Skip to content

Instantly share code, notes, and snippets.

@ersatzavian
Created January 21, 2015 01:08
Show Gist options
  • Save ersatzavian/23c491aa90963ff86eed to your computer and use it in GitHub Desktop.
Save ersatzavian/23c491aa90963ff86eed to your computer and use it in GitHub Desktop.
Driver code for LSM9DS0-based 9-degrees-of-freedom imp tail
/* 9 Degrees of Freedom Sensor Tail Firmware
* Uses LSM9DS0 IMU from ST
* http://www.adafruit.com/datasheets/LSM9DS0.pdf
*/
const XM_ADDR = 0x3C; // 8-bit I2C Student Address for Accel / Magnetometer
const G_ADDR = 0xD4; // 8-bit I2C Student Address for Angular Rate Sensor
const READING_INTERVAL = 1; // seconds between readings
/* CLASS AND GLOBAL FUNCTION DEFINITIONS ------------------------------------ */
// Inertial Measurement Unit LSM9DS0
// http://www.adafruit.com/datasheets/LSM9DS0.pdf
class LSM9DS0 {
static WHO_AM_I_G = 0x0F;
static CTRL_REG1_G = 0x20;
static CTRL_REG2_G = 0x21;
static CTRL_REG3_G = 0x22;
static CTRL_REG4_G = 0x23;
static CTRL_REG5_G = 0x24;
static REF_DATACAP_G = 0x25;
static STATUS_REG_G = 0x27;
static OUT_X_L_G = 0x28;
static OUT_X_H_G = 0x29;
static OUT_Y_L_G = 0x2A;
static OUT_Y_H_G = 0x2B;
static OUT_Z_L_G = 0x2C;
static OUT_Z_H_G = 0x2D;
static FIFO_CTRL_REG_G = 0x2E;
static FIFO_SRC_REG_G = 0x2F;
static INT1_CFG_G = 0x30;
static INT1_SRC_G = 0x31;
static INT1_THS_XH_G = 0x32;
static INT1_THS_XL_G = 0x33;
static INT1_THS_YH_G = 0x34;
static INT1_THS_YL_G = 0x35;
static INT1_THS_ZH_G = 0x36;
static INT1_THS_ZL_G = 0x37;
static INT1_DURATION_G = 0x38;
static OUT_TEMP_L_XM = 0x05;
static OUT_TEMP_H_XM = 0x06;
static STATUS_REG_M = 0x07;
static OUT_X_L_M = 0x08;
static OUT_X_H_M = 0x09;
static OUT_Y_L_M = 0x0A;
static OUT_Y_H_M = 0x0B;
static OUT_Z_L_M = 0x0C;
static OUT_Z_H_M = 0x0D;
static WHO_AM_I_XM = 0x0F;
static INT_CTRL_REG_M = 0x12;
static INT_SRC_REG_M = 0x13;
static INT_THS_L_M = 0x14;
static INT_THS_H_M = 0x15;
static OFFSET_X_L_M = 0x16;
static OFFSET_X_H_M = 0x17;
static OFFSET_Y_L_M = 0x18;
static OFFSET_Y_H_M = 0x19;
static OFFSET_Z_L_M = 0x1A;
static OFFSET_Z_H_M = 0x1B;
static REFERENCE_X = 0x1C;
static REFERENCE_Y = 0x1D;
static REFERENCE_Z = 0x1E;
static CTRL_REG0_XM = 0x1F;
static CTRL_REG1_XM = 0x20;
static CTRL_REG2_XM = 0x21;
static CTRL_REG3_XM = 0x22;
static CTRL_REG4_XM = 0x23;
static CTRL_REG5_XM = 0x24;
static CTRL_REG6_XM = 0x25;
static CTRL_REG7_XM = 0x26;
static STATUS_REG_A = 0x27;
static OUT_X_L_A = 0x28;
static OUT_X_H_A = 0x29;
static OUT_Y_L_A = 0x2A;
static OUT_Y_H_A = 0x2B;
static OUT_Z_L_A = 0x2C;
static OUT_Z_H_A = 0x2D;
static FIFO_CTRL_REG = 0x2E;
static FIFO_SRC_REG = 0x2F;
static INT_GEN_1_REG = 0x30;
static INT_GEN_1_SRC = 0x31;
static INT_GEN_1_THS = 0x32;
static INT_GEN_1_DURATION = 0x33;
static INT_GEN_2_REG = 0x34;
static INT_GEN_2_SRC = 0x35;
static INT_GEN_2_THS = 0x36;
static INT_GEN_2_DURATION = 0x37;
static CLICK_CFG = 0x38;
static CLICK_SRC = 0x39;
static CLICK_THS = 0x3A;
static TIME_LIMIT = 0x3B;
static TIME_LATENCY = 0x3C;
static TIME_WINDOW = 0x3D;
static Act_THS = 0x3E;
static Act_DUR = 0x3F;
_i2c = null;
_xm_addr = null;
_g_addr = null;
_temp_enabled = null;
// -------------------------------------------------------------------------
constructor(i2c, xm_addr, g_addr) {
_i2c = i2c;
_xm_addr = xm_addr;
_g_addr = g_addr;
_temp_enabled = false;
}
// -------------------------------------------------------------------------
function _twosComp(value, mask) {
value = ~(value & mask) + 1;
return value & mask;
}
// -------------------------------------------------------------------------
function _setRegBit(addr, reg, bit, state) {
local val = _i2c.read(addr, format("%c",reg), 1)[0];
if (state == 0) {
val = val & ~(0x01 << bit);
} else {
val = val | (0x01 << bit);
}
_i2c.write(addr, format("%c%c", reg, val));
}
// -------------------------------------------------------------------------
// Return Gyro Device ID (0xD4)
