Revision 1:411d267f9d32, committed 2019-10-04

Comitter:

iforce2d

Date:

Fri Oct 04 17:04:41 2019 +0000

Parent:

0:f76c26307f9a

Commit message:

First commit

Changed in this revision

diff -r f76c26307f9a -r 411d267f9d32 PPM.cpp
--- /dev/null	Thu Jan 01 00:00:00 1970 +0000
+++ b/PPM.cpp	Fri Oct 04 17:04:41 2019 +0000
@@ -0,0 +1,27 @@
+#include "mbed.h"
+#include "PPM.h"
+ 
+PPM::PPM(PinName pin): ppm(pin)
+{
+    for (int i = 0; i < NUM_CHANNELS; i++)
+        channels[i] = 1500;
+    currentChannel = 0;    
+    timer.start();
+    ppm.rise( callback(this, &PPM::rise) );
+}
+            
+void PPM::rise()
+{
+    uint16_t time = timer.read_us();
+    timer.reset();
+    
+    if ( time > 2500 )
+    {
+       currentChannel = 0;
+    }
+    else if ( currentChannel < NUM_CHANNELS )
+    {
+        channels[currentChannel] = time;
+        currentChannel++;
+    }
+}
\ No newline at end of file

diff -r f76c26307f9a -r 411d267f9d32 PPM.h
--- /dev/null	Thu Jan 01 00:00:00 1970 +0000
+++ b/PPM.h	Fri Oct 04 17:04:41 2019 +0000
@@ -0,0 +1,20 @@
+#ifndef PPM_IN
+#define PPM_IN
+ 
+class PPM
+{
+    public:    
+        static const uint8_t NUM_CHANNELS = 6;
+        uint16_t channels[NUM_CHANNELS];
+        
+        PPM(PinName pin);
+        
+        void rise();
+ 
+    protected:
+        InterruptIn ppm;
+        Timer timer;
+        uint8_t currentChannel;
+};
+ 
+#endif
\ No newline at end of file

