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AirspeedValidated: correct typo

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Balduin 2026-01-05 17:58:54 +01:00
parent 672d3d05c6
commit 44a03e8925
2 changed files with 9 additions and 9 deletions
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10
msg/versioned/AirspeedValidated.msg
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@ -18,10 +18,10 @@ int8 SOURCE_GROUND_MINUS_WIND = 0 # Ground speed minus wind
int8 SOURCE_SENSOR_1 = 1 # Sensor 1
int8 SOURCE_SENSOR_2 = 2 # Sensor 2
int8 SOURCE_SENSOR_3 = 3 # Sensor 3
int8 SOURCE_SYNTHETIC = 4 # Synthetic airspeed
int8 SOURCE_SYNTHETIC = 4 # Synthetic airspeed
float32 calibrated_ground_minus_wind_m_s # [m/s] [@invalid NaN] CAS calculated from groundspeed - windspeed, where windspeed is estimated based on a zero-sideslip assumption
float32 calibraded_airspeed_synth_m_s # [m/s] [@invalid NaN] Synthetic airspeed
float32 airspeed_derivative_filtered # [m/s^2] Filtered indicated airspeed derivative
float32 throttle_filtered # [-] Filtered fixed-wing throttle
float32 pitch_filtered # [rad] Filtered pitch
float32 calibrated_airspeed_synth_m_s # [m/s] [@invalid NaN] Synthetic airspeed
float32 airspeed_derivative_filtered # [m/s^2] Filtered indicated airspeed derivative
float32 throttle_filtered # [-] Filtered fixed-wing throttle
float32 pitch_filtered # [rad] Filtered pitch

8
src/modules/airspeed_selector/airspeed_selector_main.cpp
View File

@ -742,7 +742,7 @@ void AirspeedModule::select_airspeed_and_publish()
airspeed_validated_s airspeed_validated = {};
airspeed_validated.timestamp = _time_now_usec;
airspeed_validated.calibrated_ground_minus_wind_m_s = NAN;
airspeed_validated.calibraded_airspeed_synth_m_s = NAN;
airspeed_validated.calibrated_airspeed_synth_m_s = NAN;
airspeed_validated.indicated_airspeed_m_s = NAN;
airspeed_validated.calibrated_airspeed_m_s = NAN;
airspeed_validated.true_airspeed_m_s = NAN;
@ -764,7 +764,7 @@ void AirspeedModule::select_airspeed_and_publish()
airspeed_validated.calibrated_airspeed_m_s = _ground_minus_wind_CAS;
airspeed_validated.true_airspeed_m_s = _ground_minus_wind_TAS;
airspeed_validated.calibrated_ground_minus_wind_m_s = _ground_minus_wind_CAS;
airspeed_validated.calibraded_airspeed_synth_m_s = get_synthetic_airspeed(airspeed_validated.throttle_filtered);
airspeed_validated.calibrated_airspeed_synth_m_s = get_synthetic_airspeed(airspeed_validated.throttle_filtered);
break;
@ -774,7 +774,7 @@ void AirspeedModule::select_airspeed_and_publish()
float synthetic_airspeed = get_synthetic_airspeed(airspeed_validated.throttle_filtered);
airspeed_validated.calibrated_airspeed_m_s = synthetic_airspeed;
airspeed_validated.indicated_airspeed_m_s = synthetic_airspeed;
airspeed_validated.calibraded_airspeed_synth_m_s = synthetic_airspeed;
airspeed_validated.calibrated_airspeed_synth_m_s = synthetic_airspeed;
airspeed_validated.true_airspeed_m_s =
calc_true_from_calibrated_airspeed(synthetic_airspeed, _vehicle_air_data.rho);
break;
@ -785,7 +785,7 @@ void AirspeedModule::select_airspeed_and_publish()
airspeed_validated.calibrated_airspeed_m_s = _airspeed_validator[valid_airspeed_index - 1].get_CAS();
airspeed_validated.true_airspeed_m_s = _airspeed_validator[valid_airspeed_index - 1].get_TAS();
airspeed_validated.calibrated_ground_minus_wind_m_s = _ground_minus_wind_CAS;
airspeed_validated.calibraded_airspeed_synth_m_s = get_synthetic_airspeed(airspeed_validated.throttle_filtered);
airspeed_validated.calibrated_airspeed_synth_m_s = get_synthetic_airspeed(airspeed_validated.throttle_filtered);
break;
}