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598 lines
21 KiB
C
598 lines
21 KiB
C
/**
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******************************************************************************
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* @addtogroup OpenPilotModules OpenPilot Modules
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* @{
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* @addtogroup Sensors
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* @brief Acquires sensor data
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* @{
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*
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* @file sensors.c
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* @author The OpenPilot Team, http://www.openpilot.org Copyright (C) 2015.
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* @brief Module to handle fetch and preprocessing of sensor data
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*
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* @see The GNU Public License (GPL) Version 3
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*
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******************************************************************************/
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/*
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* This program 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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* This program is distributed in the hope that it will be useful, but
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* WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY
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* or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
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* for more details.
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*
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* You should have received a copy of the GNU General Public License along
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* with this program; if not, write to the Free Software Foundation, Inc.,
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* 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA
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*/
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/**
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* Input objects: None, takes sensor data via pios
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* Output objects: @ref GyroSensor @ref AccelSensor @ref MagSensor
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*
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* The module executes in its own thread.
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*
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* UAVObjects are automatically generated by the UAVObjectGenerator from
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* the object definition XML file.
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*
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* Modules have no API, all communication to other modules is done through UAVObjects.
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* However modules may use the API exposed by shared libraries.
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* See the OpenPilot wiki for more details.
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* http://www.openpilot.org/OpenPilot_Application_Architecture
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*
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*/
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#include <openpilot.h>
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#include <pios_sensors.h>
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#include <homelocation.h>
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#include <magsensor.h>
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#include <accelsensor.h>
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#include <gyrosensor.h>
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#include <barosensor.h>
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#include <flightstatus.h>
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#include <attitudesettings.h>
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#include <revocalibration.h>
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#include <accelgyrosettings.h>
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#include <revosettings.h>
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#include <mathmisc.h>
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#include <taskinfo.h>
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#include <pios_math.h>
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#include <pios_constants.h>
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#include <CoordinateConversions.h>
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#include <pios_board_info.h>
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#include <string.h>
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// Private constants
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#define STACK_SIZE_BYTES 1000
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#define TASK_PRIORITY (tskIDLE_PRIORITY + 3)
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#define MAX_SENSORS_PER_INSTANCE 2
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#ifdef PIOS_INCLUDE_WDG
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#define RELOAD_WDG() PIOS_WDG_UpdateFlag(PIOS_WDG_SENSORS)
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#define REGISTER_WDG() PIOS_WDG_RegisterFlag(PIOS_WDG_SENSORS)
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#else
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#define RELOAD_WDG()
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#define REGISTER_WDG()
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#endif
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static const TickType_t sensor_period_ticks = ((uint32_t)1000.0f / PIOS_SENSOR_RATE) / portTICK_RATE_MS;
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// Interval in number of sample to recalculate temp bias
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#define TEMP_CALIB_INTERVAL 30
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// LPF
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#define TEMP_DT_GYRO_ACCEL (1.0f / PIOS_SENSOR_RATE)
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#define TEMP_LPF_FC_GYRO_ACCEL 5.0f
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static const float temp_alpha_gyro_accel = LPF_ALPHA(TEMP_DT_GYRO_ACCEL, TEMP_LPF_FC_GYRO_ACCEL);
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// Interval in number of sample to recalculate temp bias
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#define BARO_TEMP_CALIB_INTERVAL 10
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// LPF
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#define TEMP_DT_BARO (1.0f / 120.0f)
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#define TEMP_LPF_FC_BARO 5.0f
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static const float temp_alpha_baro = TEMP_DT_BARO / (TEMP_DT_BARO + 1.0f / (2.0f * M_PI_F * TEMP_LPF_FC_BARO));
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#define ZERO_ROT_ANGLE 0.00001f
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// Private types
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typedef struct {
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// used to accumulate all samples in a task iteration
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Vector3i32 accum[2];