function getDeviceId_G() {
return _i2c.read(_g_addr, format("%c",WHO_AM_I_G), 1)[0];
}
// -------------------------------------------------------------------------
// set power state of the gyro device
// note that if individual axes were previously disabled, they still will be
function setPowerState_G(state) {
_setRegBit(_g_addr, CTRL_REG1_G, 3, state);
}
// -------------------------------------------------------------------------
function setPowerState_GZ(state) {
_setRegBit(_g_addr, CTRL_REG1_G, 2, state);
}
// -------------------------------------------------------------------------
function setPowerState_GY(state) {
_setRegBit(_g_addr, CTRL_REG1_G, 1, state);
}
// -------------------------------------------------------------------------
function setPowerState_GX(state) {
_setRegBit(_g_addr, CTRL_REG1_G, 0, state);
}
// -------------------------------------------------------------------------
// set high to enable interrupt generation from the gyro
function setIntEnable_G(state) {
_setRegBit(_g_addr, CTRL_REG3_G, 7, state);
}
// -------------------------------------------------------------------------
// set high to enable active-low interrupt on gyro interrupt
// set low to enable active-high
function setIntActivelow_G(state) {
_setRegBit(_g_addr, CTRL_REG3_G, 5, state);
}
// -------------------------------------------------------------------------
// set high to enable open-drain output on gyro interrupt
// set low to enable push-pull
function setIntOpendrain_G(state) {
_setRegBit(_g_addr, CTRL_REG3_G, 4, state);
}
// -------------------------------------------------------------------------
// Generate interrupt on data-ready
function setIntDrdy_G(state) {
_setRegBit(_g_addr, CTRL_REG3_G, 3, state);
}
// -------------------------------------------------------------------------
// Generate interrupt on FIFO watermark
function setIntFifoWatermark_G(state) {
_setRegBit(_g_addr, CTRL_REG3_G, 2, state);
}
// -------------------------------------------------------------------------
// Generate interrupt on FIFO overrun
function setIntFifoOverrun_G(state) {
_setRegBit(_g_addr, CTRL_REG3_G, 1, state);
}
// -------------------------------------------------------------------------
// Generate interrupt on FIFO empty
function setIntFifoEmpty_G(state) {
_setRegBit(_g_addr, CTRL_REG3_G, 0, state);
}
// -------------------------------------------------------------------------
// enable interrupt latch for gyro interrupts
function setIntLatchEn_G(state) {
_setRegBit(_g_addr, INT1_CFG_G, 6, state);
}
// -------------------------------------------------------------------------
// enable interrupt generation on Z high event
function setIntZhighEn_G(state) {
_setRegBit(_g_addr, INT1_CFG_G, 5, state);
}
// -------------------------------------------------------------------------
// enable interrupt generation on Z low event
function setIntZlowEn_G(state) {
_setRegBit(_g_addr, INT1_CFG_G, 4, state);
}
// -------------------------------------------------------------------------
// enable interrupt generation on Y high event
function setIntYhighEn_G(state) {
_setRegBit(_g_addr, INT1_CFG_G, 3, state);
}
// -------------------------------------------------------------------------
// enable interrupt generation on Y low event
function setIntYlowEn_G(state) {
_setRegBit(_g_addr, INT1_CFG_G, 2, state);
}
// -------------------------------------------------------------------------
// enable interrupt generation on X high event
function setIntXhighEn_G(state) {
_setRegBit(_g_addr, INT1_CFG_G, 1, state);
}
// -------------------------------------------------------------------------
// enable interrupt generation on X low event
function setIntXlowEn_G(state) {
_setRegBit(_g_addr, INT1_CFG_G, 0, state);
}
// -------------------------------------------------------------------------
// set the gyro threshold values for interrupt
function getIntThs_G(x_ths, y_ths, z_ths) {
