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Kris Winer 7 years ago committed by GitHub
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  1. 701
      EM7180_LSM6DSM_LIS2MDL_LPS22HB_Butterfly/EM7180_LSM6DSM_LIS2MDL_LPS22HB_Butterfly.ino
  2. 244
      EM7180_LSM6DSM_LIS2MDL_LPS22HB_Butterfly/LIS2MDL.cpp
  3. 74
      EM7180_LSM6DSM_LIS2MDL_LPS22HB_Butterfly/LIS2MDL.h
  4. 132
      EM7180_LSM6DSM_LIS2MDL_LPS22HB_Butterfly/LPS22HB.cpp
  5. 71
      EM7180_LSM6DSM_LIS2MDL_LPS22HB_Butterfly/LPS22HB.h
  6. 289
      EM7180_LSM6DSM_LIS2MDL_LPS22HB_Butterfly/LSM6DSM.cpp
  7. 179
      EM7180_LSM6DSM_LIS2MDL_LPS22HB_Butterfly/LSM6DSM.h
  8. 97
      EM7180_LSM6DSM_LIS2MDL_LPS22HB_Butterfly/MadgwickFilter.ino
  9. 1262
      EM7180_LSM6DSM_LIS2MDL_LPS22HB_Butterfly/USFS.cpp
  10. 328
      EM7180_LSM6DSM_LIS2MDL_LPS22HB_Butterfly/USFS.h

701
EM7180_LSM6DSM_LIS2MDL_LPS22HB_Butterfly/EM7180_LSM6DSM_LIS2MDL_LPS22HB_Butterfly.ino
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#include "LSM6DSM.h"
#include "LIS2MDL.h"
#include "LPS22HB.h"
#include "USFS.h"
#include <RTC.h>
bool SerialDebug = true; // set to true to get Serial output for debugging
bool passThru = false;
#define myLed 13
const char *build_date = __DATE__; // 11 characters MMM DD YYYY
const char *build_time = __TIME__; // 8 characters HH:MM:SS
// global constants for 9 DoF fusion and AHRS (Attitude and Heading Reference System)
float pi = 3.141592653589793238462643383279502884f;
float GyroMeasError = pi * (40.0f / 180.0f); // gyroscope measurement error in rads/s (start at 40 deg/s)
float GyroMeasDrift = pi * (0.0f / 180.0f); // gyroscope measurement drift in rad/s/s (start at 0.0 deg/s/s)
float beta = sqrtf(3.0f / 4.0f) * GyroMeasError; // compute beta
float zeta = sqrtf(3.0f / 4.0f) * GyroMeasDrift; // compute zeta, the other free parameter in the Madgwick scheme usually set to a small or zero value
uint32_t delt_t = 0; // used to control display output rate
uint32_t sumCount = 0; // used to control display output rate
float pitch, yaw, roll, Yaw, Pitch, Roll;
float a12, a22, a31, a32, a33; // rotation matrix coefficients for Euler angles and gravity components
float A12, A22, A31, A32, A33; // rotation matrix coefficients for Hardware Euler angles and gravity components
float deltat = 0.0f, sum = 0.0f; // integration interval for both filter schemes
uint32_t lastUpdate = 0, firstUpdate = 0; // used to calculate integration interval
uint32_t Now = 0; // used to calculate integration interval
float lin_ax, lin_ay, lin_az; // linear acceleration (acceleration with gravity component subtracted)
float lin_Ax, lin_Ay, lin_Az; // Hardware linear acceleration (acceleration with gravity component subtracted)
float q[4] = {1.0f, 0.0f, 0.0f, 0.0f}; // vector to hold quaternion
float Q[4] = {1.0f, 0.0f, 0.0f, 0.0f}; // hardware quaternion data register
float eInt[3] = {0.0f, 0.0f, 0.0f}; // vector to hold integral error for Mahony method
//LSM6DSM definitions
#define LSM6DSM_intPin1 10 // interrupt1 pin definitions, significant motion
#define LSM6DSM_intPin2 9 // interrupt2 pin definitions, data ready
/* Specify sensor parameters (sample rate is twice the bandwidth)
* choices are:
AFS_2G, AFS_4G, AFS_8G, AFS_16G
GFS_245DPS, GFS_500DPS, GFS_1000DPS, GFS_2000DPS
AODR_12_5Hz, AODR_26Hz, AODR_52Hz, AODR_104Hz, AODR_208Hz, AODR_416Hz, AODR_833Hz, AODR_1660Hz, AODR_3330Hz, AODR_6660Hz
GODR_12_5Hz, GODR_26Hz, GODR_52Hz, GODR_104Hz, GODR_208Hz, GODR_416Hz, GODR_833Hz, GODR_1660Hz, GODR_3330Hz, GODR_6660Hz
*/
uint8_t Ascale = AFS_2G, Gscale = GFS_245DPS, AODR = AODR_208Hz, GODR = GODR_416Hz;
float aRes, gRes; // scale resolutions per LSB for the accel and gyro sensor2
float accelBias[3] = {-0.00499, 0.01540, 0.02902}, gyroBias[3] = {-0.50, 0.14, 0.28}; // offset biases for the accel and gyro
int16_t LSM6DSMData[7]; // Stores the 16-bit signed sensor output
float Gtemperature; // Stores the real internal gyro temperature in degrees Celsius
float ax, ay, az, gx, gy, gz; // variables to hold latest accel/gyro data values
bool newLSM6DSMData = false;
bool newLSM6DSMTap = false;
LSM6DSM LSM6DSM(LSM6DSM_intPin1, LSM6DSM_intPin2); // instantiate LSM6DSM class
//LIS2MDL definitions
#define LIS2MDL_intPin 8 // interrupt for magnetometer data ready
/* Specify sensor parameters (sample rate is twice the bandwidth)
* choices are: MODR_10Hz, MOIDR_20Hz, MODR_50 Hz and MODR_100Hz
*/
uint8_t MODR = MODR_100Hz;
float mRes = 0.0015f; // mag sensitivity
float magBias[3] = {0,0,0}, magScale[3] = {0,0,0}; // Bias corrections for magnetometer
int16_t LIS2MDLData[4]; // Stores the 16-bit signed sensor output
float Mtemperature; // Stores the real internal chip temperature in degrees Celsius
float mx, my, mz; // variables to hold latest mag data values
uint8_t LIS2MDLstatus;
bool newLIS2MDLData = false;
LIS2MDL LIS2MDL(LIS2MDL_intPin); // instantiate LIS2MDL class
// LPS22H definitions
uint8_t LPS22H_intPin = 5;
/* Specify sensor parameters (sample rate is twice the bandwidth)
Choices are P_1Hz, P_10Hz P_25 Hz, P_50Hz, and P_75Hz
*/
uint8_t PODR = P_25Hz; // set pressure amd temperature output data rate
uint8_t LPS22Hstatus;
float temperature, pressure, altitude;
bool newLPS22HData = false;
LPS22H LPS22H(LPS22H_intPin);
// RTC set time using STM32L4 natve RTC class
/* Change these values to set the current initial time */
uint8_t seconds = 0;
uint8_t minutes = 33;
uint8_t hours = 12;
/* Change these values to set the current initial date */
uint8_t day = 2;
uint8_t month = 12;
uint8_t year = 17;
uint8_t Seconds, Minutes, Hours, Day, Month, Year;
bool alarmFlag = false; // for RTC alarm interrupt
const uint8_t USFS_intPin = 8;
bool newEM7180Data = false;
int16_t accelCount[3]; // Stores the 16-bit signed accelerometer sensor output
int16_t gyroCount[3]; // Stores the 16-bit signed gyro sensor output
int16_t magCount[3]; // Stores the 16-bit signed magnetometer sensor output
int16_t tempCount, rawPressure, rawTemperature; // temperature raw count output
float Temperature, Pressure, Altitude; // temperature in degrees Celsius, pressure in mbar
float Ax, Ay, Az, Gx, Gy, Gz, Mx, My, Mz; // variables to hold latest sensor data values
/* Choose EM7180, MPU9250 and MS5637 sample rates and bandwidths
Choices are:
accBW, gyroBW 0x00 = 250 Hz, 0x01 = 184 Hz, 0x02 = 92 Hz, 0x03 = 41 Hz, 0x04 = 20 Hz, 0x05 = 10 Hz, 0x06 = 5 Hz, 0x07 = no filter (3600 Hz)
QRtDiv 0x00, 0x01, 0x02, etc quat rate = gyroRt/(1 + QRtDiv)
magRt 8 Hz = 0x08 or 100 Hz 0x64
accRt, gyroRt 1000, 500, 250, 200, 125, 100, 50 Hz enter by choosing desired rate
and dividing by 10, so 200 Hz would be 200/10 = 20 = 0x14
sample rate of barometer is baroRt/2 so for 25 Hz enter 50 = 0x32
*/
uint8_t accBW = 0x03, gyroBW = 0x03, QRtDiv = 0x01, magRt = 0x64, accRt = 0x14, gyroRt = 0x14, baroRt = 0x32;
/*
Choose MPU9250 sensor full ranges
Choices are 2, 4, 8, 16 g for accFS, 250, 500, 1000, and 2000 dps for gyro FS and 1000 uT for magFS expressed as HEX values
*/
uint16_t accFS = 0x08, gyroFS = 0x7D0, magFS = 0x3E8;
USFS USFS(USFS_intPin, passThru);
void setup() {
// put your setup code here, to run once:
Serial.begin(115200);
delay(4000);
// Configure led
pinMode(myLed, OUTPUT);
digitalWrite(myLed, HIGH); // start with led off
Wire.begin(TWI_PINS_20_21); // set master mode
Wire.setClock(400000); // I2C frequency at 400 kHz
delay(1000);
LSM6DSM.I2Cscan(); // which I2C device are on the bus?