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int32_t temperature;
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uint32_t count;
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} sensor_fetch_context;
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#define MAX_SENSOR_DATA_SIZE (sizeof(PIOS_SENSORS_3Axis_SensorsWithTemp) + MAX_SENSORS_PER_INSTANCE * sizeof(Vector3i16))
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typedef union {
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PIOS_SENSORS_3Axis_SensorsWithTemp sensorSample3Axis;
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PIOS_SENSORS_1Axis_SensorsWithTemp sensorSample1Axis;
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} sensor_data;
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#define PIOS_INSTRUMENT_MODULE
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#include <pios_instrumentation_helper.h>
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PERF_DEFINE_COUNTER(counterAccelSamples);
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PERF_DEFINE_COUNTER(counterAccelPeriod);
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PERF_DEFINE_COUNTER(counterMagPeriod);
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PERF_DEFINE_COUNTER(counterBaroPeriod);
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PERF_DEFINE_COUNTER(counterSensorPeriod);
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PERF_DEFINE_COUNTER(counterSensorResets);
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// Private functions
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static void SensorsTask(void *parameters);
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static void settingsUpdatedCb(UAVObjEvent *objEv);
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static void accumulateSamples(sensor_fetch_context *sensor_context, sensor_data *sample);
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static void processSamples3d(sensor_fetch_context *sensor_context, const PIOS_SENSORS_Instance *sensor);
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static void processSamples1d(PIOS_SENSORS_1Axis_SensorsWithTemp *sample, const PIOS_SENSORS_Instance *sensor);
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static void clearContext(sensor_fetch_context *sensor_context);
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static void handleAccel(float *samples, float temperature);
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static void handleGyro(float *samples, float temperature);
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static void handleMag(float *samples, float temperature);
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static void handleBaro(float sample, float temperature);
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static void updateAccelTempBias(float temperature);
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static void updateGyroTempBias(float temperature);
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static void updateBaroTempBias(float temperature);
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// Private variables
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static sensor_data *source_data;
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static xTaskHandle sensorsTaskHandle;
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RevoCalibrationData cal;
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AccelGyroSettingsData agcal;
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// These values are initialized by settings but can be updated by the attitude algorithm
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static float mag_bias[3] = { 0, 0, 0 };
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static float mag_transform[3][3] = {
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{ 1, 0, 0 }, { 0, 1, 0 }, { 0, 0, 1 }
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};
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// Variables used to handle accel/gyro temperature bias
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static volatile bool gyro_temp_calibrated = false;
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static volatile bool accel_temp_calibrated = false;
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static float accel_temperature = NAN;
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static float gyro_temperature = NAN;
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static float accel_temp_bias[3] = { 0 };
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static float gyro_temp_bias[3] = { 0 };
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static uint8_t accel_temp_calibration_count = 0;
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static uint8_t gyro_temp_calibration_count = 0;
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static float R[3][3] = {
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{ 0 }
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};
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// Variables used to handle baro temperature bias
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static RevoSettingsBaroTempCorrectionPolynomialData baroCorrection;
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static RevoSettingsBaroTempCorrectionExtentData baroCorrectionExtent;
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static volatile bool baro_temp_correction_enabled;
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static float baro_temp_bias = 0;
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static float baro_temperature = NAN;
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static uint8_t baro_temp_calibration_count = 0;
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static int8_t rotate = 0;
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/**
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* Initialise the module. Called before the start function
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* \returns 0 on success or -1 if initialisation failed
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*/
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int32_t SensorsInitialize(void)
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{
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source_data = (sensor_data *)pios_malloc(MAX_SENSOR_DATA_SIZE);
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GyroSensorInitialize();
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AccelSensorInitialize();
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MagSensorInitialize();
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BaroSensorInitialize();
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RevoCalibrationInitialize();
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RevoSettingsInitialize();
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AttitudeSettingsInitialize();
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AccelGyroSettingsInitialize();
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rotate = 0;
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RevoSettingsConnectCallback(&settingsUpdatedCb);
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RevoCalibrationConnectCallback(&settingsUpdatedCb);
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AttitudeSettingsConnectCallback(&settingsUpdatedCb);
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AccelGyroSettingsConnectCallback(&settingsUpdatedCb);
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return 0;
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}
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/**
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* Start the task. Expects all objects to be initialized by this point.
