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Port of Adafruit Arduino code
Fork of Adafruit9-DOf by
Source/Adafruit_9DOF.cpp
- Committer:
- ivo_david_michelle
- Date:
- 2016-03-24
- Revision:
- 1:37a7df50e330
- Parent:
- 0:772bf4786416
File content as of revision 1:37a7df50e330:
/*************************************************************************** This is a library for the Adafruit 9DOF Breakout Designed specifically to work with the Adafruit 9DOF Breakout: http://www.adafruit.com/products/1714 These displays use I2C to communicate, 2 pins are required to interface. Adafruit invests time and resources providing this open source code, please support Adafruit andopen-source hardware by purchasing products from Adafruit! Written by Kevin Townsend for Adafruit Industries. BSD license, all text above must be included in any redistribution ***************************************************************************/ #include <math.h> #include "Adafruit_9DOF.h" #define PI (3.14159265F); /*************************************************************************** PRIVATE FUNCTIONS ***************************************************************************/ /*************************************************************************** CONSTRUCTOR ***************************************************************************/ /**************************************************************************/ /*! @brief Instantiates a new Adafruit_9DOF class */ /**************************************************************************/ Adafruit_9DOF::Adafruit_9DOF(void) { } /*************************************************************************** PUBLIC FUNCTIONS ***************************************************************************/ /**************************************************************************/ /*! @brief Setups the HW */ /**************************************************************************/ bool Adafruit_9DOF::begin() { // Enable I2C return true; } /**************************************************************************/ /*! @brief Populates the .pitch/.roll fields in the sensors_vec_t struct with the right angular data (in degree) @param event The sensors_event_t variable containing the data from the accelerometer @param orientation The sensors_vec_t object that will have it's .pitch and .roll fields populated @return Returns true if the operation was successful, false if there was an error @code bool error; sensors_event_t event; sensors_vec_t orientation; ... lsm303accelGetSensorEvent(&event); error = accelGetOrientation(&event, &orientation); @endcode */ /**************************************************************************/ bool Adafruit_9DOF::accelGetOrientation(sensors_event_t *event, sensors_vec_t *orientation) { /* Make sure the input is valid, not null, etc. */ if (event == NULL) return false; if (orientation == NULL) return false; float t_pitch; float t_roll; float signOfZ = event->acceleration.z >= 0 ? 1.0F : -1.0F; /* roll: Rotation around the longitudinal axis (the plane body, 'X axis'). -90<=roll<=90 */ /* roll is positive and increasing when moving downward */ /* */ /* y */ /* roll = atan(-----------------) */ /* sqrt(x^2 + z^2) */ /* where: x, y, z are returned value from accelerometer sensor */ t_roll = event->acceleration.x * event->acceleration.x + event->acceleration.z * event->acceleration.z; orientation->roll = (float)atan2(event->acceleration.y, sqrt(t_roll)) * 180 / PI; /* pitch: Rotation around the lateral axis (the wing span, 'Y axis'). -180<=pitch<=180) */ /* pitch is positive and increasing when moving upwards */ /* */ /* x */ /* roll = atan(-----------------) */ /* sqrt(y^2 + z^2) */ /* where: x, y, z are returned value from accelerometer sensor */ t_pitch = event->acceleration.y * event->acceleration.y + event->acceleration.z * event->acceleration.z; orientation->pitch = (float)atan2(event->acceleration.x, signOfZ * sqrt(t_pitch)) * 