if(!passThru)
{
// Initialize the USFS
USFS.getChipID(); // check ROM/RAM version of EM7180
USFS.loadfwfromEEPROM(); // load EM7180 firmware from EEPROM
USFS.initEM7180(accBW, gyroBW, accFS, gyroFS, magFS, QRtDiv, magRt, accRt, gyroRt, baroRt); // set MPU and MS5637 sensor parameters
} // end of "if(!passThru)" handling
if(passThru)
{
// Read the LSM6DSM Chip ID register, this is a good test of communication
Serial.println("LSM6DSM accel/gyro...");
byte c = LSM6DSM.getChipID(); // Read CHIP_ID register for LSM6DSM
Serial.print("LSM6DSM "); Serial.print("I AM "); Serial.print(c, HEX); Serial.print(" I should be "); Serial.println(0x6A, HEX);
Serial.println(" ");
delay(1000);
// Read the LIS2MDL Chip ID register, this is a good test of communication
Serial.println("LIS2MDL mag...");
byte d = LIS2MDL.getChipID(); // Read CHIP_ID register for LSM6DSM
Serial.print("LIS2MDL "); Serial.print("I AM "); Serial.print(d, HEX); Serial.print(" I should be "); Serial.println(0x40, HEX);
Serial.println(" ");
delay(1000);
Serial.println("LPS22HB barometer...");
uint8_t e = LPS22H.getChipID();
Serial.print("LPS25H "); Serial.print("I AM "); Serial.print(e, HEX); Serial.print(" I should be "); Serial.println(0xB1, HEX);
delay(1000);
if(c == 0x6A && d == 0x40 && e == 0xB1) // check if all I2C sensors have acknowledged
{
Serial.println("LSM6DSM and LIS2MDL and LPS22HB are online..."); Serial.println(" ");
digitalWrite(myLed, LOW);
LSM6DSM.reset(); // software reset LSM6DSM to default registers
// get sensor resolutions, only need to do this once
aRes = LSM6DSM.getAres(Ascale);
gRes = LSM6DSM.getGres(Gscale);
LSM6DSM.init(Ascale, Gscale, AODR, GODR);
LSM6DSM.selfTest();
LSM6DSM.offsetBias(gyroBias, accelBias);
Serial.println("accel biases (mg)"); Serial.println(1000.0f * accelBias[0]); Serial.println(1000.0f * accelBias[1]); Serial.println(1000.0f * accelBias[2]);
Serial.println("gyro biases (dps)"); Serial.println(gyroBias[0]); Serial.println(gyroBias[1]); Serial.println(gyroBias[2]);
delay(1000);
LIS2MDL.reset(); // software reset LIS2MDL to default registers
mRes = 0.0015f; // fixed sensitivity and full scale (+/- 49.152 Gauss);
LIS2MDL.init(MODR);
LIS2MDL.selfTest();
LIS2MDL.offsetBias(magBias, magScale);
Serial.println("mag biases (mG)"); Serial.println(1000.0f * magBias[0]); Serial.println(1000.0f * magBias[1]); Serial.println(1000.0f * magBias[2]);
Serial.println("mag scale (mG)"); Serial.println(magScale[0]); Serial.println(magScale[1]); Serial.println(magScale[2]);
delay(2000); // add delay to see results before serial spew of data
LPS22H.Init(PODR); // Initialize LPS22H altimeter
delay(1000);
digitalWrite(myLed, HIGH);
}
else
{
if(c != 0x6A) Serial.println(" LSM6DSM not functioning!");
if(d != 0x40) Serial.println(" LIS2MDL not functioning!");
if(e != 0xB1) Serial.println(" LPS22HB not functioning!");
while(1){};
}
} // end of "if(passThru)" handling
// Set the time
SetDefaultRTC();
/* Set up the RTC alarm interrupt */
RTC.enableAlarm(RTC.MATCH_ANY); // alarm once a second
RTC.attachInterrupt(alarmMatch); // interrupt every time the alarm sounds
if(!passThru)
{
attachInterrupt(USFS_intPin, EM7180intHandler, RISING); // define interrupt for INT pin output of EM7180
USFS.checkEM7180Status();
}
if(passThru)
{
attachInterrupt(LSM6DSM_intPin2, myinthandler1, RISING); // define interrupt for intPin2 output of LSM6DSM
attachInterrupt(LIS2MDL_intPin , myinthandler2, RISING); // define interrupt for intPin output of LIS2MDL
attachInterrupt(LPS22H_intPin , myinthandler3, RISING); // define interrupt for intPin output of LPS22HB
LIS2MDLstatus = LIS2MDL.status(); // read status register to clear interrupt before main loop
}
}
/* End of setup */
void loop() {
if(passThru)
{
// If intPin goes high, either all data registers have new data
if(newLSM6DSMData == true) { // On interrupt, read data
newLSM6DSMData = false; // reset newData flag
LSM6DSM.readData(LSM6DSMData); // INT2 cleared on any read
// Now we'll calculate the accleration value into actual g's
ax = (float)LSM6DSMData[4]*aRes - accelBias[0]; // get actual g value, this depends on scale being set
ay = (float)LSM6DSMData[5]*aRes - accelBias[1];
az = (float)LSM6DSMData[6]*aRes - accelBias[2];
// Calculate the gyro value into actual degrees per second
gx = (float)LSM6DSMData[1]*gRes - gyroBias[0]; // get actual gyro value, this depends on scale being set
gy = (float)LSM6DSMData[2]*gRes - gyroBias[1];
gz = (float)LSM6DSMData[3]*gRes - gyroBias[2];
for(uint8_t i = 0; i < 10; i++) { // iterate a fixed number of times per data read cycle
Now = micros();
deltat = ((Now - lastUpdate)/1000000.0f); // set integration time by time elapsed since last filter update
lastUpdate = Now;
sum += deltat; // sum for averaging filter update rate
sumCount++;
MadgwickQuaternionUpdate(-ax, ay, az, gx*pi/180.0f, -gy*pi/180.0f, -gz*pi/180.0f, mx, my, -mz);
}
}
// If intPin goes high, either all data registers have new data
if(newLIS2MDLData == true) { // On interrupt, read data
newLIS2MDLData = false; // reset newData flag
LIS2MDLstatus = LIS2MDL.status();
if(LIS2MDLstatus & 0x08) // if all axes have new data ready
{
LIS2MDL.readData(LIS2MDLData);
// Now we'll calculate the accleration value into actual G's
mx = (float)LIS2MDLData[0]*mRes - magBias[0]; // get actual G value
my = (float)LIS2MDLData[1]*mRes - magBias[1];
mz = (float)LIS2MDLData[2]*mRes - magBias[2];
mx *= magScale[0];
my *= magScale[1];
mz *= magScale[2];
}
}
} // end of "if(passThru)" handling
if(!passThru)
{
/*EM7180*/
// If intpin goes high, all data registers have new data
if (newEM7180Data == true) { // On interrupt, read data
newEM7180Data = false; // reset newData flag
// Check event status register, way to chech data ready by polling rather than interrupt
uint8_t eventStatus = USFS.checkEM7180Status(); // reading clears the register
// Check for errors
if (eventStatus & 0x02) { // error detected, what is it?
uint8_t errorStatus = USFS.checkEM7180Errors();
if (errorStatus != 0x00) { // is there an error?
Serial.print(" EM7180 sensor status = "); Serial.println(errorStatus);
if (errorStatus == 0x11) Serial.print("Magnetometer failure!");
if (errorStatus == 0x12) Serial.print("Accelerometer failure!");
if (errorStatus == 0x14) Serial.print("Gyro failure!");
if (errorStatus == 0x21) Serial.print("Magnetometer initialization failure!");
if (errorStatus == 0x22) Serial.print("Accelerometer initialization failure!");
if (errorStatus == 0x24) Serial.print("Gyro initialization failure!");
if (errorStatus == 0x30) Serial.print("Math error!");
if (errorStatus == 0x80) Serial.print("Invalid sample rate!");
}
// Handle errors ToDo
}
// if no errors, see if new data is ready
if (eventStatus & 0x10) { // new acceleration data available
USFS.readSENtralAccelData(accelCount);
// Now we'll calculate the accleration value into actual g's
Ax = (float)accelCount[0] * 0.000488f; // get actual g value
Ay = (float)accelCount[1] * 0.000488f;
Az = (float)accelCount[2] * 0.000488f;
}
if (eventStatus & 0x20) { // new gyro data available
USFS.readSENtralGyroData(gyroCount);
// Now we'll calculate the gyro value into actual dps's
Gx = (float)gyroCount[0] * 0.153f; // get actual dps value
Gy = (float)gyroCount[1] * 0.153f;
Gz = (float)gyroCount[2] * 0.153f;
}
if (eventStatus & 0x08) { // new mag data available
USFS.readSENtralMagData(magCount);
// Now we'll calculate the mag value into actual G's
Mx = (float)magCount[0] * 0.305176f; // get actual G value
My = (float)magCount[1] * 0.305176f;
Mz = (float)magCount[2] * 0.305176f;
}
if (eventStatus & 0x04) { // new quaternion data available
USFS.readSENtralQuatData(Q);
}
// get MS5637 pressure
if (eventStatus & 0x40) { // new baro data available
rawPressure = USFS.readSENtralBaroData();
Pressure = (float)rawPressure * 0.01f + 1013.25f; // pressure in mBar
// get MS5637 temperature
rawTemperature = USFS.readSENtralTempData();
Temperature = (float) rawTemperature * 0.01f; // temperature in degrees C
}
}
} // end of "if(!passThru)" handling
// end sensor interrupt handling
/*RTC*/
if(alarmFlag) { // update RTC output (serial display) whenever the RTC alarm condition is achieved and the MPU9250 is awake
alarmFlag = false;
// Read RTC
if(SerialDebug)
{
Serial.println("RTC:");
Day = RTC.getDay();
Month = RTC.getMonth();
Year = RTC.getYear();
Seconds = RTC.getSeconds();
Minutes = RTC.getMinutes();
Hours = RTC.getHours();
if(Hours < 10) {Serial.print("0"); Serial.print(Hours);} else Serial.print(Hours);
Serial.print(":");
if(Minutes < 10) {Serial.print("0"); Serial.print(Minutes);} else Serial.print(Minutes);
Serial.print(":");
if(Seconds < 10) {Serial.print("0"); Serial.println(Seconds);} else Serial.println(Seconds);
Serial.print(Month); Serial.print("/"); Serial.print(Day); Serial.print("/"); Serial.println(Year);
Serial.println(" ");
}
if(passThru)
{
if(SerialDebug) {
Serial.print("ax = "); Serial.print((int)1000*ax);
Serial.print(" ay = "); Serial.print((int)1000*ay);
Serial.print(" az = "); Serial.print((int)1000*az); Serial.println(" mg");
Serial.print("gx = "); Serial.print( gx, 2);
Serial.print(" gy = "); Serial.print( gy, 2);
Serial.print(" gz = "); Serial.print( gz, 2); Serial.println(" deg/s");
Serial.print("mx = "); Serial.print((int)1000*mx);
Serial.print(" my = "); Serial.print((int)1000*my);
Serial.print(" mz = "); Serial.print((int)1000*mz); Serial.println(" mG");
Serial.print("q0 = "); Serial.print(q[0]);
Serial.print(" qx = "); Serial.print(q[1]);
Serial.print(" qy = "); Serial.print(q[2]);
Serial.print(" qz = "); Serial.println(q[3]);
}
// get pressure and temperature from the LPS22HB
LPS22Hstatus = LPS22H.status();
if(LPS22Hstatus & 0x01) { // if new pressure data available
pressure = (float) LPS22H.readAltimeterPressure()/4096.0f;
temperature = (float) LPS22H.readAltimeterTemperature()/100.0f;
altitude = 145366.45f*(1.0f - pow((pressure/1013.25f), 0.190284f));
if(SerialDebug) {
Serial.print("Altimeter temperature = "); Serial.print( temperature, 2); Serial.println(" C"); // temperature in degrees Celsius
Serial.print("Altimeter temperature = "); Serial.print(9.0f*temperature/5.0f + 32.0f, 2); Serial.println(" F"); // temperature in degrees Fahrenheit
Serial.print("Altimeter pressure = "); Serial.print(pressure, 2); Serial.println(" mbar");// pressure in millibar
Serial.print("Altitude = "); Serial.print(altitude, 2); Serial.println(" feet");
}
}
Gtemperature = ((float) LSM6DSMData[0]) / 256.0f + 25.0f; // Gyro chip temperature in degrees Centigrade
// Print temperature in degrees Centigrade
if(SerialDebug) {
Serial.print("Gyro temperature is "); Serial.print(Gtemperature, 1); Serial.println(" degrees C"); // Print T values to tenths of s degree C
}
LIS2MDLData[3] = LIS2MDL.readTemperature();
Mtemperature = ((float) LIS2MDLData[3]) / 8.0f + 25.0f; // Mag chip temperature in degrees Centigrade
// Print temperature in degrees Centigrade
if(SerialDebug) {
Serial.print("Mag temperature is "); Serial.print(Mtemperature, 1); Serial.println(" degrees C"); // Print T values to tenths of s degree C
}
a12 = 2.0f * (q[1] * q[2] + q[0] * q[3]);
a22 = q[0] * q[0] + q[1] * q[1] - q[2] * q[2] - q[3] * q[3];
a31 = 2.0f * (q[0] * q[1] + q[2] * q[3]);
a32 = 2.0f * (q[1] * q[3] - q[0] * q[2]);
a33 = q[0] * q[0] - q[1] * q[1] - q[2] * q[2] + q[3] * q[3];
