add low pass filter to meas airspeed driver including logging of filtered value

This commit is contained in:
Thomas Gubler
2014-03-14 01:13:22 +01:00
parent b6a087e921
commit 0784ef9189
6 changed files with 18 additions and 6 deletions
+1
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@@ -1142,6 +1142,7 @@ int sdlog2_thread_main(int argc, char *argv[])
log_msg.body.log_SENS.baro_alt = buf.sensor.baro_alt_meter;
log_msg.body.log_SENS.baro_temp = buf.sensor.baro_temp_celcius;
log_msg.body.log_SENS.diff_pres = buf.sensor.differential_pressure_pa;
log_msg.body.log_SENS.diff_pres_filtered = buf.sensor.differential_pressure_filtered_pa;
LOGBUFFER_WRITE_AND_COUNT(SENS);
}
}
+2 -1
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@@ -92,6 +92,7 @@ struct log_SENS_s {
float baro_alt;
float baro_temp;
float diff_pres;
float diff_pres_filtered;
};
/* --- LPOS - LOCAL POSITION --- */
@@ -306,7 +307,7 @@ static const struct log_format_s log_formats[] = {
LOG_FORMAT(ATT, "fffffffff", "Roll,Pitch,Yaw,RollRate,PitchRate,YawRate,GX,GY,GZ"),
LOG_FORMAT(ATSP, "ffff", "RollSP,PitchSP,YawSP,ThrustSP"),
LOG_FORMAT(IMU, "fffffffff", "AccX,AccY,AccZ,GyroX,GyroY,GyroZ,MagX,MagY,MagZ"),
LOG_FORMAT(SENS, "ffff", "BaroPres,BaroAlt,BaroTemp,DiffPres"),
LOG_FORMAT(SENS, "ffff", "BaroPres,BaroAlt,BaroTemp,DiffPres,DiffPresFilt"),
LOG_FORMAT(LPOS, "ffffffLLfBBB", "X,Y,Z,VX,VY,VZ,RefLat,RefLon,RefAlt,XYFlags,ZFlags,Landed"),
LOG_FORMAT(LPSP, "ffff", "X,Y,Z,Yaw"),
LOG_FORMAT(GPS, "QBffLLfffff", "GPSTime,FixType,EPH,EPV,Lat,Lon,Alt,VelN,VelE,VelD,Cog"),
+1
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@@ -1028,6 +1028,7 @@ Sensors::diff_pres_poll(struct sensor_combined_s &raw)
orb_copy(ORB_ID(differential_pressure), _diff_pres_sub, &_diff_pres);
raw.differential_pressure_pa = _diff_pres.differential_pressure_pa;
raw.differential_pressure_filtered_pa = _diff_pres.differential_pressure_filtered_pa;
raw.differential_pressure_counter++;
_airspeed.indicated_airspeed_m_s = calc_indicated_airspeed(_diff_pres.differential_pressure_pa);
@@ -54,8 +54,9 @@
struct differential_pressure_s {
uint64_t timestamp; /**< microseconds since system boot, needed to integrate */
uint64_t error_count;
float differential_pressure_pa; /**< Differential pressure reading */
float max_differential_pressure_pa; /**< Maximum differential pressure reading */
float differential_pressure_pa; /**< Differential pressure reading */
float differential_pressure_filtered_pa; /**< Low pass filtered differential pressure reading */
float max_differential_pressure_pa; /**< Maximum differential pressure reading */
float voltage; /**< Voltage from analog airspeed sensors (voltage divider already compensated) */
float temperature; /**< Temperature provided by sensor */
+3 -2
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@@ -103,8 +103,9 @@ struct sensor_combined_s {
float mcu_temp_celcius; /**< Internal temperature measurement of MCU */
uint32_t baro_counter; /**< Number of raw baro measurements taken */
float differential_pressure_pa; /**< Airspeed sensor differential pressure */
uint32_t differential_pressure_counter; /**< Number of raw differential pressure measurements taken */
float differential_pressure_pa; /**< Airspeed sensor differential pressure */
float differential_pressure_filtered_pa; /**< Low pass filtered airspeed sensor differential pressure reading */
uint32_t differential_pressure_counter; /**< Number of raw differential pressure measurements taken */
};
/**