180 / PI; return true; } /**************************************************************************/ /*! @brief Utilize the sensor data from an accelerometer to compensate the magnetic sensor measurements when the sensor is tilted (the pitch and roll angles are not equal 0�) @param axis The given axis (SENSOR_AXIS_X/Y/Z) that is parallel to the gravity of the Earth @param mag_event The raw magnetometer data to adjust for tilt @param accel_event The accelerometer event data to use to determine the tilt when compensating the mag_event values @code // Perform tilt compensation with matching accelerometer data sensors_event_t accel_event; error = lsm303accelGetSensorEvent(&accel_event); if (!error) { magTiltCompensation(SENSOR_AXIS_Z, &mag_event, &accel_event); } @endcode */ /**************************************************************************/ bool Adafruit_9DOF::magTiltCompensation(sensors_axis_t axis, sensors_event_t *mag_event, sensors_event_t *accel_event) { /* Make sure the input is valid, not null, etc. */ if (mag_event == NULL) return false; if (accel_event == NULL) return false; float accel_X, accel_Y, accel_Z; float *mag_X, *mag_Y, *mag_Z; switch (axis) { case SENSOR_AXIS_X: /* The X-axis is parallel to the gravity */ accel_X = accel_event->acceleration.y; accel_Y = accel_event->acceleration.z; accel_Z = accel_event->acceleration.x; mag_X = &(mag_event->magnetic.y); mag_Y = &(mag_event->magnetic.z); mag_Z = &(mag_event->magnetic.x); break; case SENSOR_AXIS_Y: /* The Y-axis is parallel to the gravity */ accel_X = accel_event->acceleration.z; accel_Y = accel_event->acceleration.x; accel_Z = accel_event->acceleration.y; mag_X = &(mag_event->magnetic.z); mag_Y = &(mag_event->magnetic.x); mag_Z = &(mag_event->magnetic.y); break; case SENSOR_AXIS_Z: /* The Z-axis is parallel to the gravity */ accel_X = accel_event->acceleration.x; accel_Y = accel_event->acceleration.y; accel_Z = accel_event->acceleration.z; mag_X = &(mag_event->magnetic.x); mag_Y = &(mag_event->magnetic.y); mag_Z = &(mag_event->magnetic.z); break; default: return false; } float t_roll = accel_X * accel_X + accel_Z * accel_Z; float rollRadians = (float)atan2(accel_Y, sqrt(t_roll)); float t_pitch = accel_Y * accel_Y + accel_Z * accel_Z; float pitchRadians = (float)atan2(accel_X, sqrt(t_pitch)); float cosRoll = (float)cos(rollRadians); float sinRoll = (float)sin(rollRadians); float cosPitch = (float)cos(-1*pitchRadians); float sinPitch = (float)sin(-1*pitchRadians); /* The tilt compensation algorithm */ /* Xh = X.cosPitch + Z.sinPitch */ /* Yh = X.sinRoll.sinPitch + Y.cosRoll - Z.sinRoll.cosPitch */ *mag_X = (*mag_X) * cosPitch + (*mag_Z) * sinPitch; *mag_Y = (*mag_X) * sinRoll * sinPitch + (*mag_Y) * cosRoll - (*mag_Z) * sinRoll * cosPitch; return true; } /**************************************************************************/ /*! @brief Populates the .heading fields in the sensors_vec_t struct with the right angular data (0-359�) Heading increases when measuring clockwise @param axis The given axis (SENSOR_AXIS_X/Y/Z) @param event The raw magnetometer sensor data to use when calculating out heading @param orientation The sensors_vec_t object where we will assign an 'orientation.heading' value @code magGetOrientation(SENSOR_AXIS_Z, &mag_event, &orientation); @endcode */ /**************************************************************************/ bool Adafruit_9DOF::magGetOrientation(sensors_axis_t axis, sensors_event_t *event, sensors_vec_t *orientation) { /* Make sure the input is valid, not null, etc. */ if (event == NULL) return false; if (orientation == NULL) return false; switch (axis) { case SENSOR_AXIS_X: /* Sensor rotates around X-axis */ /* "heading" is the angle between the 'Y axis' and magnetic north on the horizontal plane (Oyz) */ /* heading = atan(Mz / My) */ orientation->heading = (float)atan2(event->magnetic.z, event->magnetic.y) * 180 / PI; break; case SENSOR_AXIS_Y: /* Sensor rotates