<long_desc>Default acceptance radius, overridden by acceptance radius of waypoint if set. For fixed wing the L1 turning distance is used for horizontal acceptance.</long_desc>
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@@ -7805,7 +7805,7 @@ to takeoff is reached</short_desc>
<short_desc>Airspeed sensor compensation model for the SDP3x</short_desc>
<long_desc>Model with Pitot CAL_AIR_TUBED_MM: Not used, 1.5 mm tubes assumed. CAL_AIR_TUBELEN: Length of the tubes connecting the pitot to the sensor. Model without Pitot (1.5 mm tubes) CAL_AIR_TUBED_MM: Not used, 1.5 mm tubes assumed. CAL_AIR_TUBELEN: Length of the tubes connecting the pitot to the sensor. Tube Pressure Drop CAL_AIR_TUBED_MM: Diameter in mm of the pitot and tubes, must have the same diameter. CAL_AIR_TUBELEN: Length of the tubes connecting the pitot to the sensor and the static + dynamic port length of the pitot.</long_desc>
<scope>modules/sensors</scope>
<values>
<valuecode="0">Model with Pitot</value>
<valuecode="1">Model without Pitot (1.5 mm tubes)</value>
<short_desc>Rotation of magnetometer 0 relative to airframe</short_desc>
<long_desc>An internal magnetometer will force a value of -1, so a GCS should only attempt to configure the rotation if the value is greater than or equal to zero.</long_desc>
<min>-1</min>
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@@ -8086,40 +8061,40 @@ to takeoff is reached</short_desc>
<short_desc>Rotation of magnetometer 1 relative to airframe</short_desc>
<long_desc>An internal magnetometer will force a value of -1, so a GCS should only attempt to configure the rotation if the value is greater than or equal to zero.</long_desc>
<min>-1</min>
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@@ -8156,40 +8131,40 @@ to takeoff is reached</short_desc>
<short_desc>Rotation of magnetometer 2 relative to airframe</short_desc>
<long_desc>An internal magnetometer will force a value of -1, so a GCS should only attempt to configure the rotation if the value is greater than or equal to zero.</long_desc>
<min>-1</min>
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@@ -8226,40 +8201,40 @@ to takeoff is reached</short_desc>
<short_desc>Rotation of magnetometer 2 relative to airframe</short_desc>
<long_desc>An internal magnetometer will force a value of -1, so a GCS should only attempt to configure the rotation if the value is greater than or equal to zero.</long_desc>
<min>-1</min>
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@@ -8296,31 +8271,31 @@ to takeoff is reached</short_desc>
@@ -8329,7 +8304,7 @@ to takeoff is reached</short_desc>
<long_desc>Pick the appropriate scaling from the datasheet. this number defines the (linear) conversion from voltage to Pascal (pa). For the MPXV7002DP this is 1000. NOTE: If the sensor always registers zero, try switching the static and dynamic tubes.</long_desc>
<short_desc>Airspeed sensor compensation model for the SDP3x</short_desc>
<long_desc>Model with Pitot CAL_AIR_TUBED_MM: Not used, 1.5 mm tubes assumed. CAL_AIR_TUBELEN: Length of the tubes connecting the pitot to the sensor. Model without Pitot (1.5 mm tubes) CAL_AIR_TUBED_MM: Not used, 1.5 mm tubes assumed. CAL_AIR_TUBELEN: Length of the tubes connecting the pitot to the sensor. Tube Pressure Drop CAL_AIR_TUBED_MM: Diameter in mm of the pitot and tubes, must have the same diameter. CAL_AIR_TUBELEN: Length of the tubes connecting the pitot to the sensor and the static + dynamic port length of the pitot.</long_desc>
<scope>modules/sensors</scope>
<values>
<valuecode="0">Model with Pitot</value>
<valuecode="1">Model without Pitot (1.5 mm tubes)</value>