pitch = -asinf(a32);
roll = atan2f(a31, a33);
yaw = atan2f(a12, a22);
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
if(yaw < 0) yaw += 360.0f; // Ensure yaw stays between 0 and 360
roll *= 180.0f / pi;
lin_ax = ax + a31;
lin_ay = ay + a32;
lin_az = az - a33;
if(SerialDebug) {
Serial.print("Yaw, Pitch, Roll: ");
Serial.print(yaw, 2);
Serial.print(", ");
Serial.print(pitch, 2);
Serial.print(", ");
Serial.println(roll, 2);
Serial.print("Grav_x, Grav_y, Grav_z: ");
Serial.print(-a31*1000.0f, 2);
Serial.print(", ");
Serial.print(-a32*1000.0f, 2);
Serial.print(", ");
Serial.print(a33*1000.0f, 2); Serial.println(" mg");
Serial.print("Lin_ax, Lin_ay, Lin_az: ");
Serial.print(lin_ax*1000.0f, 2);
Serial.print(", ");
Serial.print(lin_ay*1000.0f, 2);
Serial.print(", ");
Serial.print(lin_az*1000.0f, 2); Serial.println(" mg");
Serial.print("rate = "); Serial.print((float)sumCount/sum, 2); Serial.println(" Hz");
}
// Serial.print(millis()/1000);Serial.print(",");
// Serial.print(yaw, 2); Serial.print(","); Serial.print(pitch, 2); Serial.print(","); Serial.print(roll, 2); Serial.print(","); Serial.println(Pressure, 2);
sumCount = 0;
sum = 0;
} // end of "if(passThru)" handling
if(!passThru)
{
if (SerialDebug) {
Serial.print("Ax = "); Serial.print((int)1000 * Ax);
Serial.print(" Ay = "); Serial.print((int)1000 * Ay);
Serial.print(" Az = "); Serial.print((int)1000 * Az); Serial.println(" mg");
Serial.print("Gx = "); Serial.print( Gx, 2);
Serial.print(" Gy = "); Serial.print( Gy, 2);
Serial.print(" Gz = "); Serial.print( Gz, 2); Serial.println(" deg/s");
Serial.print("Mx = "); Serial.print( (int)Mx);
Serial.print(" My = "); Serial.print( (int)My);
Serial.print(" Mz = "); Serial.print( (int)Mz); Serial.println(" mG");
Serial.println("Hardware quaternions:");
Serial.print("Q0 = "); Serial.print(Q[0]);
Serial.print(" Qx = "); Serial.print(Q[1]);
Serial.print(" Qy = "); Serial.print(Q[2]);
Serial.print(" Qz = "); Serial.println(Q[3]);
}
//Hardware AHRS:
A12 = 2.0f * (Q[1] * Q[2] + Q[0] * Q[3]);
A22 = Q[0] * Q[0] + Q[1] * Q[1] - Q[2] * Q[2] - Q[3] * Q[3];
A31 = 2.0f * (Q[0] * Q[1] + Q[2] * Q[3]);
A32 = 2.0f * (Q[1] * Q[3] - Q[0] * Q[2]);
A33 = Q[0] * Q[0] - Q[1] * Q[1] - Q[2] * Q[2] + Q[3] * Q[3];
Pitch = -asinf(A32);
Roll = atan2f(A31, A33);
Yaw = atan2f(A12, A22);
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
if (Yaw < 0) Yaw += 360.0f ; // Ensure yaw stays between 0 and 360
Roll *= 180.0f / pi;
lin_Ax = ax + a31;
lin_Ay = ay + a32;
lin_Az = az - a33;
if (SerialDebug) {
Serial.print("Hardware Yaw, pitch, Roll: ");
Serial.print(Yaw, 2);
Serial.print(", ");
Serial.print(Pitch, 2);
Serial.print(", ");
Serial.println(Roll, 2);
Serial.print("Hardware Grav_x, Grav_y, Grav_z: ");
Serial.print(-A31 * 1000, 2);
Serial.print(", ");
Serial.print(-A32 * 1000, 2);
Serial.print(", ");
Serial.print(A33 * 1000, 2); Serial.println(" mg");
Serial.print("Hardware Lin_ax, Lin_ay, Lin_az: ");
Serial.print(lin_Ax * 1000, 2);
Serial.print(", ");
Serial.print(lin_Ay * 1000, 2);
Serial.print(", ");
Serial.print(lin_Az * 1000, 2); Serial.println(" mg");
Serial.println("MS5637:");
Serial.print("Altimeter temperature = ");
Serial.print(Temperature, 2);
Serial.println(" C"); // temperature in degrees Celsius
Serial.print("Altimeter temperature = ");
Serial.print(9.0f * Temperature / 5.0f + 32.0f, 2);
Serial.println(" F"); // temperature in degrees Fahrenheit
Serial.print("Altimeter pressure = ");
Serial.print(Pressure, 2);
Serial.println(" mbar");// pressure in millibar
Altitude = 145366.45f * (1.0f - pow(((Pressure) / 1013.25f), 0.190284f));
Serial.print("Altitude = ");
Serial.print(Altitude, 2);
Serial.println(" feet");
Serial.println(" ");
}
} // end of "if(!passThru)" handling
} // end of RTC alarm handling
digitalWrite(myLed, LOW); delay(10); digitalWrite(myLed, HIGH); // flash led for 10 milliseconds
STM32.sleep();
} //end of loop
/* End of main loop */
void myinthandler1()
{
newLSM6DSMData = true;
}
void myinthandler2()
{
newLIS2MDLData = true;
}
void myinthandler3()
{
newLPS22HData = true;
}
void EM7180intHandler()
{
newEM7180Data = true;
}
void alarmMatch()
{
alarmFlag = true;
}
void SetDefaultRTC() // Sets the RTC to the FW build date-time...
{
char Build_mo[3];
// Convert month string to integer
Build_mo[0] = build_date[0];
Build_mo[1] = build_date[1];
Build_mo[2] = build_date[2];
String build_mo = Build_mo;
if(build_mo == "Jan")
{
month = 1;
} else if(build_mo == "Feb")
{
month = 2;
} else if(build_mo == "Mar")
{
month = 3;
} else if(build_mo == "Apr")
{
month = 4;
} else if(build_mo == "May")
{
month = 5;
} else if(build_mo == "Jun")
{
month = 6;
} else if(build_mo == "Jul")
{
month = 7;
} else if(build_mo == "Aug")
{
month = 8;
} else if(build_mo == "Sep")
{
month = 9;
} else if(build_mo == "Oct")
{
month = 10;
} else if(build_mo == "Nov")
{
month = 11;
} else if(build_mo == "Dec")
{
month = 12;
} else
{
month = 1; // Default to January if something goes wrong...
}
// Convert ASCII strings to integers
day = (build_date[4] - 48)*10 + build_date[5] - 48; // ASCII "0" = 48
year = (build_date[9] - 48)*10 + build_date[10] - 48;
hours = (build_time[0] - 48)*10 + build_time[1] - 48;
minutes = (build_time[3] - 48)*10 + build_time[4] - 48;
seconds = (build_time[6] - 48)*10 + build_time[7] - 48;
// Set the date/time
RTC.setDay(day);
RTC.setMonth(month);
RTC.setYear(year);
RTC.setHours(hours);
RTC.setMinutes(minutes);
RTC.setSeconds(seconds);
}

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EM7180_LSM6DSM_LIS2MDL_LPS22HB_Butterfly/LIS2MDL.cpp
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/* 09/23/2017 Copyright Tlera Corporation
Created by Kris Winer
This sketch uses SDA/SCL on pins 21/20 (Butterfly default), respectively, and it uses the Butterfly STM32L433CU Breakout Board.
The LIS2MDL is a low power magnetometer, here used as 3 DoF in a 9 DoF absolute orientation solution.
Library may be used freely and without limit with attribution.
*/
#include "LIS2MDL.h"
LIS2MDL::LIS2MDL(uint8_t intPin)
{
pinMode(intPin, INPUT);
_intPin = intPin;
}
uint8_t LIS2MDL::getChipID()
{
uint8_t c = readByte(LIS2MDL_ADDRESS, LIS2MDL_WHO_AM_I);
return c;
}
void LIS2MDL::reset()
{
// reset device
uint8_t temp = readByte(LIS2MDL_ADDRESS, LIS2MDL_CFG_REG_A);
writeByte(LIS2MDL_ADDRESS, LIS2MDL_CFG_REG_A, temp | 0x20); // Set bit 5 to 1 to reset LIS2MDL
delay(1);
writeByte(LIS2MDL_ADDRESS, LIS2MDL_CFG_REG_A, temp | 0x40); // Set bit 6 to 1 to boot LIS2MDL
delay(100); // Wait for all registers to reset
}
void LIS2MDL::init(uint8_t MODR)
{
// enable temperature compensation (bit 7 == 1), continuous mode (bits 0:1 == 00)
writeByte(LIS2MDL_ADDRESS, LIS2MDL_CFG_REG_A, 0x80 | MODR<<2);
// enable low pass filter (bit 0 == 1), set to ODR/4
writeByte(LIS2MDL_ADDRESS, LIS2MDL_CFG_REG_B, 0x01);
// enable data ready on interrupt pin (bit 0 == 1), enable block data read (bit 4 == 1)
writeByte(LIS2MDL_ADDRESS, LIS2MDL_CFG_REG_C, 0x01 | 0x10);
}
uint8_t LIS2MDL::status()
{
// Read the status register of the altimeter
uint8_t temp = readByte(LIS2MDL_ADDRESS, LIS2MDL_STATUS_REG);
return temp;
}
void LIS2MDL::readData(int16_t * destination)
{
uint8_t rawData[6]; // x/y/z mag register data stored here
readBytes(LIS2MDL_ADDRESS, (0x80 | LIS2MDL_OUTX_L_REG), 8, &rawData[0]); // Read the 6 raw data registers into data array
destination[0] = ((int16_t)rawData[1] << 8) | rawData[0] ; // Turn the MSB and LSB into a signed 16-bit value
destination[1] = ((int16_t)rawData[3] << 8) | rawData[2] ;
destination[2] = ((int16_t)rawData[5] << 8) | rawData[4] ;
}
int16_t LIS2MDL::readTemperature()
{
uint8_t rawData[2]; // x/y/z mag register data stored here
readBytes(LIS2MDL_ADDRESS, (0x80 | LIS2MDL_TEMP_OUT_L_REG), 2, &rawData[0]); // Read the 8 raw data registers into data array
int16_t temp = ((int16_t)rawData[1] << 8) | rawData[0] ; // Turn the MSB and LSB into a signed 16-bit value
return temp;
}
void LIS2MDL::offsetBias(float * dest1, float * dest2)
{
int32_t mag_bias[3] = {0, 0, 0}, mag_scale[3] = {0, 0, 0};
int16_t mag_max[3] = {-32767, -32767, -32767}, mag_min[3] = {32767, 32767, 32767}, mag_temp[3] = {0, 0, 0};
float _mRes = 0.0015f;
Serial.println("Calculate mag offset bias: move all around to sample the complete response surface!");
delay(4000);
for (int ii = 0; ii < 4000; ii++)
{
readData(mag_temp);
for (int jj = 0; jj < 3; jj++) {
if(mag_temp[jj] > mag_max[jj]) mag_max[jj] = mag_temp[jj];
if(mag_temp[jj] < mag_min[jj]) mag_min[jj] = mag_temp[jj];
}
delay(12);
}
_mRes = 0.0015f; // fixed sensitivity
// Get hard iron correction
mag_bias[0] = (mag_max[0] + mag_min[0])/2; // get average x mag bias in counts
mag_bias[1] = (mag_max[1] + mag_min[1])/2; // get average y mag bias in counts
mag_bias[2] = (mag_max[2] + mag_min[2])/2; // get average z mag bias in counts
dest1[0] = (float) mag_bias[0] * _mRes; // save mag biases in G for main program
dest1[1] = (float) mag_bias[1] * _mRes;
dest1[2] = (float) mag_bias[2] * _mRes;
// Get soft iron correction estimate
mag_scale[0] = (mag_max[0] - mag_min[0])/2; // get average x axis max chord length in counts
mag_scale[1] = (mag_max[1] - mag_min[1])/2; // get average y axis max chord length in counts
mag_scale[2] = (mag_max[2] - mag_min[2])/2; // get average z axis max chord length in counts
float avg_rad = mag_scale[0] + mag_scale[1] + mag_scale[2];
avg_rad /= 3.0f;
dest2[0] = avg_rad/((float)mag_scale[0]);
dest2[1] = avg_rad/((float)mag_scale[1]);
dest2[2] = avg_rad/((float)mag_scale[2]);
Serial.println("Mag Calibration done!");
}
void LIS2MDL::selfTest()
{
int16_t temp[3] = {0, 0, 0};
float magTest[3] = {0., 0., 0.};
float magNom[3] = {0., 0., 0.};
int32_t sum[3] = {0, 0, 0};
float _mRes = 0.0015f;
// first, get average response with self test disabled
for (int ii = 0; ii < 50; ii++)
{
readData(temp);
sum[0] += temp[0];
sum[1] += temp[1];
sum[2] += temp[2];
delay(50);
}
magNom[0] = (float) sum[0] / 50.0f;
magNom[1] = (float) sum[1] / 50.0f;
magNom[2] = (float) sum[2] / 50.0f;
uint8_t c = readByte(LIS2MDL_ADDRESS, LIS2MDL_CFG_REG_C);
writeByte(LIS2MDL_ADDRESS, LIS2MDL_CFG_REG_C, c | 0x02); // enable self test
delay(100); // let mag respond
sum[0] = 0;
sum[1] = 0;
sum[2] = 0;
for (int ii = 0; ii < 50; ii++)
{
readData(temp);
sum[0] += temp[0];
sum[1] += temp[1];
sum[2] += temp[2];
delay(50);
}
magTest[0] = (float) sum[0] / 50.0f;
magTest[1] = (float) sum[1] / 50.0f;
magTest[2] = (float) sum[2] / 50.0f;
writeByte(LIS2MDL_ADDRESS, LIS2MDL_CFG_REG_C, c); // return to previous settings/normal mode
delay(100); // let mag respond
Serial.println("Mag Self Test:");
Serial.print("Mx results:"); Serial.print( (magTest[0] - magNom[0]) * _mRes * 1000.0); Serial.println(" mG");
Serial.print("My results:"); Serial.println((magTest[0] - magNom[0]) * _mRes * 1000.0);
Serial.print("Mz results:"); Serial.println((magTest[1] - magNom[1]) * _mRes * 1000.0);
Serial.println("Should be between 15 and 500 mG");
delay(2000); // give some time to read the screen
}
// I2C scan function
void LIS2MDL::I2Cscan()
{
// scan for i2c devices
byte error, address;
int nDevices;
Serial.println("Scanning...");
nDevices = 0;
for(address = 1; address < 127; address++ )
{
// The i2c_scanner uses the return value of
// the Write.endTransmission to see if
// a device did acknowledge to the address.
