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Do not make minimum airspeed assumptions, as we can trust our digital sensor a bit. A blocked pitot also most likely will result in more than just 6.5 m/s airspeed and so the check is based on a bunch of weak assumptions

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This commit is contained in:
Lorenz Meier
2014-04-05 21:06:21 +02:00
parent be6c0d2ece
commit 4a0c660088
1 changed files with 3 additions and 4 deletions
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src/modules/fw_att_control/fw_att_control_main.cpp
+3 -4
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@@ -660,14 +660,13 @@ FixedwingAttitudeControl::task_main()
float airspeed;
/* if airspeed is smaller than min, the sensor is not giving good readings */
if ((_airspeed.indicated_airspeed_m_s < 0.5f * _parameters.airspeed_min) ||
!isfinite(_airspeed.indicated_airspeed_m_s) ||
/* if airspeed is not updating, we assume the normal average speed */
if (!isfinite(_airspeed.true_airspeed_m_s) ||
hrt_elapsed_time(&_airspeed.timestamp) > 1e6) {
airspeed = _parameters.airspeed_trim;
} else {
airspeed = _airspeed.indicated_airspeed_m_s;
airspeed = _airspeed.true_airspeed_m_s;
}
float airspeed_scaling = _parameters.airspeed_trim / airspeed;