diff -r f76c26307f9a -r 411d267f9d32 main.cpp
--- a/main.cpp	Thu Feb 14 17:24:48 2013 +0000
+++ b/main.cpp	Fri Oct 04 17:04:41 2019 +0000
@@ -1,25 +1,483 @@
 #include "mbed.h"
- 
-// Read temperature from LM75BD
+#include "PPM.h"
+
+I2C i2c(PB_11, PB_10);  // sda, scl
+Serial pc(PA_9, PA_10, 115200); // tx, rx
+DigitalOut led_green(PB_3);
+DigitalOut led_red(PB_4);
+PPM ppm(PA_0);
+
+DigitalOut motorPin1(PA_8);
+DigitalOut motorPin2(PA_11);
+DigitalOut motorPin3(PB_6);
+DigitalOut motorPin4(PB_7);
+DigitalOut motorPin5(PB_8);
+DigitalOut motorPin6(PB_9);
+
+DigitalOut buzzer(PA_12);
+
+#define ROLL  0
+#define PITCH 1
+#define YAW   2
+
+#define RC_ROLL      (ppm.channels[0])
+#define RC_PITCH     (ppm.channels[1])
+#define RC_THROTTLE  (ppm.channels[2])
+#define RC_YAW       (ppm.channels[3])
+#define RC_DEADBAND_US 8
+
+#define GYRO_CALIB_SAMPLES 4000
+#define MPU6050 (0x68 << 1)
+
+float pid_p_gain_roll = 1.3;               //Gain setting for the roll P-controller
+float pid_i_gain_roll = 0.04;              //Gain setting for the roll I-controller
+float pid_d_gain_roll = 18.0;              //Gain setting for the roll D-controller
+int pid_max_roll = 400;                    //Maximum output of the PID-controller (+/-)
+
+float pid_p_gain_pitch = pid_p_gain_roll;  //Gain setting for the pitch P-controller.
+float pid_i_gain_pitch = pid_i_gain_roll;  //Gain setting for the pitch I-controller.
+float pid_d_gain_pitch = pid_d_gain_roll;  //Gain setting for the pitch D-controller.
+int pid_max_pitch = pid_max_roll;          //Maximum output of the PID-controller (+/-)
+
+float pid_p_gain_yaw = 4.0;                //Gain setting for the pitch P-controller. //4.0
+float pid_i_gain_yaw = 0.02;               //Gain setting for the pitch I-controller. //0.02
+float pid_d_gain_yaw = 0.0;                //Gain setting for the pitch D-controller.
+int pid_max_yaw = 400;                     //Maximum output of the PID-controller (+/-)
+
+int cal_int;
+double gyro_cal[3];
+int16_t acc_raw[3], gyro_raw[3];
+float acc_smoothed[3], gyro_smoothed[3];
+
+Timer armingTimer;
+
+Timer timer;
+
+float angle_roll_acc, angle_pitch_acc, angle_pitch, angle_roll;
+float acc_total_vector;
+
+float roll_level_adjust, pitch_level_adjust;
+float pid_i_mem_roll, pid_roll_setpoint, pid_output_roll, pid_last_roll_d_error;
+float pid_i_mem_pitch, pid_pitch_setpoint, pid_output_pitch, pid_last_pitch_d_error;
+float pid_i_mem_yaw, pid_yaw_setpoint, pid_output_yaw, pid_last_yaw_d_error;
+
+int constrain( int val, int lower, int upper )
+{
+    if ( val < lower ) return lower;
+    if ( val > upper ) return upper;
+    return val;
+}
+
+void beepStart() 
+{
+    buzzer = 0;
+}
+
+void beepStop() 
+{
+    buzzer = 1;
+}
+
+void beep(int ms) 
+{
+    beepStart();
+    wait_ms(ms);
+    beepStop();
+}
+
+void setIMURegisters() 
+{    
+    char cmd[2];
+    
+    cmd[0] = 0x6B;                                                          //We want to write to the PWR_MGMT_1 register (6B hex)
+    cmd[1] = 0x00;                                                          //Set the register bits as 00000000 to activate the gyro
+    i2c.write(MPU6050, cmd, 2);
+    
+    cmd[0] = 0x1B;                                                          //We want to write to the GYRO_CONFIG register (1B hex)
+    cmd[1] = 0x08;                                                          //Set the register bits as 00001000 (500dps full scale)
+    i2c.write(MPU6050, cmd, 2);
+    