// Wire.beginTransmission(address);
// error = Wire.endTransmission();
error = Wire.transfer(address, NULL, 0, NULL, 0);
if (error == 0)
{
Serial.print("I2C device found at address 0x");
if (address<16)
Serial.print("0");
Serial.print(address,HEX);
Serial.println(" !");
nDevices++;
}
else if (error==4)
{
Serial.print("Unknown error at address 0x");
if (address<16)
Serial.print("0");
Serial.println(address,HEX);
}
}
if (nDevices == 0)
Serial.println("No I2C devices found\n");
else
Serial.println("done\n");
}
// I2C read/write functions for the LIS2MDL
void LIS2MDL::writeByte(uint8_t address, uint8_t subAddress, uint8_t data) {
uint8_t temp[2];
temp[0] = subAddress;
temp[1] = data;
Wire.transfer(address, &temp[0], 2, NULL, 0);
}
uint8_t LIS2MDL::readByte(uint8_t address, uint8_t subAddress) {
uint8_t temp[1];
Wire.transfer(address, &subAddress, 1, &temp[0], 1);
return temp[0];
}
void LIS2MDL::readBytes(uint8_t address, uint8_t subAddress, uint8_t count, uint8_t * dest) {
Wire.transfer(address, &subAddress, 1, dest, count);
}

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EM7180_LSM6DSM_LIS2MDL_LPS22HB_Butterfly/LIS2MDL.h
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/* 09/23/2017 Copyright Tlera Corporation
Created by Kris Winer
This sketch uses SDA/SCL on pins 21/20 (Butterfly default), respectively, and it uses the Butterfly STM32L433CU Breakout Board.
The LIS2MDL is a low power magnetometer, here used as 3 DoF in a 9 DoF absolute orientation solution.
Library may be used freely and without limit with attribution.
*/
#ifndef LIS2MDL_h
#define LIS2MDL_h
#include "Arduino.h"
#include <Wire.h>
//Register map for LIS2MDL'
// http://www.st.com/content/ccc/resource/technical/document/datasheet/group3/29/13/d1/e0/9a/4d/4f/30/DM00395193/files/DM00395193.pdf/jcr:content/translations/en.DM00395193.pdf
#define LIS2MDL_OFFSET_X_REG_L 0x45
#define LIS2MDL_OFFSET_X_REG_L 0x46
#define LIS2MDL_OFFSET_X_REG_L 0x47
#define LIS2MDL_OFFSET_X_REG_L 0x48
#define LIS2MDL_OFFSET_X_REG_L 0x49
#define LIS2MDL_OFFSET_X_REG_L 0x4A
#define LIS2MDL_WHO_AM_I 0x4F
#define LIS2MDL_CFG_REG_A 0x60
#define LIS2MDL_CFG_REG_B 0x61
#define LIS2MDL_CFG_REG_C 0x62
#define LIS2MDL_INT_CTRL_REG 0x63
#define LIS2MDL_INT_SOURCE_REG 0x64
#define LIS2MDL_INT_THS_L_REG 0x65
#define LIS2MDL_INT_THS_H_REG 0x66
#define LIS2MDL_STATUS_REG 0x67
#define LIS2MDL_OUTX_L_REG 0x68
#define LIS2MDL_OUTX_H_REG 0x69
#define LIS2MDL_OUTY_L_REG 0x6A
#define LIS2MDL_OUTY_H_REG 0x6B
#define LIS2MDL_OUTZ_L_REG 0x6C
#define LIS2MDL_OUTZ_H_REG 0x6D
#define LIS2MDL_TEMP_OUT_L_REG 0x6E
#define LIS2MDL_TEMP_OUT_H_REG 0x6F
#define LIS2MDL_ADDRESS 0x1E
#define MODR_10Hz 0x00
#define MODR_20Hz 0x01
#define MODR_50Hz 0x02
#define MODR_100Hz 0x03
class LIS2MDL
{
public:
LIS2MDL(uint8_t intPin);
uint8_t getChipID();
void init(uint8_t MODR);
void offsetBias(float * dest1, float * dest2);
void reset();
void selfTest();
uint8_t status();
void readData(int16_t * destination);
int16_t readTemperature();
void I2Cscan();
void writeByte(uint8_t address, uint8_t subAddress, uint8_t data);
uint8_t readByte(uint8_t address, uint8_t subAddress);
void readBytes(uint8_t address, uint8_t subAddress, uint8_t count, uint8_t * dest);
private:
uint8_t _intPin;
float _mRes;
};
#endif

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EM7180_LSM6DSM_LIS2MDL_LPS22HB_Butterfly/LPS22HB.cpp
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/* 09/23/2017 Copyright Tlera Corporation
Created by Kris Winer
This sketch uses SDA/SCL on pins 21/20 (Butterfly default), respectively, and it uses the Butterfly STM32L433CU Breakout Board.
The LPS22HB is a low power barometerr.
Library may be used freely and without limit with attribution.
*/
#include "LPS22HB.h"
#include "Wire.h"
LPS22H::LPS22H(uint8_t intPin)
{
pinMode(intPin, INPUT);
_intPin = intPin;
}
uint8_t LPS22H::getChipID()
{
// Read the WHO_AM_I register of the altimeter this is a good test of communication
uint8_t temp = readByte(LPS22H_ADDRESS, LPS22H_WHOAMI); // Read WHO_AM_I register for LPS22H
return temp;
}
uint8_t LPS22H::status()
{
// Read the status register of the altimeter
uint8_t temp = readByte(LPS22H_ADDRESS, LPS22H_STATUS);
return temp;
}
int32_t LPS22H::readAltimeterPressure()
{
uint8_t rawData[3]; // 24-bit pressure register data stored here
readBytes(LPS22H_ADDRESS, (LPS22H_PRESS_OUT_XL | 0x80), 3, &rawData[0]); // bit 7 must be one to read multiple bytes
return (int32_t) ((int32_t) rawData[2] << 16 | (int32_t) rawData[1] << 8 | rawData[0]);
}
int16_t LPS22H::readAltimeterTemperature()
{
uint8_t rawData[2]; // 16-bit pressure register data stored here
readBytes(LPS22H_ADDRESS, (LPS22H_TEMP_OUT_L | 0x80), 2, &rawData[0]); // bit 7 must be one to read multiple bytes
return (int16_t)((int16_t) rawData[1] << 8 | rawData[0]);
}
void LPS22H::Init(uint8_t PODR)
{
// set sample rate by setting bits 6:4
// enable low-pass filter by setting bit 3 to one
// bit 2 == 0 means bandwidth is odr/9, bit 2 == 1 means bandwidth is odr/20
// make sure data not updated during read by setting block data udate (bit 1) to 1
writeByte(LPS22H_ADDRESS, LPS22H_CTRL_REG1, PODR << 4 | 0x08 | 0x02);
writeByte(LPS22H_ADDRESS, LPS22H_CTRL_REG3, 0x04); // enable data ready as interrupt source
}
// I2C scan function
void LPS22H::I2Cscan()
{
// scan for i2c devices
byte error, address;
int nDevices;
Serial.println("Scanning...");
nDevices = 0;
for(address = 1; address < 127; address++ )
{
// The i2c_scanner uses the return value of
// the Write.endTransmission to see if
// a device did acknowledge to the address.
Wire.beginTransmission(address);
error = Wire.endTransmission();
if (error == 0)
{
Serial.print("I2C device found at address 0x");
if (address<16)
Serial.print("0");
Serial.print(address,HEX);
Serial.println(" !");
nDevices++;
}
else if (error==4)
{
Serial.print("Unknown error at address 0x");
if (address<16)
Serial.print("0");
Serial.println(address,HEX);
}
}
if (nDevices == 0)
Serial.println("No I2C devices found\n");
else
Serial.println("done\n");
}
void LPS22H::writeByte(uint8_t address, uint8_t subAddress, uint8_t data)
{
Wire.beginTransmission(address); // Initialize the Tx buffer
Wire.write(subAddress); // Put slave register address in Tx buffer
Wire.write(data); // Put data in Tx buffer
Wire.endTransmission(); // Send the Tx buffer
}
uint8_t LPS22H::readByte(uint8_t address, uint8_t subAddress)
{
uint8_t data; // `data` will store the register data
Wire.beginTransmission(address); // Initialize the Tx buffer
Wire.write(subAddress); // Put slave register address in Tx buffer
Wire.endTransmission(false); // Send the Tx buffer, but send a restart to keep connection alive
Wire.requestFrom(address, (size_t) 1); // Read one uint8_t from slave register address
data = Wire.read(); // Fill Rx buffer with result
return data; // Return data read from slave register
}
void LPS22H::readBytes(uint8_t address, uint8_t subAddress, uint8_t count, uint8_t * dest)
{
Wire.beginTransmission(address); // Initialize the Tx buffer
Wire.write(subAddress); // Put slave register address in Tx buffer
Wire.endTransmission(false); // Send the Tx buffer, but send a restart to keep connection alive
uint8_t i = 0;
Wire.requestFrom(address, (size_t)count); // Read bytes from slave register address
while (Wire.available()) {
dest[i++] = Wire.read(); } // Put read results in the Rx buffer
}

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EM7180_LSM6DSM_LIS2MDL_LPS22HB_Butterfly/LPS22HB.h
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/* 09/23/2017 Copyright Tlera Corporation
Created by Kris Winer
This sketch uses SDA/SCL on pins 21/20 (Butterfly default), respectively, and it uses the Butterfly STM32L433CU Breakout Board.
The LPS22HB is a low power barometerr.