_i2c.write(_g_addr, format("%c%c", INT1_THS_XH_G, (x_ths & 0xff00) >> 8));
_i2c.write(_g_addr, format("%c%c", INT1_THS_XL_G, (x_ths & 0xff)));
_i2c.write(_g_addr, format("%c%c", INT1_THS_YH_G, (y_ths & 0xff00) >> 8));
_i2c.write(_g_addr, format("%c%c", INT1_THS_YL_G, (y_ths & 0xff)));
_i2c.write(_g_addr, format("%c%c", INT1_THS_ZH_G, (z_ths & 0xff00) >> 8));
_i2c.write(_g_addr, format("%c%c", INT1_THS_ZL_G, (z_ths & 0xff)));
}
// -------------------------------------------------------------------------
// set number of over-threshold samples to count before throwing interrupt
function setIntDuration_G(nsamples) {
_i2c.write(_g_addr, format("%c%c", INT1_DURATION_G, nsamples & 0xff));
}
// -------------------------------------------------------------------------
// read the interrupt source register to determine what caused an interrupt
function getIntSrc_G(state) {
return _i2c.read(_g_addr, format("%c",INT1_SRC_G), 1)[0];
}
// -------------------------------------------------------------------------
// Enable/disable FIFO for gyro
function setFifoEn_G(state) {
_setRegBit(_g_addr, CTRL_REG5_G, 6, state);
}
// -------------------------------------------------------------------------
// Enable/disable Gyro High-Pass Filter
function setHpfEn_G(state) {
_setRegBit(_g_addr, CTRL_REG5_G, 4, state);
}
// -------------------------------------------------------------------------
// Returns Accel/Magnetometer Device ID (0x49)
function getDeviceId_XM() {
return _i2c.read(_xm_addr, format("%c",WHO_AM_I_XM), 1)[0];
}
// -------------------------------------------------------------------------
// read the magnetometer's status register
function getStatus_M() {
return _i2c.read(_xm_addr, format("%c",STATUS_REG_M), 1)[0];
}
// -------------------------------------------------------------------------
// Put magnetometer into continuous-conversion mode
// IMU comes up with magnetometer powered down
function setModeCont_M() {
local val = _i2c.read(_xm_addr, format("%c",CTRL_REG7_XM), 1)[0] & 0xFC;
// bits 1:0 determine mode
// 0b00 -> continuous conversion mode
_i2c.write(_xm_addr, format("%c%c",CTRL_REG7_XM, val));
}
// -------------------------------------------------------------------------
// Put magnetometer into single-conversion mode
function setModeSingle_M() {
local val = _i2c.read(_xm_addr, format("%c",CTRL_REG7_XM), 1)[0] & 0xFC;
// 0b01 -> single conversion mode
val = val | 0x01;
_i2c.write(_xm_addr, format("%c%c",CTRL_REG7_XM, val));
}
// -------------------------------------------------------------------------
// Put magnetometer into power-down mode
function setModePowerdown_M() {
local val = _i2c.read(_xm_addr, format("%c",CTRL_REG7_XM), 1)[0] & 0xFC;
// 0b10 or 0b11 -> power-down mode
val = val | 0x20;
_i2c.write(_xm_addr, format("%c%c",CTRL_REG7_XM, val));
}
// -------------------------------------------------------------------------
// Enable interrupt generation on x axis for magnetic data
function setIntEn_MX(state) {
_setRegBit(_xm_addr, INT_CTRL_CTRL_REG_M, 7, state);
}
// -------------------------------------------------------------------------
// Enable interrupt generation on y axis for magnetic data
function setIntEn_MY(state) {
_setRegBit(_xm_addr, INT_CTRL_CTRL_REG_M, 6, state);
}
// -------------------------------------------------------------------------
// Enable interrupt generation on z axis for magnetic data
function setIntEn_MZ(state) {
_setRegBit(_xm_addr, INT_CTRL_CTRL_REG_M, 5, state);
}
// -------------------------------------------------------------------------
// set high to enable interrupt generation from the magnetometer
function setIntEn_M(state) {
_setRegBit(_xm_addr, INT_CTRL_CTRL_REG_M, 0, state);
}
// -------------------------------------------------------------------------
// set high to enable active-low interrupt for accel/mag
// set low to enable active-high
function setIntActivelow_XM(state) {