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* \returns 0 on success or -1 if initialisation failed
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*/
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int32_t SensorsStart(void)
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{
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// Start main task
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xTaskCreate(SensorsTask, "Sensors", STACK_SIZE_BYTES / 4, NULL, TASK_PRIORITY, &sensorsTaskHandle);
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PIOS_TASK_MONITOR_RegisterTask(TASKINFO_RUNNING_SENSORS, sensorsTaskHandle);
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REGISTER_WDG();
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return 0;
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}
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MODULE_INITCALL(SensorsInitialize, SensorsStart);
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int32_t accel_test;
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int32_t gyro_test;
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int32_t mag_test;
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// int32_t pressure_test;
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/**
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* The sensor task. This polls the gyros at 500 Hz and pumps that data to
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* stabilization and to the attitude loop
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*
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*/
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uint32_t sensor_dt_us;
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static void SensorsTask(__attribute__((unused)) void *parameters)
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{
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portTickType lastSysTime;
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sensor_fetch_context sensor_context;
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bool error = false;
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const PIOS_SENSORS_Instance *sensors_list = PIOS_SENSORS_GetList();
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PIOS_SENSORS_Instance *sensor;
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AlarmsClear(SYSTEMALARMS_ALARM_SENSORS);
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settingsUpdatedCb(NULL);
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// Performance counters
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PERF_INIT_COUNTER(counterAccelSamples, 0x53000001);
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PERF_INIT_COUNTER(counterAccelPeriod, 0x53000002);
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PERF_INIT_COUNTER(counterMagPeriod, 0x53000003);
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PERF_INIT_COUNTER(counterBaroPeriod, 0x53000004);
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PERF_INIT_COUNTER(counterSensorPeriod, 0x53000005);
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PERF_INIT_COUNTER(counterSensorResets, 0x53000006);
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// Test sensors
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bool sensors_test = true;
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uint8_t count = 0;
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LL_FOREACH((PIOS_SENSORS_Instance *)sensors_list, sensor) {
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sensors_test &= PIOS_SENSORS_Test(sensor);
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count++;
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}
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PIOS_Assert(count);
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RELOAD_WDG();
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if (!sensors_test) {
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AlarmsSet(SYSTEMALARMS_ALARM_SENSORS, SYSTEMALARMS_ALARM_CRITICAL);
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while (1) {
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vTaskDelay(10);
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}
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}
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// Main task loop
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lastSysTime = xTaskGetTickCount();
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uint32_t reset_counter = 0;
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while (1) {
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// TODO: add timeouts to the sensor reads and set an error if the fail
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if (error) {
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RELOAD_WDG();
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lastSysTime = xTaskGetTickCount();
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vTaskDelayUntil(&lastSysTime, sensor_period_ticks);
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AlarmsSet(SYSTEMALARMS_ALARM_SENSORS, SYSTEMALARMS_ALARM_CRITICAL);
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error = false;
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} else {
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AlarmsClear(SYSTEMALARMS_ALARM_SENSORS);
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}
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// reset the fetch context
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clearContext(&sensor_context);
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LL_FOREACH((PIOS_SENSORS_Instance *)sensors_list, sensor) {
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// we will wait on the sensor that's marked as primary( that means the sensor with higher sample rate)
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bool is_primary = (sensor->type & PIOS_SENSORS_TYPE_3AXIS_ACCEL);
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if (!sensor->driver->is_polled) {