Library may be used freely and without limit with attribution.
*/
#ifndef LPS22HB_h
#define LPS22HB_h
#include "Arduino.h"
#include "Wire.h"
// See LPS22H "MEMS pressure sensor: 260-1260 hPa absolute digital output barometer" Data Sheet
// http://www.st.com/content/ccc/resource/technical/document/datasheet/bf/c1/4f/23/61/17/44/8a/DM00140895.pdf/files/DM00140895.pdf/jcr:content/translations/en.DM00140895.pdf
#define LPS22H_INTERRUPT_CFG 0x0B
#define LPS22H_THS_P_L 0x0C
#define LPS22H_THS_P_H 0x0D
#define LPS22H_WHOAMI 0x0F // should return 0xB1
#define LPS22H_CTRL_REG1 0x10
#define LPS22H_CTRL_REG2 0x11
#define LPS22H_CTRL_REG3 0x12
#define LPS22H_FIFO_CTRL 0x14
#define LPS22H_REF_P_XL 0x15
#define LPS22H_REF_P_L 0x16
#define LPS22H_REF_P_H 0x17
#define LPS22H_RPDS_L 0x18
#define LPS22H_RPDS_H 0x19
#define LPS22H_RES_CONF 0x1A
#define LPS22H_INT_SOURCE 0x25
#define LPS22H_FIFO_STATUS 0x26
#define LPS22H_STATUS 0x27
#define LPS22H_PRESS_OUT_XL 0x28
#define LPS22H_PRESS_OUT_L 0x29
#define LPS22H_PRESS_OUT_H 0x2A
#define LPS22H_TEMP_OUT_L 0x2B
#define LPS22H_TEMP_OUT_H 0x2C
#define LPS22H_LPFP_RES 0x33
#define LPS22H_ADDRESS 0x5C // Address of altimeter
// Altimeter output data rate
#define P_1shot 0x00;
#define P_1Hz 0x01;
#define P_10Hz 0x02;
#define P_25Hz 0x03; // 25 Hz output data rate
#define P_50Hz 0x04;
#define P_75Hz 0x05;
class LPS22H
{
public:
LPS22H(uint8_t intPin);
void Init(uint8_t PODR);
uint8_t getChipID();
uint8_t status();
int32_t readAltimeterPressure();
int16_t readAltimeterTemperature();
void I2Cscan();
void writeByte(uint8_t address, uint8_t subAddress, uint8_t data);
uint8_t readByte(uint8_t address, uint8_t subAddress);
void readBytes(uint8_t address, uint8_t subAddress, uint8_t count, uint8_t * dest);
private:
uint8_t _intPin;
};
#endif

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EM7180_LSM6DSM_LIS2MDL_LPS22HB_Butterfly/LSM6DSM.cpp
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/* 09/23/2017 Copyright Tlera Corporation
Created by Kris Winer
This sketch uses SDA/SCL on pins 21/20 (Butterfly default), respectively, and it uses the Butterfly STM32L433CU Breakout Board.
The LSM6DSM is a sensor hub with embedded accel and gyro, here used as 6 DoF in a 9 DoF absolute orientation solution.
Library may be used freely and without limit with attribution.
*/
#include "LSM6DSM.h"
LSM6DSM::LSM6DSM(uint8_t intPin1, uint8_t intPin2)
{
pinMode(intPin1, INPUT);
_intPin1 = intPin1;
pinMode(intPin2, INPUT);
_intPin2 = intPin2;
}
uint8_t LSM6DSM::getChipID()
{
uint8_t c = readByte(LSM6DSM_ADDRESS, LSM6DSM_WHO_AM_I);
return c;
}
float LSM6DSM::getAres(uint8_t Ascale) {
switch (Ascale)
{
// Possible accelerometer scales (and their register bit settings) are:
// 2 Gs (00), 4 Gs (01), 8 Gs (10), and 16 Gs (11).
// Here's a bit of an algorithm to calculate DPS/(ADC tick) based on that 2-bit value:
case AFS_2G:
_aRes = 2.0f/32768.0f;
return _aRes;
break;
case AFS_4G:
_aRes = 4.0f/32768.0f;
return _aRes;
break;
case AFS_8G:
_aRes = 8.0f/32768.0f;
return _aRes;
break;
case AFS_16G:
_aRes = 16.0f/32768.0f;
return _aRes;
break;
}
}
float LSM6DSM::getGres(uint8_t Gscale) {
switch (Gscale)
{
// Possible gyro scales (and their register bit settings) are:
// 250 DPS (00), 500 DPS (01), 1000 DPS (10), and 2000 DPS (11).
case GFS_245DPS:
_gRes = 245.0f/32768.0f;
return _gRes;
break;
case GFS_500DPS:
_gRes = 500.0f/32768.0f;
return _gRes;
break;
case GFS_1000DPS:
_gRes = 1000.0f/32768.0f;
return _gRes;
break;
case GFS_2000DPS:
_gRes = 2000.0f/32768.0f;
return _gRes;
break;
}
}
void LSM6DSM::reset()
{
// reset device
uint8_t temp = readByte(LSM6DSM_ADDRESS, LSM6DSM_CTRL3_C);
writeByte(LSM6DSM_ADDRESS, LSM6DSM_CTRL3_C, temp | 0x01); // Set bit 0 to 1 to reset LSM6DSM
delay(100); // Wait for all registers to reset
}
void LSM6DSM::init(uint8_t Ascale, uint8_t Gscale, uint8_t AODR, uint8_t GODR)
{
writeByte(LSM6DSM_ADDRESS, LSM6DSM_CTRL1_XL, AODR << 4 | Ascale << 2);
writeByte(LSM6DSM_ADDRESS, LSM6DSM_CTRL2_G, GODR << 4 | Gscale << 2);
uint8_t temp = readByte(LSM6DSM_ADDRESS, LSM6DSM_CTRL3_C);
// enable block update (bit 6 = 1), auto-increment registers (bit 2 = 1)
writeByte(LSM6DSM_ADDRESS, LSM6DSM_CTRL3_C, temp | 0x40 | 0x04);
// by default, interrupts active HIGH, push pull, little endian data
// (can be changed by writing to bits 5, 4, and 1, resp to above register)
// enable accel LP2 (bit 7 = 1), set LP2 tp ODR/9 (bit 6 = 1), enable input_composite (bit 3) for low noise
writeByte(LSM6DSM_ADDRESS, LSM6DSM_CTRL8_XL, 0x80 | 0x40 | 0x08 );
// interrupt handling
writeByte(LSM6DSM_ADDRESS, LSM6DSM_DRDY_PULSE_CFG, 0x80); // latch interrupt until data read
writeByte(LSM6DSM_ADDRESS, LSM6DSM_INT1_CTRL, 0x40); // enable significant motion interrupts on INT1
writeByte(LSM6DSM_ADDRESS, LSM6DSM_INT2_CTRL, 0x03); // enable accel/gyro data ready interrupts on INT2
}
void LSM6DSM::selfTest()
{
int16_t temp[7] = {0, 0, 0, 0, 0, 0, 0};
int16_t accelPTest[3] = {0, 0, 0}, accelNTest[3] = {0, 0, 0}, gyroPTest[3] = {0, 0, 0}, gyroNTest[3] = {0, 0, 0};
int16_t accelNom[3] = {0, 0, 0}, gyroNom[3] = {0, 0, 0};
readData(temp);
accelNom[0] = temp[4];
accelNom[1] = temp[5];
accelNom[2] = temp[6];
gyroNom[0] = temp[1];
gyroNom[1] = temp[2];
gyroNom[2] = temp[3];
writeByte(LSM6DSM_ADDRESS, LSM6DSM_CTRL5_C, 0x01); // positive accel self test
delay(100); // let accel respond
readData(temp);
accelPTest[0] = temp[4];
accelPTest[1] = temp[5];
accelPTest[2] = temp[6];
writeByte(LSM6DSM_ADDRESS, LSM6DSM_CTRL5_C, 0x03); // negative accel self test
delay(100); // let accel respond
readData(temp);
accelNTest[0] = temp[4];
accelNTest[1] = temp[5];
accelNTest[2] = temp[6];
writeByte(LSM6DSM_ADDRESS, LSM6DSM_CTRL5_C, 0x04); // positive gyro self test
delay(100); // let gyro respond
readData(temp);
gyroPTest[0] = temp[1];
gyroPTest[1] = temp[2];
gyroPTest[2] = temp[3];
writeByte(LSM6DSM_ADDRESS, LSM6DSM_CTRL5_C, 0x0C); // negative gyro self test
delay(100); // let gyro respond
readData(temp);
gyroNTest[0] = temp[1];
gyroNTest[1] = temp[2];
gyroNTest[2] = temp[3];
writeByte(LSM6DSM_ADDRESS, LSM6DSM_CTRL5_C, 0x00); // normal mode
delay(100); // let accel and gyro respond
Serial.println("Accel Self Test:");
Serial.print("+Ax results:"); Serial.print( (accelPTest[0] - accelNom[0]) * _aRes * 1000.0); Serial.println(" mg");
Serial.print("-Ax results:"); Serial.println((accelNTest[0] - accelNom[0]) * _aRes * 1000.0);
Serial.print("+Ay results:"); Serial.println((accelPTest[1] - accelNom[1]) * _aRes * 1000.0);
Serial.print("-Ay results:"); Serial.println((accelNTest[1] - accelNom[1]) * _aRes * 1000.0);
Serial.print("+Az results:"); Serial.println((accelPTest[2] - accelNom[2]) * _aRes * 1000.0);
Serial.print("-Az results:"); Serial.println((accelNTest[2] - accelNom[2]) * _aRes * 1000.0);
Serial.println("Should be between 90 and 1700 mg");
Serial.println("Gyro Self Test:");
Serial.print("+Gx results:"); Serial.print((gyroPTest[0] - gyroNom[0]) * _gRes); Serial.println(" dps");
Serial.print("-Gx results:"); Serial.println((gyroNTest[0] - gyroNom[0]) * _gRes);
Serial.print("+Gy results:"); Serial.println((gyroPTest[1] - gyroNom[1]) * _gRes);
Serial.print("-Gy results:"); Serial.println((gyroNTest[1] - gyroNom[1]) * _gRes);
Serial.print("+Gz results:"); Serial.println((gyroPTest[2] - gyroNom[2]) * _gRes);
Serial.print("-Gz results:"); Serial.println((gyroNTest[2] - gyroNom[2]) * _gRes);
Serial.println("Should be between 20 and 80 dps");
delay(2000);
}
void LSM6DSM::offsetBias(float * dest1, float * dest2)
{
int16_t temp[7] = {0, 0, 0, 0, 0, 0, 0};
int32_t sum[7] = {0, 0, 0, 0, 0, 0, 0};
Serial.println("Calculate accel and gyro offset biases: keep sensor flat and motionless!");
delay(4000);
for (int ii = 0; ii < 128; ii++)
{
readData(temp);
sum[1] += temp[1];
sum[2] += temp[2];
sum[3] += temp[3];
sum[4] += temp[4];
sum[5] += temp[5];
sum[6] += temp[6];
delay(50);
}
dest1[0] = sum[1]*_gRes/128.0f;
dest1[1] = sum[2]*_gRes/128.0f;
dest1[2] = sum[3]*_gRes/128.0f;
dest2[0] = sum[4]*_aRes/128.0f;
dest2[1] = sum[5]*_aRes/128.0f;
dest2[2] = sum[6]*_aRes/128.0f;
if(dest2[0] > 0.8f) {dest2[0] -= 1.0f;} // Remove gravity from the x-axis accelerometer bias calculation
if(dest2[0] < -0.8f) {dest2[0] += 1.0f;} // Remove gravity from the x-axis accelerometer bias calculation
if(dest2[1] > 0.8f) {dest2[1] -= 1.0f;} // Remove gravity from the y-axis accelerometer bias calculation
if(dest2[1] < -0.8f) {dest2[1] += 1.0f;} // Remove gravity from the y-axis accelerometer bias calculation
if(dest2[2] > 0.8f) {dest2[2] -= 1.0f;} // Remove gravity from the z-axis accelerometer bias calculation
if(dest2[2] < -0.8f) {dest2[2] += 1.0f;} // Remove gravity from the z-axis accelerometer bias calculation
}
void LSM6DSM::readData(int16_t * destination)
{
uint8_t rawData[14]; // x/y/z accel register data stored here
readBytes(LSM6DSM_ADDRESS, LSM6DSM_OUT_TEMP_L, 14, &rawData[0]); // Read the 14 raw data registers into data array
destination[0] = ((int16_t)rawData[1] << 8) | rawData[0] ; // Turn the MSB and LSB into a signed 16-bit value
destination[1] = ((int16_t)rawData[3] << 8) | rawData[2] ;
destination[2] = ((int16_t)rawData[5] << 8) | rawData[4] ;
destination[3] = ((int16_t)rawData[7] << 8) | rawData[6] ;
destination[4] = ((int16_t)rawData[9] << 8) | rawData[8] ;
destination[5] = ((int16_t)rawData[11] << 8) | rawData[10] ;
destination[6] = ((int16_t)rawData[13] << 8) | rawData[12] ;
}
// I2C scan function
void LSM6DSM::I2Cscan()
{
// scan for i2c devices
byte error, address;
int nDevices;
Serial.println("Scanning...");
nDevices = 0;
for(address = 1; address < 127; address++ )
{
// The i2c_scanner uses the return value of
// the Write.endTransmission to see if
// a device did acknowledge to the address.