_setRegBit(_xm_addr, INT_CTRL_CTRL_REG_M, 3, state);
}
// -------------------------------------------------------------------------
// set high to enable open-drain output for accel/mag
// set low to enable push-pull
function setIntOpendrain_XM(state) {
_setRegBit(_xm_addr, INT_CTRL_CTRL_REG_M, 4, state);
}
// -------------------------------------------------------------------------
// enable/disable interrupt latching for accel/magnetometer
// if set, clear interrupt by reading INT_GEN1_SRC, INT_GEN2_SRC, AND INT_SRC_REG_M
function setIntLatch_XM(state) {
_setRegBit(_xm_addr, INT_CTRL_CTRL_REG_M, 2, state);
}
// -------------------------------------------------------------------------
// read the interrupt source register to determine what caused an interrupt
function getIntSrc_M() {
return _i2c.read(_xm_addr, format("%c",INT_SRC_REG_M), 1)[0];
}
// -------------------------------------------------------------------------
// set the absolute value of the magnetometer interrupt threshold for all axes
function setIntThs_M(val) {
_i2c.write(_xm_addr, format("%c%c",INT_THS_H_M, (val & 0xff00) << 8));
_i2c.write(_xm_addr, format("%c%c",INT_THS_L_M, (val & 0xff)));
}
// -------------------------------------------------------------------------
function setFifoEn_XM(state) {
_setRegBit(_xm_addr, CTRL_REG0_XM, 6, state);
}
// -------------------------------------------------------------------------
function setFifoWatermarkEn_XM(state) {
_setRegBit(_xm_addr, CTRL_REG0_XM, 5, state);
}
// -------------------------------------------------------------------------
// Enable/disable high-pass filter for click detection interrupt
function setHpfClick_XM(state) {
_setRegBit(_xm_addr, CTRL_REG0_XM, 2, state);
}
// -------------------------------------------------------------------------
// Enable/disable high-pass filter for interrupt generator 1
function setHpfInt1_XM(state) {
_setRegBit(_xm_addr, CTRL_REG0_XM, 1, state);
}
// -------------------------------------------------------------------------
function setHpfInt2_XM(state) {
_setRegBit(_xm_addr, CTRL_REG0_XM, 0, state);
}
// -------------------------------------------------------------------------
// Set Accelerometer Data Rate in Hz
// IMU comes up with accelerometer disabled; rate must be set to enable
function setDatarate_A(rate) {
local val = _i2c.read(_xm_addr, format("%c",CTRL_REG1_XM), 1)[0] & 0x0F;
if (rate == 0) {
// 0b0000 -> power-down mode
// we've already ANDed-out the top 4 bits; just write back
} else if (rate <= 3.125) {
val = val | 0x10;
} else if (rate <= 6.25) {
val = val | 0x20;
} else if (rate <= 12.5) {
val = val | 0x30;
} else if (rate <= 25) {
val = val | 0x40;
} else if (rate <= 50) {
val = val | 0x50;
} else if (rate <= 100) {
val = val | 0x60;
} else if (rate <= 200) {
val = val | 0x70;
} else if (rate <= 400) {
val = val | 0x80;
} else if (rate <= 800) {
val = val | 0x90;
} else if (rate <= 1600) {
val = val | 0xA0;
}
_i2c.write(_xm_addr, format("%c%c",CTRL_REG1_XM, val));
}
// -------------------------------------------------------------------------
// Set Magnetometer Data Rate in Hz
// IMU comes up with magnetometer data rate set to 3.125 Hz
function setDatarate_M(rate) {
local val = _i2c.read(_xm_addr, format("%c",CTRL_REG5_XM), 1)[0] & 0xE3;
if (rate <= 3.125) {
// rate already set
} else if (rate <= 6.25) {
val = val | 0x04;
} else if (rate <= 12.5) {
val = val | 0x08;
} else if (rate <= 25) {
val = val | 0x0C;
} else if (rate <= 50) {
val = val | 0x10;
} else {
// rate = 100 Hz
val = val | 0x14;
}
_i2c.write(_xm_addr, format("%c%c",CTRL_REG5_XM, val));
}
// -------------------------------------------------------------------------
// Enable Interrupt Generation on INT1_XM pin on "tap" event
function setTapIntEn_P1(state) {
_setRegBit(_xm_addr, CTRL_REG3_XM, 6, state);
}
// -------------------------------------------------------------------------
