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Attitude: Do not start attitude estimation until accel data appears. This
fixes the NaN when AttitudeSettings not available.
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69f8aac967
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@ -76,7 +76,7 @@ static void AttitudeTask(void *parameters);
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static float gyro_correct_int[3] = {0,0,0};
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static xQueueHandle gyro_queue;
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static void updateSensors(AttitudeRawData *);
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static int8_t updateSensors(AttitudeRawData *);
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static void updateAttitude(AttitudeRawData *);
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static void settingsUpdatedCb(UAVObjEvent * objEv);
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@ -163,6 +163,11 @@ static void AttitudeTask(void *parameters)
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PIOS_FLASH_DISABLE;
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PIOS_ADXL345_Init();
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// Set critical error and wait until the accel is producing data
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while(PIOS_ADXL345_FifoElements() == 0) {
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AlarmsSet(SYSTEMALARMS_ALARM_ATTITUDE, SYSTEMALARMS_ALARM_CRITICAL);
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PIOS_WDG_UpdateFlag(PIOS_WDG_ATTITUDE);
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}
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// Force settings update to make sure rotation loaded
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settingsUpdatedCb(AttitudeSettingsHandle());
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@ -197,14 +202,24 @@ static void AttitudeTask(void *parameters)
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AttitudeRawData attitudeRaw;
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AttitudeRawGet(&attitudeRaw);
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updateSensors(&attitudeRaw);
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if(updateSensors(&attitudeRaw) != 0)
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AlarmsSet(SYSTEMALARMS_ALARM_ATTITUDE, SYSTEMALARMS_ALARM_ERROR);
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else {
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// Only update attitude when sensor data is good
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updateAttitude(&attitudeRaw);
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AttitudeRawSet(&attitudeRaw);
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AlarmsClear(SYSTEMALARMS_ALARM_ATTITUDE);
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}
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}
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}
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static void updateSensors(AttitudeRawData * attitudeRaw)
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/**
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* Get an update from the sensors
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* @param[in] attitudeRaw Populate the UAVO instead of saving right here
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* @return 0 if successfull, -1 if not
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*/
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static int8_t updateSensors(AttitudeRawData * attitudeRaw)
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{
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struct pios_adxl345_data accel_data;
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float gyro[4];
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@ -212,9 +227,12 @@ static void updateSensors(AttitudeRawData * attitudeRaw)
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// Only wait the time for two nominal updates before setting an alarm
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if(xQueueReceive(gyro_queue, (void * const) gyro, UPDATE_RATE * 2) == errQUEUE_EMPTY) {
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AlarmsSet(SYSTEMALARMS_ALARM_ATTITUDE, SYSTEMALARMS_ALARM_ERROR);
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return;
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return -1;
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}
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// No accel data available
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if(PIOS_ADXL345_FifoElements() == 0)
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return -1;
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// First sample is temperature
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attitudeRaw->gyros[ATTITUDERAW_GYROS_X] = -(gyro[1] - GYRO_NEUTRAL) * gyroGain;
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@ -270,6 +288,8 @@ static void updateSensors(AttitudeRawData * attitudeRaw)
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// Because most crafts wont get enough information from gravity to zero yaw gyro, we try
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// and make it average zero (weakly)
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gyro_correct_int[2] += - attitudeRaw->gyros[ATTITUDERAW_GYROS_Z] * yawBiasRate;
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return 0;
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}
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static void updateAttitude(AttitudeRawData * attitudeRaw)
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@ -307,6 +327,7 @@ static void updateAttitude(AttitudeRawData * attitudeRaw)
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// Accumulate integral of error. Scale here so that units are (deg/s) but Ki has units of s
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gyro_correct_int[0] += accel_err[0] * accelKi;
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gyro_correct_int[1] += accel_err[1] * accelKi;
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//gyro_correct_int[2] += accel_err[2] * settings.AccelKI * dT;
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// Correct rates based on error, integral component dealt with in updateSensors
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@ -96,6 +96,22 @@ void PIOS_ADXL345_Init()
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PIOS_ADXL345_SetMeasure(1);
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}
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/**
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* @brief Return number of entries in the fifo
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*/
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uint8_t PIOS_ADXL345_FifoElements()
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{
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uint8_t buf[2] = {0,0};
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uint8_t rec[2] = {0,0};
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buf[0] = ADXL_FIFOSTATUS_ADDR | ADXL_READ_BIT ; // Read fifo status
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PIOS_ADXL345_ClaimBus();
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PIOS_SPI_TransferBlock(PIOS_SPI_ACCEL,&buf[0],&rec[0],sizeof(buf),NULL);
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PIOS_ADXL345_ReleaseBus();
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return rec[1] & 0x3f;
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}
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/**
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* @brief Read a single set of values from the x y z channels
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* @returns The number of samples remaining in the fifo
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@ -16,6 +16,7 @@
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#define ADXL_MULTI_BIT 0x40
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#define ADXL_X0_ADDR 0x32
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#define ADXL_FIFOSTATUS_ADDR 0x39
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#define ADXL_RATE_ADDR 0x2C
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#define ADXL_RATE_100 0x0A
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@ -52,5 +53,6 @@ void PIOS_ADXL345_FifoDepth(uint8_t depth);
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void PIOS_ADXL345_Attach(uint32_t spi_id);
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void PIOS_ADXL345_Init();
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uint8_t PIOS_ADXL345_Read(struct pios_adxl345_data * data);
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uint8_t PIOS_ADXL345_FifoElements();
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#endif
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