Modified to run on Renesas GR Peach board
Dependencies: EthernetInterface HTTP-Server Webpage mbed-rpc mbed-src
Fork of HTTPServer_echoback by
Diff: Adafruit_10DOF/Adafruit_10DOF.cpp
- Revision:
- 16:5d102be2566c
diff -r eae1575da9ca -r 5d102be2566c Adafruit_10DOF/Adafruit_10DOF.cpp --- /dev/null Thu Jan 01 00:00:00 1970 +0000 +++ b/Adafruit_10DOF/Adafruit_10DOF.cpp Wed Oct 07 20:42:51 2015 +0000 @@ -0,0 +1,353 @@ +/*************************************************************************** + This is a library for the Adafruit 10DOF Breakout + + Designed specifically to work with the Adafruit 10DOF Breakout + + 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 "WProgram.h" + + +#include "Adafruit_10DOF.h" +#include "Adafruit_Sensor.h" +#include "I2C.h" + +#define PI (3.14159265F); + +/*************************************************************************** + PRIVATE FUNCTIONS + ***************************************************************************/ + + +/*************************************************************************** + CONSTRUCTOR + ***************************************************************************/ + +/**************************************************************************/ +/*! + @brief Instantiates a new Adafruit_10DOF class +*/ +/**************************************************************************/ +Adafruit_10DOF::Adafruit_10DOF(void) +{ +} + +/*************************************************************************** + PUBLIC FUNCTIONS + ***************************************************************************/ + +/**************************************************************************/ +/*! + @brief Setups the HW +*/ +/**************************************************************************/ +bool Adafruit_10DOF::begin() +{ + // Enable I2C + //Wire.begin(); + + 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_10DOF::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 t_heading; + 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 */ + /* pitch = 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_10DOF::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_10DOF::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_10DOF::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; +}