+    cmd[0] = 0x1C;                                                          //We want to write to the ACCEL_CONFIG register (1A hex)
+    cmd[1] = 0x10;                                                          //Set the register bits as 00010000 (+/- 8g full scale range)
+    i2c.write(MPU6050, cmd, 2);
+    
+    //Let's perform a random register check to see if the values are written correct
+    cmd[0] = 0x1B;                                                          //Start reading at register 0x1B
+    i2c.write(MPU6050, cmd, 1);    
+    i2c.read(MPU6050, cmd, 1);
+    if (cmd[0] != 0x08) {                                                   //Check if the value is 0x08
+        led_red = 0;                                                        //Turn on the warning led
+        pc.printf("Gyro init failed! (%d)\n", cmd[0]);
+        while (true)
+            wait(1);                                                      //Stay in this loop for ever
+    }
+    
+    cmd[0] = 0x1A;                                                          //We want to write to the CONFIG register (1A hex)
+    cmd[1] = 0x03;                                                          //Set the register bits as 00000011 (Set Digital Low Pass Filter to ~43Hz)
+    i2c.write(MPU6050, cmd, 2);
+}
+
+void readIMU(bool calibrated = true)
+{    
+    char cmd[14];
 
-I2C i2c(p28, p27);
+    cmd[0] = 0x3B;                                                          //Start reading at register 43h and auto increment with every read.
+    i2c.write(MPU6050, cmd, 1);
+    i2c.read(MPU6050, cmd, 14);                                             //Read 14 bytes from the gyro.
+    
+    acc_raw[0] = (cmd[0] << 8) | cmd[1];                               //Add the low and high byte to the acc_x variable.
+    acc_raw[1] = (cmd[2] << 8) | cmd[3];                               //Add the low and high byte to the acc_y variable.
+    acc_raw[2] = (cmd[4] << 8) | cmd[5];                               //Add the low and high byte to the acc_z variable.
+    
+    gyro_raw[0] = (cmd[8] << 8) |  cmd[9];                              //Read high and low part of the angular data.
+    gyro_raw[1] = (cmd[10] << 8) | cmd[11];                              //Read high and low part of the angular data.
+    gyro_raw[2] = (cmd[12] << 8) | cmd[13];                              //Read high and low part of the angular data.
+    
+    if ( calibrated ) {
+        for (int i = 0; i < 3; i++)
+            gyro_raw[i] -= gyro_cal[i];                                       
+    }
+}
+
+void calibrateGyro() 
+{
+    for (int i = 0; i < 3; i++) 
+        gyro_cal[i] = 0;
+    
+    for (int s = 0; s < GYRO_CALIB_SAMPLES; s++) {                            //Take GYRO_CALIB_SAMPLES readings for calibration.
+        if (s % 50 == 0)
+            led_green = 1 - led_green;                                          //Change the led status to indicate calibration.
+        readIMU(false);                                                        //Read the gyro output.
+        for (int i = 0; i < 3; i++)
+            gyro_cal[i] += gyro_raw[i];                                       //Ad roll value to gyro_roll_cal.
+        wait_us(3);                                                               //Wait 3 milliseconds before the next loop.
+    }
+    
+    for (int i = 0; i < 3; i++)
+        gyro_cal[i] /= (float)GYRO_CALIB_SAMPLES;                                                 //Divide the roll total by GYRO_CALIB_SAMPLES.
+}
 
