Changing about IMU

Dependencies:   Servo mbed-rtos mbed

Fork of TurtleBot_V1 by TurtleBot

Files at this revision

API Documentation at this revision

Comitter:
worasuchad
Date:
Fri Mar 23 18:32:18 2018 +0000
Parent:
2:d4bd9ff10e8e
Commit message:
edit and test IMU

Changed in this revision

attitude.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
mbed.bld Show annotated file Show diff for this revision Revisions of this file
--- /dev/null	Thu Jan 01 00:00:00 1970 +0000
+++ b/attitude.h	Fri Mar 23 18:32:18 2018 +0000
@@ -0,0 +1,81 @@
+#include "MPU9250.h"
+
+MPU9250 mpu9250;
+
+Timer t;
+
+void attitude_setup(void)
+{
+    i2c.frequency(400000);  // use fast (400 kHz) I2C
+    
+    t.start();
+
+    // 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
+    
+
+    if (whoami == 0x73) { // WHO_AM_I should always be 0x68
+        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
+        wait(2);
+        mpu9250.initMPU9250();
+        mpu9250.initAK8963(magCalibration);
+        wait(2);
+    } else while(1) ; // Loop forever if communication doesn't happen
+
+    mpu9250.getAres(); // Get accelerometer sensitivity
+    mpu9250.getGres(); // Get gyro sensitivity
+    mpu9250.getMres(); // Get magnetometer sensitivity
+
+    magbias[0] = +470.;  // User environmental x-axis correction in milliGauss, should be automatically calculated
+    magbias[1] = +120.;  // User environmental x-axis correction in milliGauss
+    magbias[2] = +125.;  // User environmental x-axis correction in milliGauss
+}
+
+int attitude_get(void)
+{
+    // If intPin goes high, all data registers have new data
+    if(mpu9250.readByte(MPU9250_ADDRESS, INT_STATUS) & 0x01) {  // On interrupt, check if data ready interrupt
+
+        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;
+
+        // Pass gyro rate as rad/s
+        mpu9250.MadgwickQuaternionUpdate(ax, ay, az, gx*PI/180.0f, gy*PI/180.0f, gz*PI/180.0f,  my,  mx, mz);
+        mpu9250.MahonyQuaternionUpdate(ax, ay, az, gx*PI/180.0f, gy*PI/180.0f, gz*PI/180.0f, my, mx, mz);
+
+        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;
+
+        return 0;
+    }
+    return -1;
+}
+
--- a/main.cpp	Fri Mar 23 16:25:17 2018 +0000
+++ b/main.cpp	Fri Mar 23 18:32:18 2018 +0000
@@ -19,6 +19,8 @@
 
 /////////////////////////   IMU   ////////////////////////////////
 //////////////////////////////////////////////////////////////////
+#include "attitude.h"
+/*
 #include "MPU9250.h"
 
 float sum = 0;
@@ -28,7 +30,7 @@
 
 MPU9250 mpu9250;
 Timer t;
-
+*/
 
 ///////////////////////// Servo   ////////////////////////////////
 //////////////////////////////////////////////////////////////////
@@ -58,9 +60,10 @@
 //////////////////////////////////////////////////////////////////
 int main()
 {
+
+    IMU();
     thread1.start(myservoLeft);
     thread2.start(myservoRight);
-    IMU();
 /*    while(1) 
     {
         printf("Hello World! Turtlebot is READY\n");
@@ -199,182 +202,13 @@
 