// Wire.beginTransmission(address);
// error = Wire.endTransmission();
error = Wire.transfer(address, NULL, 0, NULL, 0);
if (error == 0)
{
Serial.print("I2C device found at address 0x");
if (address<16)
Serial.print("0");
Serial.print(address,HEX);
Serial.println(" !");
nDevices++;
}
else if (error==4)
{
Serial.print("Unknown error at address 0x");
if (address<16)
Serial.print("0");
Serial.println(address,HEX);
}
}
if (nDevices == 0)
Serial.println("No I2C devices found\n");
else
Serial.println("done\n");
}
// I2C read/write functions for the LSM6DSM
void LSM6DSM::writeByte(uint8_t address, uint8_t subAddress, uint8_t data) {
uint8_t temp[2];
temp[0] = subAddress;
temp[1] = data;
Wire.transfer(address, &temp[0], 2, NULL, 0);
}
uint8_t LSM6DSM::readByte(uint8_t address, uint8_t subAddress) {
uint8_t temp[1];
Wire.transfer(address, &subAddress, 1, &temp[0], 1);
return temp[0];
}
void LSM6DSM::readBytes(uint8_t address, uint8_t subAddress, uint8_t count, uint8_t * dest) {
Wire.transfer(address, &subAddress, 1, dest, count);
}

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EM7180_LSM6DSM_LIS2MDL_LPS22HB_Butterfly/LSM6DSM.h
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/* 09/23/2017 Copyright Tlera Corporation
Created by Kris Winer
This sketch uses SDA/SCL on pins 21/20 (Butterfly default), respectively, and it uses the Butterfly STM32L433CU Breakout Board.
The LSM6DSM is a sensor hub with embedded accel and gyro, here used as 6 DoF in a 9 DoF absolute orientation solution.
Library may be used freely and without limit with attribution.
*/
#ifndef LSM6DSM_h
#define LSM6DSM_h
#include "Arduino.h"
#include <Wire.h>
/* LSM6DSM registers
http://www.st.com/content/ccc/resource/technical/document/datasheet/76/27/cf/88/c5/03/42/6b/DM00218116.pdf/files/DM00218116.pdf/jcr:content/translations/en.DM00218116.pdf
*/
#define LSM6DSM_FUNC_CFG_ACCESS 0x01
#define LSM6DSM_SENSOR_SYNC_TIME_FRAME 0x04
#define LSM6DSM_SENSOR_SYNC_RES_RATIO 0x05
#define LSM6DSM_FIFO_CTRL1 0x06
#define LSM6DSM_FIFO_CTRL2 0x07
#define LSM6DSM_FIFO_CTRL3 0x08
#define LSM6DSM_FIFO_CTRL4 0x09
#define LSM6DSM_FIFO_CTRL5 0x0A
#define LSM6DSM_DRDY_PULSE_CFG 0x0B
#define LSM6DSM_INT1_CTRL 0x0D
#define LSM6DSM_INT2_CTRL 0x0E
#define LSM6DSM_WHO_AM_I 0x0F // should be 0x6A
#define LSM6DSM_CTRL1_XL 0x10
#define LSM6DSM_CTRL2_G 0x11
#define LSM6DSM_CTRL3_C 0x12
#define LSM6DSM_CTRL4_C 0x13
#define LSM6DSM_CTRL5_C 0x14
#define LSM6DSM_CTRL6_C 0x15
#define LSM6DSM_CTRL7_G 0x16
#define LSM6DSM_CTRL8_XL 0x17
#define LSM6DSM_CTRL9_XL 0x18
#define LSM6DSM_CTRL10_C 0x19
#define LSM6DSM_MASTER_CONFIG 0x1A
#define LSM6DSM_WAKE_UP_SRC 0x1B
#define LSM6DSM_TAP_SRC 0x1C
#define LSM6DSM_D6D_SRC 0x1D
#define LSM6DSM_STATUS_REG 0x1E
#define LSM6DSM_OUT_TEMP_L 0x20
#define LSM6DSM_OUT_TEMP_H 0x21
#define LSM6DSM_OUTX_L_G 0x22
#define LSM6DSM_OUTX_H_G 0x23
#define LSM6DSM_OUTY_L_G 0x24
#define LSM6DSM_OUTY_H_G 0x25
#define LSM6DSM_OUTZ_L_G 0x26
#define LSM6DSM_OUTZ_H_G 0x27
#define LSM6DSM_OUTX_L_XL 0x28
#define LSM6DSM_OUTX_H_XL 0x29
#define LSM6DSM_OUTY_L_XL 0x2A
#define LSM6DSM_OUTY_H_XL 0x2B
#define LSM6DSM_OUTZ_L_XL 0x2C
#define LSM6DSM_OUTZ_H_XL 0x2D
#define LSM6DSM_SENSORHUB1_REG 0x2E
#define LSM6DSM_SENSORHUB2_REG 0x2F
#define LSM6DSM_SENSORHUB3_REG 0x30
#define LSM6DSM_SENSORHUB4_REG 0x31
#define LSM6DSM_SENSORHUB5_REG 0x32
#define LSM6DSM_SENSORHUB6_REG 0x33
#define LSM6DSM_SENSORHUB7_REG 0x34
#define LSM6DSM_SENSORHUB8_REG 0x35
#define LSM6DSM_SENSORHUB9_REG 0x36
#define LSM6DSM_SENSORHUB10_REG 0x37
#define LSM6DSM_SENSORHUB11_REG 0x38
#define LSM6DSM_SENSORHUB12_REG 0x39
#define LSM6DSM_FIFO_STATUS1 0x3A
#define LSM6DSM_FIFO_STATUS2 0x3B
#define LSM6DSM_FIFO_STATUS3 0x3C
#define LSM6DSM_FIFO_STATUS4 0x3D
#define LSM6DSM_FIFO_DATA_OUT_L 0x3E
#define LSM6DSM_FIFO_DATA_OUT_H 0x3F
#define LSM6DSM_TIMESTAMP0_REG 0x40
#define LSM6DSM_TIMESTAMP1_REG 0x41
#define LSM6DSM_TIMESTAMP2_REG 0x42
#define LSM6DSM_STEP_TIMESTAMP_L 0x49
#define LSM6DSM_STEP_TIMESTAMP_H 0x4A
#define LSM6DSM_STEP_COUNTER_L 0x4B
#define LSM6DSM_STEP_COUNTER_H 0x4C
#define LSM6DSM_SENSORHUB13_REG 0x4D
#define LSM6DSM_SENSORHUB14_REG 0x4E
#define LSM6DSM_SENSORHUB15_REG 0x4F
#define LSM6DSM_SENSORHUB16_REG 0x50
#define LSM6DSM_SENSORHUB17_REG 0x51
#define LSM6DSM_SENSORHUB18_REG 0x52
#define LSM6DSM_FUNC_SRC1 0x53
#define LSM6DSM_FUNC_SRC2 0x54
#define LSM6DSM_WRIST_TILT_IA 0x55
#define LSM6DSM_TAP_CFG 0x58
#define LSM6DSM_TAP_THS_6D 0x59
#define LSM6DSM_INT_DUR2 0x5A
#define LSM6DSM_WAKE_UP_THS 0x5B
#define LSM6DSM_WAKE_UP_DUR 0x5C
#define LSM6DSM_FREE_FALL 0x5D
#define LSM6DSM_MD1_CFG 0x5E
#define LSM6DSM_MD2_CFG 0x5F
#define LSM6DSM_MASTER_MODE_CODE 0x60
#define LSM6DSM_SENS_SYNC_SPI_ERROR_CODE 0x61
#define LSM6DSM_OUT_MAG_RAW_X_L 0x66
#define LSM6DSM_OUT_MAG_RAW_X_H 0x67
#define LSM6DSM_OUT_MAG_RAW_Y_L 0x68
#define LSM6DSM_OUT_MAG_RAW_Y_H 0x69
#define LSM6DSM_OUT_MAG_RAW_Z_L 0x6A
#define LSM6DSM_OUT_MAG_RAW_Z_H 0x6B
#define LSM6DSM_INT_OIS 0x6F
#define LSM6DSM_CTRL1_OIS 0x70
#define LSM6DSM_CTRL2_OIS 0x71
#define LSM6DSM_CTRL3_OIS 0x72
#define LSM6DSM_X_OFS_USR 0x73
#define LSM6DSM_Y_OFS_USR 0x74
#define LSM6DSM_Z_OFS_USR 0x75
#define LSM6DSM_ADDRESS 0x6A // Address of LSM6DSM accel/gyro when ADO = 0
#define AFS_2G 0x00
#define AFS_4G 0x02
#define AFS_8G 0x03
#define AFS_16G 0x01
#define GFS_245DPS 0x00
#define GFS_500DPS 0x01
#define GFS_1000DPS 0x02
#define GFS_2000DPS 0x03
#define AODR_12_5Hz 0x01 // same for accel and gyro in normal mode
#define AODR_26Hz 0x02
#define AODR_52Hz 0x03
#define AODR_104Hz 0x04
#define AODR_208Hz 0x05
#define AODR_416Hz 0x06
#define AODR_833Hz 0x07
#define AODR_1660Hz 0x08
#define AODR_3330Hz 0x09
#define AODR_6660Hz 0x0A
#define GODR_12_5Hz 0x01
#define GODR_26Hz 0x02
#define GODR_52Hz 0x03
#define GODR_104Hz 0x04
#define GODR_208Hz 0x05
#define GODR_416Hz 0x06
#define GODR_833Hz 0x07
#define GODR_1660Hz 0x08
#define GODR_3330Hz 0x09
#define GODR_6660Hz 0x0A
class LSM6DSM
{
public:
LSM6DSM(uint8_t intPin1, uint8_t intPin2);
float getAres(uint8_t Ascale);
float getGres(uint8_t Gscale);
uint8_t getChipID();
void init(uint8_t Ascale, uint8_t Gscale, uint8_t AODR, uint8_t GODR);
void offsetBias(float * dest1, float * dest2);
void reset();
void selfTest();
void readData(int16_t * destination);
void I2Cscan();
void writeByte(uint8_t address, uint8_t subAddress, uint8_t data);
uint8_t readByte(uint8_t address, uint8_t subAddress);
void readBytes(uint8_t address, uint8_t subAddress, uint8_t count, uint8_t * dest);
private:
uint8_t _intPin1;
uint8_t _intPin2;
float _aRes, _gRes;
};
#endif

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// Implementation of Sebastian Madgwick's "...efficient orientation filter for... inertial/magnetic sensor arrays"
// (see http://www.x-io.co.uk/category/open-source/ for examples and more details)
// which fuses acceleration, rotation rate, and magnetic moments to produce a quaternion-based estimate of absolute
// device orientation -- which can be converted to yaw, pitch, and roll. Useful for stabilizing quadcopters, etc.