-const int addr = 0x90;
+bool checkArmStateChange(bool armed) 
+{
+    static int armingState = 0;
+    
+    if ( RC_THROTTLE > 1100 )
+        return false;
+    
+    if ( ! armed && RC_YAW > 1900 ) {
+        if ( armingState == 0 ) {
+            armingState = 1;
+            armingTimer.reset();
+            armingTimer.start();
+            pc.printf("Started arming\n");
+        }
+        else {
+            uint16_t time = armingTimer.read_ms();
+            if ( time > 2000 ) {
+                armed = true;
+                armingState = 0;
+                pc.printf("ARMED\n");
+                //beep(300);
+                return true;
+            }
+        }
+    }
+    else if ( armed && RC_YAW < 1100 ) {
+        if ( armingState == 0 ) {
+            armingState = -1;
+            armingTimer.reset();
+            armingTimer.start();
+            pc.printf("Started disarming\n");
+        }
+        else {
+            uint16_t time = armingTimer.read_ms();
+            if ( time > 2000 ) {
+                armed = false;
+                armingState = 0;
+                pc.printf("DISARMED\n");
+                //beep(50);
+                //wait_ms(50);
+                //beep(50);
+                return false;
+            }
+        }
+    }
+    else {
+        armingState = 0;
+        armingTimer.reset();
+    }
+    
+    return armed;
+}
+
+bool getAutoLevelState()
+{
+    return ppm.channels[5] > 1600;
+}
+
+int afterDeadband(int in)
+{
+    int lower = 1500 - RC_DEADBAND_US;
+    int upper = 1500 + RC_DEADBAND_US;
+    if ( in < lower )
+        return in - lower;
+    if ( in > upper )
+        return in - upper;
+    return 0;
+}
+
+void resetPID()
+{
+    pid_i_mem_roll = 0;
+    pid_last_roll_d_error = 0;
+    pid_i_mem_pitch = 0;
+    pid_last_pitch_d_error = 0;
+    pid_i_mem_yaw = 0;
+    pid_last_yaw_d_error = 0;
+}
+
+void calculatePID()
+{
+    //Roll calculations
+    float pid_error_temp = gyro_smoothed[ROLL] - pid_roll_setpoint;
+    pid_i_mem_roll += pid_i_gain_roll * pid_error_temp;
+    if(pid_i_mem_roll > pid_max_roll)pid_i_mem_roll = pid_max_roll;
+    else if(pid_i_mem_roll < pid_max_roll * -1)pid_i_mem_roll = pid_max_roll * -1;
+    
+    pid_output_roll = pid_p_gain_roll * pid_error_temp + pid_i_mem_roll + pid_d_gain_roll * (pid_error_temp - pid_last_roll_d_error);
+    if(pid_output_roll > pid_max_roll)pid_output_roll = pid_max_roll;
+    else if(pid_output_roll < pid_max_roll * -1)pid_output_roll = pid_max_roll * -1;
+    
+    pid_last_roll_d_error = pid_error_temp;
+    
+    //Pitch calculations
+    pid_error_temp = gyro_smoothed[PITCH] - pid_pitch_setpoint;
+    pid_i_mem_pitch += pid_i_gain_pitch * pid_error_temp;
+    if(pid_i_mem_pitch > pid_max_pitch)pid_i_mem_pitch = pid_max_pitch;
+    else if(pid_i_mem_pitch < pid_max_pitch * -1)pid_i_mem_pitch = pid_max_pitch * -1;
+    
+    pid_output_pitch = pid_p_gain_pitch * pid_error_temp + pid_i_mem_pitch + pid_d_gain_pitch * (pid_error_temp - pid_last_pitch_d_error);
+    if(pid_output_pitch > pid_max_pitch)pid_output_pitch = pid_max_pitch;
+    else if(pid_output_pitch < pid_max_pitch * -1)pid_output_pitch = pid_max_pitch * -1;
+    
+    pid_last_pitch_d_error = pid_error_temp;
+    
+    //Yaw calculations
+    pid_error_temp = gyro_smoothed[YAW] - pid_yaw_setpoint;
+    pid_i_mem_yaw += pid_i_gain_yaw * pid_error_temp;
+    if(pid_i_mem_yaw > pid_max_yaw)pid_i_mem_yaw = pid_max_yaw;
+    else if(pid_i_mem_yaw < pid_max_yaw * -1)pid_i_mem_yaw = pid_max_yaw * -1;
+    
+    pid_output_yaw = pid_p_gain_yaw * pid_error_temp + pid_i_mem_yaw + pid_d_gain_yaw * (pid_error_temp - pid_last_yaw_d_error);
+    if(pid_output_yaw > pid_max_yaw)pid_output_yaw = pid_max_yaw;
+    else if(pid_output_yaw < pid_max_yaw * -1)pid_output_yaw = pid_max_yaw * -1;
+    
+    pid_last_yaw_d_error = pid_error_temp;
+}
 