 /////////////////////////      IMU         ///////////////////////
 //////////////////////////////////////////////////////////////////
+
 void IMU()
 {
-    //Set up I2C
-    i2c.frequency(400000);  // use fast (400 kHz) I2C  
-  
-    //pc.printf("CPU SystemCoreClock is %d Hz\r\n", SystemCoreClock);   
-    t.start();        
-      
-    // 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 0x68\n\r");
-  
-    if (whoami == 0x73 ) // WHO_AM_I should always be 0x68
-    {  
-        //pc.printf("MPU9250 WHO_AM_I is 0x%x\n\r", whoami);
-        //pc.printf("MPU9250 is online...\n\r");
-        sprintf(buffer, "0x%x", whoami);  
-        wait(1);
-    
-        mpu9250.resetMPU9250(); // Reset registers to default in preparation for device calibration
-        mpu9250.MPU9250SelfTest(SelfTest); // Start by performing self test and reporting values
-        pc.printf("x-axis self test: acceleration trim within : %f % of factory value\n\r", SelfTest[0]);  
-        pc.printf("y-axis self test: acceleration trim within : %f % of factory value\n\r", SelfTest[1]);  
-        pc.printf("z-axis self test: acceleration trim within : %f % of factory value\n\r", SelfTest[2]);  
-        pc.printf("x-axis self test: gyration trim within : %f % of factory value\n\r", SelfTest[3]);  
-        pc.printf("y-axis self test: gyration trim within : %f % of factory value\n\r", SelfTest[4]);  
-        pc.printf("z-axis self test: gyration trim within : %f % of factory value\n\r", SelfTest[5]);  
-        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(1);
-    }
-    else
+    attitude_setup();
+    while(1)
     {
-        pc.printf("Could not connect to MPU9250: \n\r");
-        pc.printf("%#x \n",  whoami);
- 
-        sprintf(buffer, "WHO_AM_I 0x%x", whoami); 
- 
-        while(1) ; // Loop forever if communication doesn't happen
-        }
-
-            mpu9250.getAres(); // Get accelerometer sensitivity
-            mpu9250.getGres(); // Get gyro sensitivity
-            mpu9250.getMres(); // Get magnetometer sensitivity
-            pc.printf("Accelerometer sensitivity is %f LSB/g \n\r", 1.0f/aRes);
-            pc.printf("Gyroscope sensitivity is %f LSB/deg/s \n\r", 1.0f/gRes);
-            pc.printf("Magnetometer sensitivity is %f LSB/G \n\r", 1.0f/mRes);
-            magbias[0] = +470.;  // User environmental x-axis correction in milliGauss, should be automatically calculated
-            magbias[1] = +120.;  // User environmental x-axis correction in milliGauss
-            magbias[2] = +125.;  // User environmental x-axis correction in milliGauss
-
-
-            while(1) 
-            {
-                // If intPin goes high, all data registers have new data
-                if(mpu9250.readByte(MPU9250_ADDRESS, INT_STATUS) & 0x01) {  // On interrupt, check if data ready interrupt
-
-                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
-            mpu9250.MadgwickQuaternionUpdate(ax, ay, az, gx*PI/180.0f, gy*PI/180.0f, gz*PI/180.0f,  my,  mx, mz);
-            //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 > 10) 
-            { // update LCD once per half-second independent of read rate
-
-                //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("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
-                yaw   += 0.8f; 
-                roll  *= 180.0f / PI;
-
-                pc.printf("%f  %f  %f  %f \n\r",roll, pitch, yaw,origin);
-                //pc.printf("average rate = %f\n\r", (float) sumCount/sum);
-                //sprintf(buffer, "YPR: %f %f %f", yaw, pitch, roll);
-                //lcd.printString(buffer, 0, 4);
-                //sprintf(buffer, "rate = %f", (float) sumCount/sum);
-                //lcd.printString(buffer, 0, 5);
-    
-                myled= !myled;
-                count = t.read_ms(); 
-
-                if(count > 1<<21) 
-                {
-                    t.start(); // start the timer over again if ~30 minutes has passed
-                    count = 0;
-                    deltat= 0;
-                    lastUpdate = t.read_us();
-                }
-                sum = 0;
-                sumCount = 0; 
-            }
-        }
-}
\ No newline at end of file
+        attitude_get();
+        pc.printf("%.0f  %.0f  %.0f \n\r",  roll,   pitch, yaw );
+    }
+}
--- a/mbed.bld	Fri Mar 23 16:25:17 2018 +0000
+++ b/mbed.bld	Fri Mar 23 18:32:18 2018 +0000
@@ -1,1 +1,1 @@
-https://os.mbed.com/users/mbed_official/code/mbed/builds/7130f322cb7e
\ No newline at end of file
+http://mbed.org/users/mbed_official/code/mbed/builds/994bdf8177cb
\ No newline at end of file