// The performance of the orientation filter is at least as good as conventional Kalman-based filtering algorithms
// but is much less computationally intensive---it can be performed on a 3.3 V Pro Mini operating at 8 MHz!
__attribute__((optimize("O3"))) void MadgwickQuaternionUpdate(float ax, float ay, float az, float gx, float gy, float gz, float mx, float my, float mz)
{
float q1 = q[0], q2 = q[1], q3 = q[2], q4 = q[3]; // short name local variable for readability
float norm;
float hx, hy, _2bx, _2bz;
float s1, s2, s3, s4;
float qDot1, qDot2, qDot3, qDot4;
// Auxiliary variables to avoid repeated arithmetic
float _2q1mx;
float _2q1my;
float _2q1mz;
float _2q2mx;
float _4bx;
float _4bz;
float _2q1 = 2.0f * q1;
float _2q2 = 2.0f * q2;
float _2q3 = 2.0f * q3;
float _2q4 = 2.0f * q4;
float _2q1q3 = 2.0f * q1 * q3;
float _2q3q4 = 2.0f * q3 * q4;
float q1q1 = q1 * q1;
float q1q2 = q1 * q2;
float q1q3 = q1 * q3;
float q1q4 = q1 * q4;
float q2q2 = q2 * q2;
float q2q3 = q2 * q3;
float q2q4 = q2 * q4;
float q3q3 = q3 * q3;
float q3q4 = q3 * q4;
float q4q4 = q4 * q4;
// Normalise accelerometer measurement
norm = sqrtf(ax * ax + ay * ay + az * az);
if (norm == 0.0f) return; // handle NaN
norm = 1.0f/norm;
ax *= norm;
ay *= norm;
az *= norm;
// Normalise magnetometer measurement
norm = sqrtf(mx * mx + my * my + mz * mz);
if (norm == 0.0f) return; // handle NaN
norm = 1.0f/norm;
mx *= norm;
my *= norm;
mz *= norm;
// Reference direction of Earth's magnetic field
_2q1mx = 2.0f * q1 * mx;
_2q1my = 2.0f * q1 * my;
_2q1mz = 2.0f * q1 * mz;
_2q2mx = 2.0f * q2 * mx;
hx = mx * q1q1 - _2q1my * q4 + _2q1mz * q3 + mx * q2q2 + _2q2 * my * q3 + _2q2 * mz * q4 - mx * q3q3 - mx * q4q4;
hy = _2q1mx * q4 + my * q1q1 - _2q1mz * q2 + _2q2mx * q3 - my * q2q2 + my * q3q3 + _2q3 * mz * q4 - my * q4q4;
_2bx = sqrtf(hx * hx + hy * hy);
_2bz = -_2q1mx * q3 + _2q1my * q2 + mz * q1q1 + _2q2mx * q4 - mz * q2q2 + _2q3 * my * q4 - mz * q3q3 + mz * q4q4;
_4bx = 2.0f * _2bx;
_4bz = 2.0f * _2bz;
// Gradient decent algorithm corrective step
s1 = -_2q3 * (2.0f * q2q4 - _2q1q3 - ax) + _2q2 * (2.0f * q1q2 + _2q3q4 - ay) - _2bz * q3 * (_2bx * (0.5f - q3q3 - q4q4) + _2bz * (q2q4 - q1q3) - mx) + (-_2bx * q4 + _2bz * q2) * (_2bx * (q2q3 - q1q4) + _2bz * (q1q2 + q3q4) - my) + _2bx * q3 * (_2bx * (q1q3 + q2q4) + _2bz * (0.5f - q2q2 - q3q3) - mz);
s2 = _2q4 * (2.0f * q2q4 - _2q1q3 - ax) + _2q1 * (2.0f * q1q2 + _2q3q4 - ay) - 4.0f * q2 * (1.0f - 2.0f * q2q2 - 2.0f * q3q3 - az) + _2bz * q4 * (_2bx * (0.5f - q3q3 - q4q4) + _2bz * (q2q4 - q1q3) - mx) + (_2bx * q3 + _2bz * q1) * (_2bx * (q2q3 - q1q4) + _2bz * (q1q2 + q3q4) - my) + (_2bx * q4 - _4bz * q2) * (_2bx * (q1q3 + q2q4) + _2bz * (0.5f - q2q2 - q3q3) - mz);
s3 = -_2q1 * (2.0f * q2q4 - _2q1q3 - ax) + _2q4 * (2.0f * q1q2 + _2q3q4 - ay) - 4.0f * q3 * (1.0f - 2.0f * q2q2 - 2.0f * q3q3 - az) + (-_4bx * q3 - _2bz * q1) * (_2bx * (0.5f - q3q3 - q4q4) + _2bz * (q2q4 - q1q3) - mx) + (_2bx * q2 + _2bz * q4) * (_2bx * (q2q3 - q1q4) + _2bz * (q1q2 + q3q4) - my) + (_2bx * q1 - _4bz * q3) * (_2bx * (q1q3 + q2q4) + _2bz * (0.5f - q2q2 - q3q3) - mz);
s4 = _2q2 * (2.0f * q2q4 - _2q1q3 - ax) + _2q3 * (2.0f * q1q2 + _2q3q4 - ay) + (-_4bx * q4 + _2bz * q2) * (_2bx * (0.5f - q3q3 - q4q4) + _2bz * (q2q4 - q1q3) - mx) + (-_2bx * q1 + _2bz * q3) * (_2bx * (q2q3 - q1q4) + _2bz * (q1q2 + q3q4) - my) + _2bx * q2 * (_2bx * (q1q3 + q2q4) + _2bz * (0.5f - q2q2 - q3q3) - mz);
norm = sqrtf(s1 * s1 + s2 * s2 + s3 * s3 + s4 * s4); // normalise step magnitude
norm = 1.0f/norm;
s1 *= norm;
s2 *= norm;
s3 *= norm;
s4 *= norm;
// Compute rate of change of quaternion
qDot1 = 0.5f * (-q2 * gx - q3 * gy - q4 * gz) - beta * s1;
qDot2 = 0.5f * (q1 * gx + q3 * gz - q4 * gy) - beta * s2;
qDot3 = 0.5f * (q1 * gy - q2 * gz + q4 * gx) - beta * s3;
qDot4 = 0.5f * (q1 * gz + q2 * gy - q3 * gx) - beta * s4;
// Integrate to yield quaternion
q1 += qDot1 * deltat;
q2 += qDot2 * deltat;
q3 += qDot3 * deltat;
q4 += qDot4 * deltat;
norm = sqrtf(q1 * q1 + q2 * q2 + q3 * q3 + q4 * q4); // normalise quaternion
norm = 1.0f/norm;
q[0] = q1 * norm;
q[1] = q2 * norm;
q[2] = q3 * norm;
q[3] = q4 * norm;
}

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EM7180_LSM6DSM_LIS2MDL_LPS22HB_Butterfly/USFS.cpp
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EM7180_LSM6DSM_LIS2MDL_LPS22HB_Butterfly/USFS.h
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#ifndef USFS_h
#define USFSh_h
#include "Arduino.h"
#include "Wire.h"
// See MS5637-02BA03 Low Voltage Barometric Pressure Sensor Data Sheet
#define MS5637_RESET 0x1E
#define MS5637_CONVERT_D1 0x40
#define MS5637_CONVERT_D2 0x50
#define MS5637_ADC_READ 0x00
// 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
//
//Magnetometer Registers
#define AK8963_ADDRESS 0x0C
#define WHO_AM_I_AK8963 0x00 // should return 0x48
#define INFO 0x01
#define AK8963_ST1 0x02 // data ready status bit 0
#define AK8963_XOUT_L 0x03 // data
#define AK8963_XOUT_H 0x04
#define AK8963_YOUT_L 0x05
#define AK8963_YOUT_H 0x06
#define AK8963_ZOUT_L 0x07
#define AK8963_ZOUT_H 0x08
#define AK8963_ST2 0x09 // Data overflow bit 3 and data read error status bit 2
#define AK8963_CNTL 0x0A // Power down (0000), single-measurement (0001), self-test (1000) and Fuse ROM (1111) modes on bits 3:0
#define AK8963_ASTC 0x0C // Self test control
#define AK8963_I2CDIS 0x0F // I2C disable
#define AK8963_ASAX 0x10 // Fuse ROM x-axis sensitivity adjustment value
#define AK8963_ASAY 0x11 // Fuse ROM y-axis sensitivity adjustment value
#define AK8963_ASAZ 0x12 // Fuse ROM z-axis sensitivity adjustment value
#define SELF_TEST_X_GYRO 0x00
#define SELF_TEST_Y_GYRO 0x01
#define SELF_TEST_Z_GYRO 0x02
/*#define X_FINE_GAIN 0x03 // [7:0] fine gain
#define Y_FINE_GAIN 0x04
#define Z_FINE_GAIN 0x05
#define XA_OFFSET_H 0x06 // User-defined trim values for accelerometer
#define XA_OFFSET_L_TC 0x07
#define YA_OFFSET_H 0x08
#define YA_OFFSET_L_TC 0x09
#define ZA_OFFSET_H 0x0A
#define ZA_OFFSET_L_TC 0x0B */
#define SELF_TEST_X_ACCEL 0x0D
#define SELF_TEST_Y_ACCEL 0x0E
#define SELF_TEST_Z_ACCEL 0x0F
#define SELF_TEST_A 0x10
#define XG_OFFSET_H 0x13 // User-defined trim values for gyroscope
#define XG_OFFSET_L 0x14
#define YG_OFFSET_H 0x15
#define YG_OFFSET_L 0x16
#define ZG_OFFSET_H 0x17
#define ZG_OFFSET_L 0x18
#define SMPLRT_DIV 0x19
#define CONFIG 0x1A
#define GYRO_CONFIG 0x1B
#define ACCEL_CONFIG 0x1C
#define ACCEL_CONFIG2 0x1D
#define LP_ACCEL_ODR 0x1E
#define WOM_THR 0x1F
#define MOT_DUR 0x20 // Duration counter threshold for motion interrupt generation, 1 kHz rate, LSB = 1 ms
#define ZMOT_THR 0x21 // Zero-motion detection threshold bits [7:0]
#define ZRMOT_DUR 0x22 // Duration counter threshold for zero motion interrupt generation, 16 Hz rate, LSB = 64 ms
#define FIFO_EN 0x23
#define I2C_MST_CTRL 0x24
#define I2C_SLV0_ADDR 0x25
#define I2C_SLV0_REG 0x26
#define I2C_SLV0_CTRL 0x27
#define I2C_SLV1_ADDR 0x28
#define I2C_SLV1_REG 0x29
#define I2C_SLV1_CTRL 0x2A
#define I2C_SLV2_ADDR 0x2B
#define I2C_SLV2_REG 0x2C
#define I2C_SLV2_CTRL 0x2D
#define I2C_SLV3_ADDR 0x2E
#define I2C_SLV3_REG 0x2F
#define I2C_SLV3_CTRL 0x30
#define I2C_SLV4_ADDR 0x31
#define I2C_SLV4_REG 0x32
#define I2C_SLV4_DO 0x33
#define I2C_SLV4_CTRL 0x34
#define I2C_SLV4_DI 0x35
#define I2C_MST_STATUS 0x36
#define INT_PIN_CFG 0x37
#define INT_ENABLE 0x38
#define DMP_INT_STATUS 0x39 // Check DMP interrupt
#define INT_STATUS 0x3A
#define ACCEL_XOUT_H 0x3B
#define ACCEL_XOUT_L 0x3C
#define ACCEL_YOUT_H 0x3D
#define ACCEL_YOUT_L 0x3E
#define ACCEL_ZOUT_H 0x3F
#define ACCEL_ZOUT_L 0x40
#define TEMP_OUT_H 0x41
#define TEMP_OUT_L 0x42
#define GYRO_XOUT_H 0x43
#define GYRO_XOUT_L 0x44
#define GYRO_YOUT_H 0x45
#define GYRO_YOUT_L 0x46
#define GYRO_ZOUT_H 0x47
#define GYRO_ZOUT_L 0x48
#define EXT_SENS_DATA_00 0x49
#define EXT_SENS_DATA_01 0x4A
#define EXT_SENS_DATA_02 0x4B
#define EXT_SENS_DATA_03 0x4C
#define EXT_SENS_DATA_04 0x4D
#define EXT_SENS_DATA_05 0x4E
#define EXT_SENS_DATA_06 0x4F
#define EXT_SENS_DATA_07 0x50
#define EXT_SENS_DATA_08 0x51
#define EXT_SENS_DATA_09 0x52
#define EXT_SENS_DATA_10 0x53
#define EXT_SENS_DATA_11 0x54
#define EXT_SENS_DATA_12 0x55
#define EXT_SENS_DATA_13 0x56
#define EXT_SENS_DATA_14 0x57
#define EXT_SENS_DATA_15 0x58
#define EXT_SENS_DATA_16 0x59
#define EXT_SENS_DATA_17 0x5A