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const QueueHandle_t queue = PIOS_SENSORS_GetQueue(sensor);
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while (xQueueReceive(queue,
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(void *)source_data,
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(is_primary && !sensor_context.count) ? sensor_period_ticks : 0) == pdTRUE) {
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accumulateSamples(&sensor_context, source_data);
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}
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if (sensor_context.count) {
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processSamples3d(&sensor_context, sensor);
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clearContext(&sensor_context);
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} else if (is_primary) {
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PIOS_SENSOR_Reset(sensor);
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reset_counter++;
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PERF_TRACK_VALUE(counterSensorResets, reset_counter);
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error = true;
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}
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} else {
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if (PIOS_SENSORS_Poll(sensor)) {
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PIOS_SENSOR_Fetch(sensor, (void *)source_data, MAX_SENSORS_PER_INSTANCE);
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if (sensor->type & PIOS_SENSORS_TYPE_3D) {
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accumulateSamples(&sensor_context, source_data);
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processSamples3d(&sensor_context, sensor);
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} else {
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processSamples1d(&source_data->sensorSample1Axis, sensor);
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}
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clearContext(&sensor_context);
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}
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}
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}
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PERF_MEASURE_PERIOD(counterSensorPeriod);
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RELOAD_WDG();
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vTaskDelayUntil(&lastSysTime, sensor_period_ticks);
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}
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}
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static void clearContext(sensor_fetch_context *sensor_context)
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{
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// clear the context once it has finished
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for (uint32_t i = 0; i < MAX_SENSORS_PER_INSTANCE; i++) {
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sensor_context->accum[i].x = 0;
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sensor_context->accum[i].y = 0;
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sensor_context->accum[i].z = 0;
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}
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sensor_context->temperature = 0;
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sensor_context->count = 0;
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}
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static void accumulateSamples(sensor_fetch_context *sensor_context, sensor_data *sample)
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{
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for (uint32_t i = 0; (i < MAX_SENSORS_PER_INSTANCE) && (i < sample->sensorSample3Axis.count); i++) {
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sensor_context->accum[i].x += sample->sensorSample3Axis.sample[i].x;
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sensor_context->accum[i].y += sample->sensorSample3Axis.sample[i].y;
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sensor_context->accum[i].z += sample->sensorSample3Axis.sample[i].z;
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}
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sensor_context->temperature += sample->sensorSample3Axis.temperature;
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sensor_context->count++;
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}
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static void processSamples3d(sensor_fetch_context *sensor_context, const PIOS_SENSORS_Instance *sensor)
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{
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float samples[3];
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float temperature;
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float scales[MAX_SENSORS_PER_INSTANCE];
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PIOS_SENSORS_GetScales(sensor, scales, MAX_SENSORS_PER_INSTANCE);
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float inv_count = 1.0f / (float)sensor_context->count;
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if ((sensor->type & PIOS_SENSORS_TYPE_3AXIS_ACCEL) ||
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(sensor->type == PIOS_SENSORS_TYPE_3AXIS_MAG)) {
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float t = inv_count * scales[0];
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samples[0] = ((float)sensor_context->accum[0].x * t);
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samples[1] = ((float)sensor_context->accum[0].y * t);
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samples[2] = ((float)sensor_context->accum[0].z * t);
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temperature = (float)sensor_context->temperature * inv_count * 0.01f;
