forked from Archive/PX4-Autopilot
AirspeedSelector: improve/shorten param descriptions
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
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@ -1,6 +1,6 @@
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/**
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* Airspeed Selector: Wind estimator wind process noise noise spectral density
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* Wind estimator wind process noise spectral density
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*
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* Wind process noise of the internal wind estimator(s) of the airspeed selector.
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* When unaided, the wind estimate uncertainty (1-sigma, in m/s) increases by this amount every second.
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@ -14,7 +14,7 @@
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PARAM_DEFINE_FLOAT(ASPD_WIND_NSD, 1.e-2f);
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/**
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* Airspeed Selector: Wind estimator true airspeed scale process noise spectral density
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* Wind estimator true airspeed scale process noise spectral density
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*
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* Airspeed scale process noise of the internal wind estimator(s) of the airspeed selector.
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* When unaided, the scale uncertainty (1-sigma, unitless) increases by this amount every second.
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@ -28,7 +28,7 @@ PARAM_DEFINE_FLOAT(ASPD_WIND_NSD, 1.e-2f);
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PARAM_DEFINE_FLOAT(ASPD_SCALE_NSD, 1.e-4f);
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/**
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* Airspeed Selector: Wind estimator true airspeed measurement noise
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* Wind estimator true airspeed measurement noise
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*
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* True airspeed measurement noise of the internal wind estimator(s) of the airspeed selector.
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*
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@ -41,7 +41,7 @@ PARAM_DEFINE_FLOAT(ASPD_SCALE_NSD, 1.e-4f);
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PARAM_DEFINE_FLOAT(ASPD_TAS_NOISE, 1.4f);
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/**
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* Airspeed Selector: Wind estimator sideslip measurement noise
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* Wind estimator sideslip measurement noise
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*
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* Sideslip measurement noise of the internal wind estimator(s) of the airspeed selector.
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*
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@ -54,7 +54,7 @@ PARAM_DEFINE_FLOAT(ASPD_TAS_NOISE, 1.4f);
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PARAM_DEFINE_FLOAT(ASPD_BETA_NOISE, 0.3f);
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/**
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* Airspeed Selector: Gate size for true airspeed fusion
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* Gate size for true airspeed fusion
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*
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* Sets the number of standard deviations used by the innovation consistency test.
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*
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@ -66,7 +66,7 @@ PARAM_DEFINE_FLOAT(ASPD_BETA_NOISE, 0.3f);
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PARAM_DEFINE_INT32(ASPD_TAS_GATE, 3);
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/**
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* Airspeed Selector: Gate size for sideslip angle fusion
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* Gate size for sideslip angle fusion
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*
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* Sets the number of standard deviations used by the innovation consistency test.
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*
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@ -148,7 +148,6 @@ PARAM_DEFINE_INT32(ASPD_PRIMARY, 1);
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* Enable checks on airspeed sensors
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*
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* Controls which checks are run to check airspeed data for validity. Only applied if ASPD_PRIMARY > 0.
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* Note that the data missing check is enabled if any of the options is set.
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*
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* @min 0
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* @max 15
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@ -232,7 +231,7 @@ PARAM_DEFINE_INT32(ASPD_FS_T_START, -1);
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* Horizontal wind uncertainty threshold for synthetic airspeed.
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*
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* The synthetic airspeed estimate (from groundspeed and heading) will be declared valid
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* as soon and as long the horizontal wind uncertainty drops below this value.
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* as soon and as long the horizontal wind uncertainty is below this value.
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*
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* @unit m/s
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* @min 0.001
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