 int main() {
-    char cmd[2];
-    while (1) {
-        cmd[0] = 0x01;
-        cmd[1] = 0x00;
-        i2c.write(addr, cmd, 2);
- 
-        wait(0.5);
- 
-        cmd[0] = 0x00;
-        i2c.write(addr, cmd, 1);
-        i2c.read(addr, cmd, 2);
- 
-        float tmp = (float((cmd[0]<<8)|cmd[1]) / 256.0);
-        printf("Temp = %.2f\n", tmp);
+    
+    i2c.frequency(400000);
+    
+    buzzer = 1;
+    led_red = 1;
+    led_green = 1;
+    
+    motorPin1 = 0;
+    motorPin2 = 0;
+    motorPin3 = 0;
+    motorPin4 = 0;
+    motorPin5 = 0;
+    motorPin6 = 0;
+    
+    armingTimer.reset();
+    
+    beep(50);
+        
+    pc.printf("setIMURegisters\n");    
+    setIMURegisters();
+    
+    pc.printf("calibrateGyro\n");
+    calibrateGyro();
+    
+    pc.printf("Finished gyro calibration (%f, %f, %f)\n", gyro_cal[0], gyro_cal[1], gyro_cal[2]);
+    
+    timer.reset();
+    timer.start();
+    
+    for (int i = 0; i < 3; i++)
+        gyro_smoothed[i] = 0;
+    angle_pitch = 0;
+    angle_roll = 0;
+        
+    beep(50);
+    wait_ms(50);
+    beep(50);
+    
+    bool armed = false;
+    bool armedLastTime = armed;
+    
+    bool autoLevel = getAutoLevelState();
+    bool autoLevelLastTime = autoLevel;
+    
+    unsigned long oneShotCounter = 0;
+    
+    unsigned long loopCounter = 0;
+    
+    float initialAccUptake = 0.8;
+    
+    while (true) {
+        
+        //pc.printf("Gyro (%f, %f, %f)\n", gyro_smoothed[0], gyro_smoothed[1], gyro_smoothed[2]);
+        //pc.printf("Accel (%f, %f)\n", angle_pitch, angle_roll);
+        
+        armed = checkArmStateChange(armed);
+        led_green = ! armed;
+        
+        if ( ! armedLastTime && armed )
+            resetPID();
+        if ( armed != armedLastTime ) {
+            oneShotCounter = 20;
+            beepStart();
+        }
+        armedLastTime = armed;
+        
+        autoLevel = getAutoLevelState();
+        if ( autoLevel != autoLevelLastTime ) {
+            oneShotCounter = 4;
+            beepStart();
+        }
+        autoLevelLastTime = autoLevel;
+        
+        if ( oneShotCounter > 0 ) {
+            if ( --oneShotCounter == 0 ) {
+                beepStop();
+            }
+        }
+        
+        const float uptake = 0.3;
+        for (int i = 0; i < 3; i++)
+            gyro_smoothed[i] = (gyro_smoothed[i] * (1-uptake)) + ((gyro_raw[i] / 65.5) * uptake);   //Gyro pid input is deg/sec.
+            
+            
+        //Gyro angle calculations
+        //0.0000611 = 1 / (250Hz / 65.5)
+        angle_pitch += gyro_raw[ROLL] * 0.0000611;                                    //Calculate the traveled pitch angle and add this to the angle_pitch variable.
+        angle_roll += gyro_raw[PITCH] * 0.0000611;                                      //Calculate the traveled roll angle and add this to the angle_roll variable.
+        
+        //0.000001066 = 0.0000611 * (3.142(PI) / 180degr) The Arduino sin function is in radians
+        float new_angle_pitch = angle_pitch + angle_roll * sin(gyro_raw[YAW] * 0.000001066);                  //If the IMU has yawed transfer the roll angle to the pitch angel.
+        angle_roll -= angle_pitch * sin(gyro_raw[YAW] * 0.000001066);                  //If the IMU has yawed transfer the pitch angle to the roll angel.
+        angle_pitch = new_angle_pitch;
+        
+        //Accelerometer angle calculations
+        acc_total_vector = sqrtf((acc_raw[0]*acc_raw[0])+(acc_raw[1]*acc_raw[1])+(acc_raw[2]*acc_raw[2]));       //Calculate the total accelerometer vector.
+        
+        if (abs(acc_raw[PITCH]) < acc_total_vector) {                                        //Prevent the asin function to produce a NaN
+            angle_pitch_acc = asin((float)acc_raw[PITCH]/acc_total_vector)* 57.296;          //Calculate the pitch angle.
+        }
+        if (abs(acc_raw[ROLL]) < acc_total_vector) {                                        //Prevent the asin function to produce a NaN
+            angle_roll_acc = asin((float)acc_raw[ROLL]/acc_total_vector)* -57.296;          //Calculate the roll angle.
+        }
+        
+        //Place the MPU-6050 spirit level and note the values in the following two lines for calibration.
+        angle_pitch_acc -= 0.0;                                                   //Accelerometer calibration value for pitch.
+        angle_roll_acc -= 0.0;                                                    //Accelerometer calibration value for roll.
+        
+        initialAccUptake *= 0.98;
+        
+        float acc_uptake = 0.0004 + initialAccUptake;
+        angle_pitch = angle_pitch * (1-acc_uptake) + angle_pitch_acc * acc_uptake;            //Correct the drift of the gyro pitch angle with the accelerometer pitch angle.
+        angle_roll = angle_roll * (1-acc_uptake) + angle_roll_acc * acc_uptake;               //Correct the drift of the gyro roll angle with the accelerometer roll angle.
+        
+        pitch_level_adjust = angle_pitch * 15;                                    //Calculate the pitch angle correction
+        roll_level_adjust = angle_roll * 15;                                      //Calculate the roll angle correction
+        
+        if ( ! autoLevel ){                                                          //If the quadcopter is not in auto-level mode