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if (sensor->type == PIOS_SENSORS_TYPE_3AXIS_MAG) {
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handleMag(samples, temperature);
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PERF_MEASURE_PERIOD(counterMagPeriod);
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return;
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} else {
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PERF_TRACK_VALUE(counterAccelSamples, sensor_context->count);
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PERF_MEASURE_PERIOD(counterAccelPeriod);
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handleAccel(samples, temperature);
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}
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}
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if (sensor->type & PIOS_SENSORS_TYPE_3AXIS_GYRO) {
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uint8_t index = 0;
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if (sensor->type == PIOS_SENSORS_TYPE_3AXIS_GYRO_ACCEL) {
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index = 1;
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}
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float t = inv_count * scales[index];
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samples[0] = ((float)sensor_context->accum[index].x * t);
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samples[1] = ((float)sensor_context->accum[index].y * t);
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samples[2] = ((float)sensor_context->accum[index].z * t);
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temperature = (float)sensor_context->temperature * inv_count * 0.01f;
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handleGyro(samples, temperature);
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return;
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}
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}
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static void processSamples1d(PIOS_SENSORS_1Axis_SensorsWithTemp *sample, const PIOS_SENSORS_Instance *sensor)
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{
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switch (sensor->type) {
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case PIOS_SENSORS_TYPE_1AXIS_BARO:
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PERF_MEASURE_PERIOD(counterBaroPeriod);
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handleBaro(sample->sample, sample->temperature);
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return;
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default:
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PIOS_Assert(0);
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}
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}
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static void handleAccel(float *samples, float temperature)
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{
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AccelSensorData accelSensorData;
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updateAccelTempBias(temperature);
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float accels_out[3] = { samples[0] * agcal.accel_scale.X - agcal.accel_bias.X - accel_temp_bias[0],
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samples[1] * agcal.accel_scale.Y - agcal.accel_bias.Y - accel_temp_bias[1],
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samples[2] * agcal.accel_scale.Z - agcal.accel_bias.Z - accel_temp_bias[2] };
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rot_mult(R, accels_out, samples);
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accelSensorData.x = samples[0];
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accelSensorData.y = samples[1];
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accelSensorData.z = samples[2];
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accelSensorData.temperature = temperature;
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AccelSensorSet(&accelSensorData);
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}
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static void handleGyro(float *samples, float temperature)
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{
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GyroSensorData gyroSensorData;
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updateGyroTempBias(temperature);
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float gyros_out[3] = { samples[0] * agcal.gyro_scale.X - agcal.gyro_bias.X - gyro_temp_bias[0],
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samples[1] * agcal.gyro_scale.Y - agcal.gyro_bias.Y - gyro_temp_bias[1],
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samples[2] * agcal.gyro_scale.Z - agcal.gyro_bias.Z - gyro_temp_bias[2] };
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rot_mult(R, gyros_out, samples);
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gyroSensorData.temperature = temperature;
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gyroSensorData.x = samples[0];
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gyroSensorData.y = samples[1];
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gyroSensorData.z = samples[2];
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GyroSensorSet(&gyroSensorData);
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}
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static void handleMag(float *samples, float temperature)
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{
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MagSensorData mag;
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float mags[3] = { (float)samples[1] - mag_bias[0],
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(float)samples[0] - mag_bias[1],
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(float)samples[2] - mag_bias[2] };
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rot_mult(mag_transform, mags, samples);