// Enable Inertial Interrupt Generator 1 on INT1_XM pin
function setInertInt1En_P1(state) {
_setRegBit(_xm_addr, CTRL_REG3_XM, 5, state);
}
// -------------------------------------------------------------------------
// Enable Inertial Interrupt Generator 2 on INT1_XM pin
function setInertInt1En_P2(state) {
_setRegBit(_xm_addr, CTRL_REG3_XM, 4, state);
}
// -------------------------------------------------------------------------
// Enable Magnetic Interrupt on INT1_XM pin
function setMagIntEn_P1(state) {
_setRegBit(_xm_addr, CTRL_REG3_XM, 3, state);
}
// -------------------------------------------------------------------------
// Enable Accel Data Ready Interrupt INT1_XM pin
function setAccelDrdyIntEn_P1(state) {
_setRegBit(_xm_addr, CTRL_REG3_XM, 2, state);
}
// -------------------------------------------------------------------------
// Enable Magnetometer Data Ready Interrupt INT1_XM pin
function setMagDrdyIntEn_P1(state) {
_setRegBit(_xm_addr, CTRL_REG3_XM, 1, state);
}
// -------------------------------------------------------------------------
// Enable FIFO Empty Interrupt INT1_XM pin
function setAccelDrdyIntEn_P1(state) {
_setRegBit(_xm_addr, CTRL_REG3_XM, 0, state);
}
// -------------------------------------------------------------------------
// Enable Interrupt Generation on INT2_XM pin on "tap" event
function setTapIntEn_P2(state) {
_setRegBit(_xm_addr, CTRL_REG4_XM, 6, state);
}
// -------------------------------------------------------------------------
// Enable Inertial Interrupt Generator 1 on INT2_XM pin
function setInertInt1En_P2(state) {
_setRegBit(_xm_addr, CTRL_REG4_XM, 5, state);
}
// -------------------------------------------------------------------------
// Enable Inertial Interrupt Generator 2 on INT2_XM pin
function setInertInt2En_P2(state) {
_setRegBit(_xm_addr, CTRL_REG4_XM, 4, state);
}
// -------------------------------------------------------------------------
// Enable Magnetic Interrupt on INT2_XM pin
function setMagIntEn_P2(state) {
_setRegBit(_xm_addr, CTRL_REG4_XM, 3, state);
}
// -------------------------------------------------------------------------
// Enable Accel Data Ready Interrupt INT2_XM pin
function setAccelDrdyIntEn_P2(state) {
_setRegBit(_xm_addr, CTRL_REG4_XM, 2, state);
}
// -------------------------------------------------------------------------
// Enable Magnetometer Data Ready Interrupt INT2_XM pin
function set_mag_drdy_int_en_p2(state) {
_setRegBit(_xm_addr, CTRL_REG4_XM, 1, state);
}
// -------------------------------------------------------------------------
// Enable FIFO Empty Interrupt INT2_XM pin
function setAccelDrdyIntEn_P2(state) {
_setRegBit(_xm_addr, CTRL_REG4_XM, 0, state);
}
// -------------------------------------------------------------------------
// Enable / Disable Interrupt Latching on XM_INT1 Pin
function setInt1LatchEn_XM(state) {
_setRegBit(_xm_addr, CTRL_REG5_XM, 1, state);
}
// -------------------------------------------------------------------------
// Enable / Disable Interrupt Latching onh XM_INT1 Pin
function setInt2LatchEn_XM(state) {
_setRegBit(_xm_addr, CTRL_REG5_XM, 0, state);
}
// -------------------------------------------------------------------------
// Enable temperature sensor
function setTempEn(state) {
_setRegBit(_xm_addr, CTRL_REG5_XM, 7, state);
if (state == 0) {
_temp_enabled = false;
} else {
_temp_enabled = true;
}
}
// -------------------------------------------------------------------------
// read the acceleromter's status register
function getStatus_A() {
return _i2c.read(_xm_addr, format("%c",STATUS_REG_A), 1)[0];
}
// -------------------------------------------------------------------------
function getInt1Src_XM(val) {
return _i2c.read(_xm_addr, format("%c",INT_GEN_1_SRC), 1)[0];
}
// -------------------------------------------------------------------------
function getInt2Src_XM(val) {
return _i2c.read(_xm_addr, format("%c",INT_GEN_2_SRC), 1)[0];
