q[3]); + pc.printf("q0 = %f\n\r", q[0]); + pc.printf("q1 = %f\n\r", q[1]); + pc.printf("q2 = %f\n\r", q[2]); + pc.printf("q3 = %f\n\r", q[3]); + + - - - // Define output variables from updated quaternion---these are Tait-Bryan angles, commonly used in aircraft orientation. - // In this coordinate system, the positive z-axis is down toward Earth. - // Yaw is the angle between Sensor x-axis and Earth magnetic North (or true North if corrected for local declination, looking down on the sensor positive yaw is counterclockwise. - // Pitch is angle between sensor x-axis and Earth ground plane, toward the Earth is positive, up toward the sky is negative. - // Roll is angle between sensor y-axis and Earth ground plane, y-axis up is positive roll. - // These arise from the definition of the homogeneous rotation matrix constructed from quaternions. - // Tait-Bryan angles as well as Euler angles are non-commutative; that is, the get the correct orientation the rotations must be - // applied in the correct order which for this configuration is yaw, pitch, and then roll. - // For more see http://en.wikipedia.org/wiki/Conversion_between_quaternions_and_Euler_angles which has additional links. - yaw = atan2(2.0f * (q[1] * q[2] + q[0] * q[3]), q[0] * q[0] + q[1] * q[1] - q[2] * q[2] - q[3] * q[3]); - pitch = -asin(2.0f * (q[1] * q[3] - q[0] * q[2])); - roll = atan2(2.0f * (q[0] * q[1] + q[2] * q[3]), q[0] * q[0] - q[1] * q[1] - q[2] * q[2] + q[3] * q[3]); - pitch *= 180.0f / PI; - yaw *= 180.0f / PI; - yaw -= 13.8f; // Declination at Danville, California is 13 degrees 48 minutes and 47 seconds on 2014-04-04 - roll *= 180.0f / PI; + // Define output variables from updated quaternion---these are Tait-Bryan angles, commonly used in aircraft orientation. + // In this coordinate system, the positive z-axis is down toward Earth. + // Yaw is the angle between Sensor x-axis and Earth magnetic North (or true North if corrected for local declination, looking down on the sensor positive yaw is counterclockwise. + // Pitch is angle between sensor x-axis and Earth ground plane, toward the Earth is positive, up toward the sky is negative. + // Roll is angle between sensor y-axis and Earth ground plane, y-axis up is positive roll. + // These arise from the definition of the homogeneous rotation matrix constructed from quaternions. + // Tait-Bryan angles as well as Euler angles are non-commutative; that is, the get the correct orientation the rotations must be + // applied in the correct order which for this configuration is yaw, pitch, and then roll. + // For more see http://en.wikipedia.org/wiki/Conversion_between_quaternions_and_Euler_angles which has additional links. + yaw = atan2(2.0f * (q[1] * q[2] + q[0] * q[3]), q[0] * q[0] + q[1] * q[1] - q[2] * q[2] - q[3] * q[3]); + pitch = -asin(2.0f * (q[1] * q[3] - q[0] * q[2])); + roll = atan2(2.0f * (q[0] * q[1] + q[2] * q[3]), q[0] * q[0] - q[1] * q[1] - q[2] * q[2] + q[3] * q[3]); + pitch *= 180.0f / PI; + yaw *= 180.0f / PI; + yaw -= 13.8f; // Declination at Danville, California is 13 degrees 48 minutes and 47 seconds on 2014-04-04 + roll *= 180.0f / PI; - pc.printf("Yaw, Pitch, Roll: %f %f %f\n\r", yaw, pitch, roll); - pc.printf("average rate = %f\n\r", (float) sumCount/sum); - - myled= !myled; - count = t.read_ms(); - sum = 0; - sumCount = 0; -} -} - - } \ No newline at end of file + pc.printf("Yaw, Pitch, Roll: %f %f %f\n\r", yaw, pitch, roll); + pc.printf("average rate = %f\n\r", (float) sumCount/sum); + + myled= !myled; + count = t.read_ms(); + sum = 0; + sumCount = 0; + } + } + +} \ No newline at end of file