+            pitch_level_adjust = 0;                                                 //Set the pitch angle correction to zero.
+            roll_level_adjust = 0;                                                  //Set the roll angle correcion to zero.
+        }
+            
+           
+           
+        //The PID set point in degrees per second is determined by the roll receiver input.
+        //In the case of deviding by 3 the max roll rate is aprox 164 degrees per second ( (500-8)/3 = 164d/s ).
+        pid_roll_setpoint = afterDeadband(RC_ROLL);        
+        pid_roll_setpoint -= roll_level_adjust;                                   //Subtract the angle correction from the standardized receiver roll input value.
+        pid_roll_setpoint /= 3.0;                                                 //Divide the setpoint for the PID roll controller by 3 to get angles in degrees.
+        
+        //The PID set point in degrees per second is determined by the pitch receiver input.
+        //In the case of deviding by 3 the max pitch rate is aprox 164 degrees per second ( (500-8)/3 = 164d/s ).
+        pid_pitch_setpoint = afterDeadband(RC_PITCH);        
+        pid_pitch_setpoint -= pitch_level_adjust;                                  //Subtract the angle correction from the standardized receiver pitch input value.
+        pid_pitch_setpoint /= 3.0;                                                 //Divide the setpoint for the PID pitch controller by 3 to get angles in degrees.
+        
+        //The PID set point in degrees per second is determined by the yaw receiver input.
+        //In the case of dividing by 3 the max yaw rate is aprox 164 degrees per second ( (500-8)/3 = 164d/s ).
+        pid_yaw_setpoint = 0;
+        //We need a little dead band of 16us for better results.
+        if (RC_THROTTLE > 1050) { //Do not yaw when turning off the motors.
+            pid_yaw_setpoint = afterDeadband(RC_YAW) / 3.0;
+        }
+        
+        calculatePID();           
+           
+        int pwm[6];
+        
+        if (armed) {                                                          //The motors are started.
+            int throttle = RC_THROTTLE;
+            if (throttle > 1800) 
+                throttle = 1800;                                   //We need some room to keep full control at full throttle.
+            pwm[0] = throttle - pid_output_pitch + pid_output_roll - pid_output_yaw; //Calculate the pulse for esc 1 (front-right - CCW)
+            pwm[1] = throttle + pid_output_pitch + pid_output_roll + pid_output_yaw; //Calculate the pulse for esc 2 (rear-right - CW)
+            pwm[2] = throttle + pid_output_pitch - pid_output_roll - pid_output_yaw; //Calculate the pulse for esc 3 (rear-left - CCW)
+            pwm[3] = throttle - pid_output_pitch - pid_output_roll + pid_output_yaw; //Calculate the pulse for esc 4 (front-left - CW)
+            pwm[4] = 1000;
+            pwm[5] = 1000;
+            
+            for (int i = 0; i < 6; i++)
+                pwm[i] = constrain( pwm[i], 1100, 2000);                                         //Keep the motors running.
+        }        
+        else {
+            for (int i = 0; i < 6; i++)
+                pwm[i] = 1000;                                                           //If start is not 2 keep a 1000us pulse for ess-1.
+        }
+    
+    
+    
+        
+        while ( timer.read_us() < 4000 )
+            ; // wait
+            
+        motorPin1 = motorPin2 = motorPin3 = motorPin4 = 1;
+        timer.reset();
+        
+        readIMU();
+        
+        if ( loopCounter++ % 20 == 0 ) {
+            //pc.printf("%d %d %d %d\n", pwm[0], pwm[1], pwm[2], pwm[3]);
+            pc.printf("%f %f\n", angle_roll, angle_pitch );
+            //pc.printf("%d\n", pwm[0] );
+            //pc.printf("Gyro (%f, %f, %f)\n", gyro_smoothed[0], gyro_smoothed[1], gyro_smoothed[2]);
+            //pc.printf("%d, %d, %d, %d, %d, %d\n", ppm.channels[0], ppm.channels[1], ppm.channels[2], ppm.channels[3], ppm.channels[4], ppm.channels[5]);
+        }
+        
+        bool doneOutput = false;
+        while ( ! doneOutput ) {
+            int now = timer.read_us();
+            int c = 0;
+            if ( now >= pwm[0] ) { motorPin1 = 0; c++; }
+            if ( now >= pwm[1] ) { motorPin2 = 0; c++; }
+            if ( now >= pwm[2] ) { motorPin3 = 0; c++; }
+            if ( now >= pwm[3] ) { motorPin4 = 0; c++; }
+            if ( now >= pwm[4] ) { motorPin5 = 0; c++; }
+            if ( now >= pwm[5] ) { motorPin6 = 0; c++; }
+            doneOutput = c >= 6;
+        }
+        
     }
-}
\ No newline at end of file
+    
+    /*while (true) {
+        pc.printf("%d, %d, %d, %d, %d, %d\n", ppm.channels[0], ppm.channels[1], ppm.channels[2], ppm.channels[3], ppm.channels[4], ppm.channels[5]);
+    }*/
+}

diff -r f76c26307f9a -r 411d267f9d32 mbed.bld
--- a/mbed.bld	Thu Feb 14 17:24:48 2013 +0000
+++ b/mbed.bld	Fri Oct 04 17:04:41 2019 +0000
@@ -1,1 +1,1 @@
-http://mbed.org/users/mbed_official/code/mbed/builds/0954ebd79f59
\ No newline at end of file
+https://os.mbed.com/users/mbed_official/code/mbed/builds/65be27845400
\ No newline at end of file