}
// -------------------------------------------------------------------------
// enable interrupt 1 generation on Z high event
function setInt1ZhighEn_A(state) {
_setRegBit(_xm_addr, INT_GEN_1_REG, 5, state);
}
// -------------------------------------------------------------------------
// enable interrupt 1 generation on Z low event
function setInt1ZlowEn_A(state) {
_setRegBit(_xm_addr, INT_GEN_1_REG, 4, state);
}
// -------------------------------------------------------------------------
// enable interrupt 1 generation on Y high event
function setInt1YhighEn_A(state) {
_setRegBit(_xm_addr, INT_GEN_1_REG, 3, state);
}
// -------------------------------------------------------------------------
// enable interrupt 1 generation on Y low event
function setInt1YlowEn_A(state) {
_setRegBit(_xm_addr, INT_GEN_1_REG, 2, state);
}
// -------------------------------------------------------------------------
// enable interrupt 1 generation on X high event
function setInt1XhighEn_A(state) {
_setRegBit(_xm_addr, INT_GEN_1_REG, 1, state);
}
// -------------------------------------------------------------------------
// enable interrupt 1 generation on X low event
function setInt1XlowEn_A(state) {
_setRegBit(_xm_addr, INT_GEN_1_REG, 0, state);
}
// -------------------------------------------------------------------------
// set the accelerometer threshold value interrupt 1
function setInt1Ths_A(ths) {
_i2c.write(_g_addr, format("%c%c", INT_GEN_1_THS, (ths & 0xff)));
}
// -------------------------------------------------------------------------
// set the event duration over threshold before throwing interrupt
// duration steps and max values depend on selected ODR
function setInt1Duration_A(duration) {
_i2c.write(_g_addr, format("%c%c", INT_GEN_1_DURATION, duration & 0x7f));
}
// -------------------------------------------------------------------------
// enable interrupt 2 generation on Z high event
function setInt2ZhighEn_A(state) {
_setRegBit(_xm_addr, INT_GEN_2_REG, 5, state);
}
// -------------------------------------------------------------------------
// enable interrupt 2 generation on Z low event
function setInt2ZlowEn_A(state) {
_setRegBit(_xm_addr, INT_GEN_2_REG, 4, state);
}
// -------------------------------------------------------------------------
// enable interrupt 2 generation on Y high event
function setInt2YhighEn_A(state) {
_setRegBit(_xm_addr, INT_GEN_2_REG, 3, state);
}
// -------------------------------------------------------------------------
// enable interrupt 2 generation on Y low event
function setInt2YlowEn_A(state) {
_setRegBit(_xm_addr, INT_GEN_2_REG, 2, state);
}
// -------------------------------------------------------------------------
// enable interrupt 2 generation on X high event
function setInt2XhighEn_A(state) {
_setRegBit(_xm_addr, INT_GEN_2_REG, 1, state);
}
// -------------------------------------------------------------------------
// enable interrupt 2 generation on X low event
function setInt2XlowEn_A(state) {
_setRegBit(_xm_addr, INT_GEN_2_REG, 0, state);
}
// -------------------------------------------------------------------------
// set the accelerometer threshold value interrupt 2
function setInt2Ths_A(ths) {
_i2c.write(_g_addr, format("%c%c", INT_GEN_2_THS, (ths & 0xff)));
}
// -------------------------------------------------------------------------
// set the event duration over threshold before throwing interrupt
// duration steps and max values depend on selected ODR
function setInt2Duration_A(duration) {
_i2c.write(_g_addr, format("%c%c", INT_GEN_2_DURATION, duration & 0x7f));
}
// -------------------------------------------------------------------------
// enable / disable double-click detection on z-axis
function setDblclickIntEn_Z(state) {
_setRegBit(_xm_addr, CLICK_CFG, 5, state);
}
// -------------------------------------------------------------------------
