212 lines
6.0 KiB
C
212 lines
6.0 KiB
C
/*
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* This file is part of Cleanflight.
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*
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* Cleanflight is free software: you can redistribute it and/or modify
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* it under the terms of the GNU General Public License as published by
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* the Free Software Foundation, either version 3 of the License, or
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* (at your option) any later version.
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*
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* Cleanflight is distributed in the hope that it will be useful,
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* but WITHOUT ANY WARRANTY; without even the implied warranty of
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* MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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* GNU General Public License for more details.
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*
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* You should have received a copy of the GNU General Public License
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* along with Cleanflight. If not, see <http://www.gnu.org/licenses/>.
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*/
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#include <stdbool.h>
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#include <stdint.h>
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#include "platform.h"
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#include "common/axis.h"
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#include "config/parameter_group.h"
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#include "config/parameter_group_ids.h"
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#include "drivers/compass/compass.h"
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#include "drivers/compass/compass_ak8975.h"
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#include "drivers/compass/compass_ak8963.h"
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#include "drivers/compass/compass_fake.h"
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#include "drivers/compass/compass_hmc5883l.h"
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#include "drivers/io.h"
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#include "drivers/light_led.h"
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#include "fc/config.h"
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#include "fc/runtime_config.h"
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#include "sensors/boardalignment.h"
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#include "sensors/compass.h"
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#include "sensors/gyro.h"
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#include "sensors/sensors.h"
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#ifdef USE_HARDWARE_REVISION_DETECTION
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#include "hardware_revision.h"
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#endif
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magDev_t magDev;
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mag_t mag; // mag access functions
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#ifdef MAG_INT_EXTI
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#define COMPASS_INTERRUPT_TAG IO_TAG(MAG_INT_EXTI)
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#else
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#define COMPASS_INTERRUPT_TAG IO_TAG_NONE
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#endif
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PG_REGISTER_WITH_RESET_TEMPLATE(compassConfig_t, compassConfig, PG_COMPASS_CONFIG, 0);
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PG_RESET_TEMPLATE(compassConfig_t, compassConfig,
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.mag_align = ALIGN_DEFAULT,
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// xxx_hardware: 0:default/autodetect, 1: disable
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.mag_hardware = 1,
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.mag_declination = 0,
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.interruptTag = COMPASS_INTERRUPT_TAG
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);
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#ifdef MAG
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static int16_t magADCRaw[XYZ_AXIS_COUNT];
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static uint8_t magInit = 0;
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bool compassDetect(magDev_t *dev, magSensor_e magHardwareToUse)
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{
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magSensor_e magHardware;
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retry:
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dev->magAlign = ALIGN_DEFAULT;
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switch (magHardwareToUse) {
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case MAG_DEFAULT:
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; // fallthrough
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case MAG_HMC5883:
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#ifdef USE_MAG_HMC5883
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if (hmc5883lDetect(dev, compassConfig()->interruptTag)) {
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#ifdef MAG_HMC5883_ALIGN
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dev->magAlign = MAG_HMC5883_ALIGN;
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#endif
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magHardware = MAG_HMC5883;
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break;
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}
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#endif
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; // fallthrough
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case MAG_AK8975:
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#ifdef USE_MAG_AK8975
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if (ak8975Detect(dev)) {
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#ifdef MAG_AK8975_ALIGN
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dev->magAlign = MAG_AK8975_ALIGN;
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#endif
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magHardware = MAG_AK8975;
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break;
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}
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#endif
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; // fallthrough
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case MAG_AK8963:
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#ifdef USE_MAG_AK8963
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if (ak8963Detect(dev)) {
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#ifdef MAG_AK8963_ALIGN
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dev->magAlign = MAG_AK8963_ALIGN;
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#endif
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magHardware = MAG_AK8963;
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break;
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}
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#endif
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; // fallthrough
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case MAG_NONE:
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magHardware = MAG_NONE;
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break;
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}
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if (magHardware == MAG_NONE && magHardwareToUse != MAG_DEFAULT && magHardwareToUse != MAG_NONE) {
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// Nothing was found and we have a forced sensor that isn't present.
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magHardwareToUse = MAG_DEFAULT;
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goto retry;
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}
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if (magHardware == MAG_NONE) {
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return false;
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}
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detectedSensors[SENSOR_INDEX_MAG] = magHardware;
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sensorsSet(SENSOR_MAG);
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return true;
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}
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bool compassInit(void)
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{
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// initialize and calibration. turn on led during mag calibration (calibration routine blinks it)
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// calculate magnetic declination
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mag.magneticDeclination = 0.0f; // TODO investigate if this is actually needed if there is no mag sensor or if the value stored in the config should be used.
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// copy over SPI bus settings for AK8963 compass
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magDev.bus = *gyroSensorBus();
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if (!compassDetect(&magDev, compassConfig()->mag_hardware)) {
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return false;
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}
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const int16_t deg = compassConfig()->mag_declination / 100;
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const int16_t min = compassConfig()->mag_declination % 100;
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mag.magneticDeclination = (deg + ((float)min * (1.0f / 60.0f))) * 10; // heading is in 0.1deg units
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LED1_ON;
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magDev.init();
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LED1_OFF;
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magInit = 1;
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if (compassConfig()->mag_align != ALIGN_DEFAULT) {
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magDev.magAlign = compassConfig()->mag_align;
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}
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return true;
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}
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void compassUpdate(uint32_t currentTime, flightDynamicsTrims_t *magZero)
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{
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static uint32_t tCal = 0;
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static flightDynamicsTrims_t magZeroTempMin;
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static flightDynamicsTrims_t magZeroTempMax;
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magDev.read(magADCRaw);
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for (int axis = 0; axis < XYZ_AXIS_COUNT; axis++) {
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mag.magADC[axis] = magADCRaw[axis];
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}
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alignSensors(mag.magADC, magDev.magAlign);
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if (STATE(CALIBRATE_MAG)) {
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tCal = currentTime;
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for (int axis = 0; axis < 3; axis++) {
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magZero->raw[axis] = 0;
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magZeroTempMin.raw[axis] = mag.magADC[axis];
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magZeroTempMax.raw[axis] = mag.magADC[axis];
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}
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DISABLE_STATE(CALIBRATE_MAG);
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}
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if (magInit) { // we apply offset only once mag calibration is done
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mag.magADC[X] -= magZero->raw[X];
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mag.magADC[Y] -= magZero->raw[Y];
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mag.magADC[Z] -= magZero->raw[Z];
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}
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if (tCal != 0) {
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if ((currentTime - tCal) < 30000000) { // 30s: you have 30s to turn the multi in all directions
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LED0_TOGGLE;
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for (int axis = 0; axis < 3; axis++) {
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if (mag.magADC[axis] < magZeroTempMin.raw[axis])
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magZeroTempMin.raw[axis] = mag.magADC[axis];
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if (mag.magADC[axis] > magZeroTempMax.raw[axis])
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magZeroTempMax.raw[axis] = mag.magADC[axis];
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}
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} else {
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tCal = 0;
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for (int axis = 0; axis < 3; axis++) {
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magZero->raw[axis] = (magZeroTempMin.raw[axis] + magZeroTempMax.raw[axis]) / 2; // Calculate offsets
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}
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saveConfigAndNotify();
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}
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}
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}
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#endif
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