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mag.x = samples[0];
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mag.y = samples[1];
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mag.z = samples[2];
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mag.temperature = temperature;
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MagSensorSet(&mag);
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}
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static void handleBaro(float sample, float temperature)
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{
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updateBaroTempBias(temperature);
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sample -= baro_temp_bias;
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float altitude = 44330.0f * (1.0f - powf((sample) / PIOS_CONST_MKS_STD_ATMOSPHERE_F, (1.0f / 5.255f)));
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if (!isnan(altitude)) {
|
|
BaroSensorData data;
|
|
data.Altitude = altitude;
|
|
data.Temperature = temperature;
|
|
data.Pressure = sample;
|
|
// Update the BasoSensor UAVObject
|
|
BaroSensorSet(&data);
|
|
}
|
|
}
|
|
|
|
static void updateAccelTempBias(float temperature)
|
|
{
|
|
if (isnan(accel_temperature)) {
|
|
accel_temperature = temperature;
|
|
}
|
|
accel_temperature = temp_alpha_gyro_accel * (temperature - accel_temperature) + accel_temperature;
|
|
|
|
if ((accel_temp_calibrated) && !accel_temp_calibration_count) {
|
|
accel_temp_calibration_count = TEMP_CALIB_INTERVAL;
|
|
if (accel_temp_calibrated) {
|
|
float ctemp = boundf(accel_temperature, agcal.temp_calibrated_extent.max, agcal.temp_calibrated_extent.min);
|
|
accel_temp_bias[0] = agcal.accel_temp_coeff.X * ctemp;
|
|
accel_temp_bias[1] = agcal.accel_temp_coeff.Y * ctemp;
|
|
accel_temp_bias[2] = agcal.accel_temp_coeff.Z * ctemp;
|
|
}
|
|
}
|
|
accel_temp_calibration_count--;
|
|
}
|
|
|
|
static void updateGyroTempBias(float temperature)
|
|
{
|
|
if (isnan(gyro_temperature)) {
|
|
gyro_temperature = temperature;
|
|
}
|
|
|
|
gyro_temperature = temp_alpha_gyro_accel * (temperature - gyro_temperature) + gyro_temperature;
|
|
|
|
if (gyro_temp_calibrated && !gyro_temp_calibration_count) {
|
|
gyro_temp_calibration_count = TEMP_CALIB_INTERVAL;
|
|
|
|
if (gyro_temp_calibrated) {
|
|
float ctemp = boundf(gyro_temperature, agcal.temp_calibrated_extent.max, agcal.temp_calibrated_extent.min);
|
|
gyro_temp_bias[0] = (agcal.gyro_temp_coeff.X + agcal.gyro_temp_coeff.X2 * ctemp) * ctemp;
|
|
gyro_temp_bias[1] = (agcal.gyro_temp_coeff.Y + agcal.gyro_temp_coeff.Y2 * ctemp) * ctemp;
|
|
gyro_temp_bias[2] = (agcal.gyro_temp_coeff.Z + agcal.gyro_temp_coeff.Z2 * ctemp) * ctemp;
|
|
}
|
|
}
|
|
gyro_temp_calibration_count--;
|
|
}
|
|
|
|
static void updateBaroTempBias(float temperature)
|
|
{
|
|
if (isnan(baro_temperature)) {
|
|
baro_temperature = temperature;
|
|
}
|
|
|
|
baro_temperature = temp_alpha_baro * (temperature - baro_temperature) + baro_temperature;
|
|
|
|
if (baro_temp_correction_enabled && !baro_temp_calibration_count) {
|
|
baro_temp_calibration_count = BARO_TEMP_CALIB_INTERVAL;
|
|
// pressure bias = A + B*t + C*t^2 + D * t^3
|
|
// in case the temperature is outside of the calibrated range, uses the nearest extremes
|
|
float ctemp = boundf(baro_temperature, baroCorrectionExtent.max, baroCorrectionExtent.min);
|
|
baro_temp_bias = baroCorrection.a + ((baroCorrection.d * ctemp + baroCorrection.c) * ctemp + baroCorrection.b) * ctemp;
|
|
}
|
|
baro_temp_calibration_count--;
|
|
}
|
|
/**
|
|
* Locally cache some variables from the AtttitudeSettings object
|
|
*/
|
|
static void settingsUpdatedCb(__attribute__((unused)) UAVObjEvent *objEv)
|
|
{
|
|
RevoCalibrationGet(&cal);
|
|
AccelGyroSettingsGet(&agcal);
|
|
mag_bias[0] = cal.mag_bias.X;
|
|
mag_bias[1] = cal.mag_bias.Y;
|
|
mag_bias[2] = cal.mag_bias.Z;
|
|
|
|
accel_temp_calibrated = (agcal.temp_calibrated_extent.max - agcal.temp_calibrated_extent.min > .1f) &&
|
|
(fabsf(agcal.accel_temp_coeff.X) > 1e-9f || fabsf(agcal.accel_temp_coeff.Y) > 1e-9f || fabsf(agcal.accel_temp_coeff.Z) > 1e-9f);
|
|
|
|
gyro_temp_calibrated = (agcal.temp_calibrated_extent.max - agcal.temp_calibrated_extent.min > .1f) &&
|
|
(fabsf(agcal.gyro_temp_coeff.X) > 1e-9f || fabsf(agcal.gyro_temp_coeff.Y) > 1e-9f ||
|
|
fabsf(agcal.gyro_temp_coeff.Z) > 1e-9f || fabsf(agcal.gyro_temp_coeff.Z2) > 1e-9f);
|
|
|
|
|
|
AttitudeSettingsData attitudeSettings;
|
|
AttitudeSettingsGet(&attitudeSettings);
|
|
|
|
// Indicates not to expend cycles on rotation
|
|
if (fabsf(attitudeSettings.BoardRotation.Roll) < ZERO_ROT_ANGLE
|
|
&& fabsf(attitudeSettings.BoardRotation.Pitch) < ZERO_ROT_ANGLE &&
|
|
fabsf(attitudeSettings.BoardRotation.Yaw) < ZERO_ROT_ANGLE) {
|
|
rotate = 0;
|
|
} else {
|
|
rotate = 1;
|
|
}
|
|
|
|
const float rpy[3] = { attitudeSettings.BoardRotation.Roll,
|
|
attitudeSettings.BoardRotation.Pitch,
|
|
attitudeSettings.BoardRotation.Yaw };
|
|
|
|
float rotationQuat[4];
|
|
RPY2Quaternion(rpy, rotationQuat);
|
|
|
|
if (fabsf(attitudeSettings.BoardLevelTrim.Roll) > ZERO_ROT_ANGLE ||
|
|
fabsf(attitudeSettings.BoardLevelTrim.Pitch) > ZERO_ROT_ANGLE) {
|
|
float trimQuat[4];
|
|
float sumQuat[4];
|
|
rotate = 1;
|
|
|
|
const float trimRpy[3] = { attitudeSettings.BoardLevelTrim.Roll, attitudeSettings.BoardLevelTrim.Pitch, 0.0f };
|
|
RPY2Quaternion(trimRpy, trimQuat);
|
|
|
|
quat_mult(rotationQuat, trimQuat, sumQuat);
|
|
Quaternion2R(sumQuat, R);
|
|
} else {
|
|
Quaternion2R(rotationQuat, R);
|
|
}
|
|
matrix_mult_3x3f((float(*)[3])RevoCalibrationmag_transformToArray(cal.mag_transform), R, mag_transform);
|
|
|
|
RevoSettingsBaroTempCorrectionPolynomialGet(&baroCorrection);
|
|
RevoSettingsBaroTempCorrectionExtentGet(&baroCorrectionExtent);
|
|
baro_temp_correction_enabled = !(baroCorrectionExtent.max - baroCorrectionExtent.min < 0.1f ||
|
|
(baroCorrection.a < 1e-9f && baroCorrection.b < 1e-9f && baroCorrection.c < 1e-9f && baroCorrection.d < 1e-9f));
|
|
}
|
|
/**
|
|
* @}
|
|
* @}
|
|
*/
|