around Y-axis */ /* "heading" is the angle between the 'Z axis' and magnetic north on the horizontal plane (Ozx) */ /* heading = atan(Mx / Mz) */ orientation->heading = (float)atan2(event->magnetic.x, event->magnetic.z) * 180 / PI; break; case SENSOR_AXIS_Z: /* Sensor rotates around Z-axis */ /* "heading" is the angle between the 'X axis' and magnetic north on the horizontal plane (Oxy) */ /* heading = atan(My / Mx) */ orientation->heading = (float)atan2(event->magnetic.y, event->magnetic.x) * 180 / PI; break; default: return false; } /* Normalize to 0-359� */ if (orientation->heading < 0) { orientation->heading = 360 + orientation->heading; } return true; } /**************************************************************************/ /*! @brief Populates the .roll/.pitch/.heading fields in the sensors_vec_t struct with the right angular data (in degree). The starting position is set by placing the object flat and pointing northwards (Z-axis pointing upward and X-axis pointing northwards). The orientation of the object can be modeled as resulting from 3 consecutive rotations in turn: heading (Z-axis), pitch (Y-axis), and roll (X-axis) applied to the starting position. @param accel_event The sensors_event_t variable containing the data from the accelerometer @param mag_event The sensors_event_t variable containing the data from the magnetometer @param orientation The sensors_vec_t object that will have it's .roll, .pitch and .heading fields populated */ /**************************************************************************/ bool Adafruit_9DOF::fusionGetOrientation(sensors_event_t *accel_event, sensors_event_t *mag_event, sensors_vec_t *orientation) { /* Make sure the input is valid, not null, etc. */ if ( accel_event == NULL) return false; if ( mag_event == NULL) return false; if ( orientation == NULL) return false; float const PI_F = 3.14159265F; /* roll: Rotation around the X-axis. -180 <= roll <= 180 */ /* a positive roll angle is defined to be a clockwise rotation about the positive X-axis */ /* */ /* y */ /* roll = atan2(---) */ /* z */ /* */ /* where: y, z are returned value from accelerometer sensor */ orientation->roll = (float)atan2(accel_event->acceleration.y, accel_event->acceleration.z); /* pitch: Rotation around the Y-axis. -180 <= roll <= 180 */ /* a positive pitch angle is defined to be a clockwise rotation about the positive Y-axis */ /* */ /* -x */ /* pitch = atan(-------------------------------) */ /* y * sin(roll) + z * cos(roll) */ /* */ /* where: x, y, z are returned value from accelerometer sensor */ if (accel_event->acceleration.y * sin(orientation->roll) + accel_event->acceleration.z * cos(orientation->roll) == 0) orientation->pitch = accel_event->acceleration.x > 0 ? (PI_F / 2) : (-PI_F / 2); else orientation->pitch = (float)atan(-accel_event->acceleration.x / (accel_event->acceleration.y * sin(orientation->roll) + \ accel_event->acceleration.z * cos(orientation->roll))); /* heading: Rotation around the Z-axis. -180 <= roll <= 180 */ /* a positive heading angle is defined to be a clockwise rotation about the positive Z-axis */ /* */ /* z * sin(roll) - y * cos(roll) */ /* heading = atan2(--------------------------------------------------------------------------) */ /* x * cos(pitch) + y * sin(pitch) * sin(roll) + z * sin(pitch) * cos(roll)) */ /* */ /* where: x, y, z are returned value from magnetometer sensor */ orientation->heading = (float)atan2(mag_event->magnetic.z * sin(orientation->roll) - mag_event->magnetic.y * cos(orientation->roll), \ mag_event->magnetic.x * cos(orientation->pitch) + \ mag_event->magnetic.y * sin(orientation->pitch) * sin(orientation->roll) + \ mag_event->magnetic.z * sin(orientation->pitch) * cos(orientation->roll)); /* Convert angular data to degree */ orientation->roll = orientation->roll * 180 / PI_F; orientation->pitch = orientation->pitch * 180 / PI_F; orientation->heading = orientation->heading * 180 / PI_F; return true; }