// enable / disable single-click detection on z-axis
function setSnglclickIntEn_Z(state) {
_setRegBit(_xm_addr, CLICK_CFG, 4, state);
}
// -------------------------------------------------------------------------
// enable / disable double-click detection on y-axis
function setDblclickIntEn_Y(state) {
_setRegBit(_xm_addr, CLICK_CFG, 3, state);
}
// -------------------------------------------------------------------------
// enable / disable single-click detection on y-axis
function setSnglclickIntEn_Y(state) {
_setRegBit(_xm_addr, CLICK_CFG, 2, state);
}
// -------------------------------------------------------------------------
// enable / disable double-click detection on x-axis
function setDblclickIntEn_X(state) {
_setRegBit(_xm_addr, CLICK_CFG, 1, state);
}
// -------------------------------------------------------------------------
// enable / disable single-click detection on x-axis
function setSnglclickIntEn_X(state) {
_setRegBit(_xm_addr, CLICK_CFG, 0, state);
}
// -------------------------------------------------------------------------
function clickIntActive() {
return (0x40 & _i2c.read(_xm_addr, format("%c", CLICK_SRC), 1)[0]);
}
// -------------------------------------------------------------------------
function dblclickDet() {
return (0x20 & _i2c.read(_xm_addr, format("%c", CLICK_SRC), 1)[0]);
}
// -------------------------------------------------------------------------
function snglclickDet() {
return (0x10 & _i2c.read(_xm_addr, format("%c", CLICK_SRC), 1)[0]);
}
// -------------------------------------------------------------------------
function clickNegDir() {
return (0x08 & _i2c.read(_xm_addr, format("%c", CLICK_SRC), 1)[0]);
}
// -------------------------------------------------------------------------
function zclickDet() {
return (0x04 & _i2c.read(_xm_addr, format("%c", CLICK_SRC), 1)[0]);
}
// -------------------------------------------------------------------------
function yclickDet() {
return (0x02 & _i2c.read(_xm_addr, format("%c", CLICK_SRC), 1)[0]);
}
// -------------------------------------------------------------------------
function xclickDet() {
return (0x01 & _i2c.read(_xm_addr, format("%c", CLICK_SRC), 1)[0]);
}
// -------------------------------------------------------------------------
// set the click detection threshold
function setClickDetThs(ths) {
_i2c.write(_xm_addr, format("%c%c", CLICK_THS, (ths & 0x7f)));
}
// -------------------------------------------------------------------------
// read the internal temperature sensor in the accelerometer / magnetometer
function getTemp() {
if (!_temp_enabled) { setTempEn(1) };
local temp = (_i2c.read(_xm_addr, format("%c", OUT_TEMP_H_XM), 1)[0] << 8) + _i2c.read(_xm_addr, format("%c", OUT_TEMP_L_XM), 1)[0];
temp = temp & 0x0fff; // temp data is 12 bits, 2's comp, right-justified
if (temp & 0x0800) {
return (-1.0) * _twosComp(temp, 0x0fff);
} else {
return temp;
}
}
// -------------------------------------------------------------------------
// Read data from the Gyro
// Returns a table {x: <data>, y: <data>, z: <data>}
function getGyro() {
local x_raw = (_i2c.read(_g_addr, format("%c", OUT_X_H_G), 1)[0] << 8) + _i2c.read(_g_addr, format("%c", OUT_X_L_G), 1)[0];
local y_raw = (_i2c.read(_g_addr, format("%c", OUT_Y_H_G), 1)[0] << 8) + _i2c.read(_g_addr, format("%c", OUT_Y_L_G), 1)[0];
local z_raw = (_i2c.read(_g_addr, format("%c", OUT_Z_H_G), 1)[0] << 8) + _i2c.read(_g_addr, format("%c", OUT_Z_L_G), 1)[0];
local result = {};
if (x_raw & 0x8000) {
result.x <- (-1.0) * _twosComp(x_raw, 0xffff);
} else {
result.x <- x_raw;
}
if (y_raw & 0x8000) {
result.y <- (-1.0) * _twosComp(y_raw, 0xffff);
} else {
result.y <- y_raw;
}
if (z_raw & 0x8000) {
result.z <- (-1.0) * _twosComp(z_raw, 0xffff);
} else {
result.z <- z_raw;
}
return result;
}
// -------------------------------------------------------------------------
// Read data from the Magnetometer