#define EXT_SENS_DATA_18 0x5B
#define EXT_SENS_DATA_19 0x5C
#define EXT_SENS_DATA_20 0x5D
#define EXT_SENS_DATA_21 0x5E
#define EXT_SENS_DATA_22 0x5F
#define EXT_SENS_DATA_23 0x60
#define MOT_DETECT_STATUS 0x61
#define I2C_SLV0_DO 0x63
#define I2C_SLV1_DO 0x64
#define I2C_SLV2_DO 0x65
#define I2C_SLV3_DO 0x66
#define I2C_MST_DELAY_CTRL 0x67
#define SIGNAL_PATH_RESET 0x68
#define MOT_DETECT_CTRL 0x69
#define USER_CTRL 0x6A // Bit 7 enable DMP, bit 3 reset DMP
#define PWR_MGMT_1 0x6B // Device defaults to the SLEEP mode
#define PWR_MGMT_2 0x6C
#define DMP_BANK 0x6D // Activates a specific bank in the DMP
#define DMP_RW_PNT 0x6E // Set read/write pointer to a specific start address in specified DMP bank
#define DMP_REG 0x6F // Register in DMP from which to read or to which to write
#define DMP_REG_1 0x70
#define DMP_REG_2 0x71
#define FIFO_COUNTH 0x72
#define FIFO_COUNTL 0x73
#define FIFO_R_W 0x74
#define WHO_AM_I_MPU9250 0x75 // Should return 0x71
#define XA_OFFSET_H 0x77
#define XA_OFFSET_L 0x78
#define YA_OFFSET_H 0x7A
#define YA_OFFSET_L 0x7B
#define ZA_OFFSET_H 0x7D
#define ZA_OFFSET_L 0x7E
// EM7180 SENtral register map
// see http://www.emdeveloper.com/downloads/7180/EMSentral_EM7180_Register_Map_v1_3.pdf
//
#define EM7180_QX 0x00 // this is a 32-bit normalized floating point number read from registers 0x00-03
#define EM7180_QY 0x04 // this is a 32-bit normalized floating point number read from registers 0x04-07
#define EM7180_QZ 0x08 // this is a 32-bit normalized floating point number read from registers 0x08-0B
#define EM7180_QW 0x0C // this is a 32-bit normalized floating point number read from registers 0x0C-0F
#define EM7180_QTIME 0x10 // this is a 16-bit unsigned integer read from registers 0x10-11
#define EM7180_MX 0x12 // int16_t from registers 0x12-13
#define EM7180_MY 0x14 // int16_t from registers 0x14-15
#define EM7180_MZ 0x16 // int16_t from registers 0x16-17
#define EM7180_MTIME 0x18 // uint16_t from registers 0x18-19
#define EM7180_AX 0x1A // int16_t from registers 0x1A-1B
#define EM7180_AY 0x1C // int16_t from registers 0x1C-1D
#define EM7180_AZ 0x1E // int16_t from registers 0x1E-1F
#define EM7180_ATIME 0x20 // uint16_t from registers 0x20-21
#define EM7180_GX 0x22 // int16_t from registers 0x22-23
#define EM7180_GY 0x24 // int16_t from registers 0x24-25
#define EM7180_GZ 0x26 // int16_t from registers 0x26-27
#define EM7180_GTIME 0x28 // uint16_t from registers 0x28-29
#define EM7180_Baro 0x2A // start of two-byte MS5637 pressure data, 16-bit signed interger
#define EM7180_BaroTIME 0x2C // start of two-byte MS5637 pressure timestamp, 16-bit unsigned
#define EM7180_Temp 0x2E // start of two-byte MS5637 temperature data, 16-bit signed interger
#define EM7180_TempTIME 0x30 // start of two-byte MS5637 temperature timestamp, 16-bit unsigned
#define EM7180_QRateDivisor 0x32 // uint8_t
#define EM7180_EnableEvents 0x33
#define EM7180_HostControl 0x34
#define EM7180_EventStatus 0x35
#define EM7180_SensorStatus 0x36
#define EM7180_SentralStatus 0x37
#define EM7180_AlgorithmStatus 0x38
#define EM7180_FeatureFlags 0x39
#define EM7180_ParamAcknowledge 0x3A
#define EM7180_SavedParamByte0 0x3B
#define EM7180_SavedParamByte1 0x3C
#define EM7180_SavedParamByte2 0x3D
#define EM7180_SavedParamByte3 0x3E
#define EM7180_ActualMagRate 0x45
#define EM7180_ActualAccelRate 0x46
#define EM7180_ActualGyroRate 0x47
#define EM7180_ActualBaroRate 0x48
#define EM7180_ActualTempRate 0x49
#define EM7180_ErrorRegister 0x50
#define EM7180_AlgorithmControl 0x54
#define EM7180_MagRate 0x55
#define EM7180_AccelRate 0x56
#define EM7180_GyroRate 0x57
#define EM7180_BaroRate 0x58
#define EM7180_TempRate 0x59
#define EM7180_LoadParamByte0 0x60
#define EM7180_LoadParamByte1 0x61
#define EM7180_LoadParamByte2 0x62
#define EM7180_LoadParamByte3 0x63
#define EM7180_ParamRequest 0x64
#define EM7180_ROMVersion1 0x70
#define EM7180_ROMVersion2 0x71
#define EM7180_RAMVersion1 0x72
#define EM7180_RAMVersion2 0x73
#define EM7180_ProductID 0x90
#define EM7180_RevisionID 0x91
#define EM7180_RunStatus 0x92
#define EM7180_UploadAddress 0x94 // uint16_t registers 0x94 (MSB)-5(LSB)
#define EM7180_UploadData 0x96
#define EM7180_CRCHost 0x97 // uint32_t from registers 0x97-9A
#define EM7180_ResetRequest 0x9B
#define EM7180_PassThruStatus 0x9E
#define EM7180_PassThruControl 0xA0
#define EM7180_ACC_LPF_BW 0x5B //Register GP36
#define EM7180_GYRO_LPF_BW 0x5C //Register GP37
#define EM7180_BARO_LPF_BW 0x5D //Register GP38
#define EM7180_ADDRESS 0x28 // Address of the EM7180 SENtral sensor hub
#define M24512DFM_DATA_ADDRESS 0x50 // Address of the 500 page M24512DFM EEPROM data buffer, 1024 bits (128 8-bit bytes) per page
#define M24512DFM_IDPAGE_ADDRESS 0x58 // Address of the single M24512DFM lockable EEPROM ID page
#define MPU9250_ADDRESS 0x68 // Device address when ADO = 0
#define AK8963_ADDRESS 0x0C // Address of magnetometer
#define MS5637_ADDRESS 0x76 // Address of altimeter
#define AFS_2G 0
#define AFS_4G 1
#define AFS_8G 2
#define AFS_16G 3
#define GFS_250DPS 0
#define GFS_500DPS 1
#define GFS_1000DPS 2
#define GFS_2000DPS 3
#define MFS_14BITS 0 // 0.6 mG per LSB
#define MFS_16BITS 1 // 0.15 mG per LSB
#define ADC_256 0x00 // define pressure and temperature conversion rates
#define ADC_512 0x02
#define ADC_1024 0x04
#define ADC_2048 0x06
#define ADC_4096 0x08
#define ADC_8192 0x0A
#define ADC_D1 0x40
#define ADC_D2 0x50
class USFS
{
public:
USFS(uint8_t intPin, bool passThru);
float getAres(uint8_t Ascale);
float getGres(uint8_t Gscale);
float getMres(uint8_t Mscale);
float uint32_reg_to_float (uint8_t *buf);
float int32_reg_to_float (uint8_t *buf);
void float_to_bytes (float param_val, uint8_t *buf);
void EM7180_set_gyro_FS (uint16_t gyro_fs);
void EM7180_set_mag_acc_FS (uint16_t mag_fs, uint16_t acc_fs);
void EM7180_set_integer_param (uint8_t param, uint32_t param_val);
void EM7180_set_float_param (uint8_t param, float param_val);
void readSENtralQuatData(float * destination);
void readSENtralAccelData(int16_t * destination);
void readSENtralGyroData(int16_t * destination);
void readSENtralMagData(int16_t * destination);
void readAccelData(int16_t * destination);
void readGyroData(int16_t * destination);
void readMagData(int16_t * destination);
int16_t readTempData();
void initEM7180(uint8_t accBW, uint8_t gyroBW, uint16_t accFS, uint16_t gyroFS, uint16_t magFS, uint8_t QRtDiv, uint8_t magRt, uint8_t accRt, uint8_t gyroRt, uint8_t baroRt);
void initAK8963(uint8_t Mscale, uint8_t Mmode, float * destination);
void initMPU9250(uint8_t Ascale, uint8_t Gscale);
void accelgyrocalMPU9250(float * dest1, float * dest2);
void magcalMPU9250(float * dest1, float * dest2);
void MPU9250SelfTest(float * destination);
int16_t readSENtralBaroData();
int16_t readSENtralTempData();
void SENtralPassThroughMode();
void M24512DFMwriteByte(uint8_t device_address, uint8_t data_address1, uint8_t data_address2, uint8_t data);
void M24512DFMwriteBytes(uint8_t device_address, uint8_t data_address1, uint8_t data_address2, uint8_t count, uint8_t * dest);
uint8_t M24512DFMreadByte(uint8_t device_address, uint8_t data_address1, uint8_t data_address2);
void M24512DFMreadBytes(uint8_t device_address, uint8_t data_address1, uint8_t data_address2, uint8_t count, uint8_t * dest);
void MS5637Reset();
void MS5637PromRead(uint16_t * destination);
uint32_t MS5637Read(uint8_t CMD, uint8_t OSR);
unsigned char MS5637checkCRC(uint16_t * n_prom);
void MadgwickQuaternionUpdate(float ax, float ay, float az, float gx, float gy, float gz, float mx, float my, float mz);
void MahonyQuaternionUpdate(float ax, float ay, float az, float gx, float gy, float gz, float mx, float my, float mz);
void getChipID();
void loadfwfromEEPROM();
uint8_t checkEM7180Status();
uint8_t checkEM7180Errors();
void I2Cscan();
void writeByte(uint8_t address, uint8_t subAddress, uint8_t data);
uint8_t readByte(uint8_t address, uint8_t subAddress);
void readBytes(uint8_t address, uint8_t subAddress, uint8_t count, uint8_t * dest);
private:
uint8_t _intPin;
bool _passThru;
float _aRes;
float _gRes;
float _mRes;
uint8_t _Mmode;
float _fuseROMx;
float _fuseROMy;
float _fuseROMz;
float _q[4];
float _beta;
float _deltat;
float _Kp;
float _Ki;
};
#endif
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