// Returns a table {x: <data>, y: <data>, z: <data>}
function getMag() {
local x_raw = (_i2c.read(_xm_addr, format("%c", OUT_X_H_M), 1)[0] << 8) + _i2c.read(_xm_addr, format("%c", OUT_X_L_M), 1)[0];
local y_raw = (_i2c.read(_xm_addr, format("%c", OUT_Y_H_M), 1)[0] << 8) + _i2c.read(_xm_addr, format("%c", OUT_Y_L_M), 1)[0];
local z_raw = (_i2c.read(_xm_addr, format("%c", OUT_Z_H_M), 1)[0] << 8) + _i2c.read(_xm_addr, format("%c", OUT_Z_L_M), 1)[0];
local result = {};
if (x_raw & 0x8000) {
result.x <- (-1.0) * _twosComp(x_raw, 0xffff);
} else {
result.x <- x_raw;
}
if (y_raw & 0x8000) {
result.y <- (-1.0) * _twosComp(y_raw, 0xffff);
} else {
result.y <- y_raw;
}
if (z_raw & 0x8000) {
result.z <- (-1.0) * _twosComp(z_raw, 0xffff);
} else {
result.z <- z_raw;
}
return result;
}
// -------------------------------------------------------------------------
// Read data from the Accelerometer
// Returns a table {x: <data>, y: <data>, z: <data>}
function getAccel() {
local x_raw = (_i2c.read(_xm_addr, format("%c", OUT_X_H_A), 1)[0] << 8) + _i2c.read(_xm_addr, format("%c", OUT_X_L_A), 1)[0];
local y_raw = (_i2c.read(_xm_addr, format("%c", OUT_Y_H_A), 1)[0] << 8) + _i2c.read(_xm_addr, format("%c", OUT_Y_L_A), 1)[0];
local z_raw = (_i2c.read(_xm_addr, format("%c", OUT_Z_H_A), 1)[0] << 8) + _i2c.read(_xm_addr, format("%c", OUT_Z_L_A), 1)[0];
//server.log(format("%02X, %02X, %02X",x_raw, y_raw, z_raw));
local result = {};
if (x_raw & 0x8000) {
result.x <- (-1.0) * _twosComp(x_raw, 0xffff);
} else {
result.x <- x_raw;
}
if (y_raw & 0x8000) {
result.y <- (-1.0) * _twosComp(y_raw, 0xffff);
} else {
result.y <- y_raw;
}
if (z_raw & 0x8000) {
result.z <- (-1.0) * _twosComp(z_raw, 0xffff);
} else {
result.z <- z_raw;
}
return result;
}
}
// -----------------------------------------------------------------------------
function g_drdy_cb() {
if (g_drdy.read()) {
server.log("Gyro has data ready");
}
}
function g_int_cb() {
if (g_int.read()) {
server.log("Gyro Interrupt");
}
}
function xm_int1_cb() {
if (xm_int1.read()) {
server.log("Interrupt on XM_INT1");
}
}
function xm_int2_cb() {
if (xm_int2.read()) {
server.log("Interrupt on XM_INT2");
}
}
function logloop() {
imp.wakeup(READING_INTERVAL,logloop);
local acc = imu.getAccel();
local mag = imu.getMag();
local gyr = imu.getGyro();
server.log(format("Accel: (%0.2f, %0.2f, %0.2f)", acc.x, acc.y, acc.z));
server.log(format("Mag: (%0.2f, %0.2f, %0.2f)", mag.x, mag.y, mag.z));
server.log(format("Gyro: (%0.2f, %0.2f, %0.2f)", gyr.x, gyr.y, gyr.z));
server.log(format("Temp: %dºC", imu.getTemp()));
}
/* AGENT CALLBACKS ---------------------------------------------------------- */
/* RUNTIME START ------------------------------------------------------------ */
xm_int1 <- hardware.pin1; // accel / magnetometer interrupt 1
xm_int2 <- hardware.pin2; // accel / magnetometer interrupt 2
g_drdy <- hardware.pin5; // angular rate Data Ready
g_int <- hardware.pin7; // angular rate Interrupt
i2c <- hardware.i2c89;
i2c.configure(CLOCK_SPEED_400_KHZ);
g_drdy.configure(DIGITAL_IN, g_drdy_cb);
g_int.configure(DIGITAL_IN, g_int_cb);
xm_int1.configure(DIGITAL_IN, xm_int1_cb);
xm_int2.configure(DIGITAL_IN, xm_int2_cb);
imu <- LSM9DS0(i2c, XM_ADDR, G_ADDR);
server.log("SW: "+imp.getsoftwareversion());
server.log("Memory Free: "+imp.getmemoryfree());
imp.enableblinkup(true);
imp.setpowersave(true);
server.log(format("Gyro ID: %02X", imu.getDeviceId_G()));
server.log(format("XM ID: %02X", imu.getDeviceId_XM()));
// imu.setPowerStateG(0);
// imu.setModePowerdown_M();
// imu.setDatarate_A(0);
imu.setPowerState_G(1);
server.log("Gyro Enabled");
imu.setDatarate_A(3);
server.log("Accel Enabled at 3.125 Hz");
imu.setModeCont_M();
server.log("Magnetometer in Continuous Measurement Mode at 3.125 Hz");
logloop();
imp.onidle( function() {
//server.sleepfor(30);
});
Sign up for free to join this conversation on GitHub. Already have an account? Sign in to comment