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Commit 05992691 authored by PX4 Jenkins's avatar PX4 Jenkins Committed by Daniel Agar
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Update PX4 Firmware metadata Thu Mar 8 22:37:37 CST 2018

parent 7ce0a866
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src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
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...@@ -9336,9 +9336,10 @@ Airbrakes need to be enables for your selected model/mixer</short_desc> ...@@ -9336,9 +9336,10 @@ Airbrakes need to be enables for your selected model/mixer</short_desc>
<scope>modules/vtol_att_control</scope> <scope>modules/vtol_att_control</scope>
</parameter> </parameter>
<parameter default="0.0" name="VT_B_TRANS_THR" type="FLOAT"> <parameter default="0.0" name="VT_B_TRANS_THR" type="FLOAT">
<short_desc>Thottle output during back transition <short_desc>Target throttle value for the transition to hover flight.
For ESCs and mixers that support reverse thrust on low PWM values set this to a negative value to apply active breaking standard vtol: pusher
For ESCs that support thrust reversal with a control channel please set VT_B_REV_OUT and set this to a positive value to apply active breaking</short_desc> tailsitter, tiltrotor: main throttle</short_desc>
<long_desc>Note for standard vtol: For ESCs and mixers that support reverse thrust on low PWM values set this to a negative value to apply active breaking For ESCs that support thrust reversal with a control channel please set VT_B_REV_OUT and set this to a positive value to apply active breaking</long_desc>
<min>-1</min> <min>-1</min>
<max>1</max> <max>1</max>
<decimal>2</decimal> <decimal>2</decimal>
...@@ -9411,15 +9412,6 @@ to accelerate forward if necessary</short_desc> ...@@ -9411,15 +9412,6 @@ to accelerate forward if necessary</short_desc>
<boolean /> <boolean />
<scope>modules/vtol_att_control</scope> <scope>modules/vtol_att_control</scope>
</parameter> </parameter>
<parameter default="0.0" name="VT_FW_PITCH_TRIM" type="FLOAT">
<short_desc>Fixed wing pitch trim</short_desc>
<long_desc>This parameter allows to adjust the neutral elevon position in fixed wing mode.</long_desc>
<min>-1.0</min>
<max>1.0</max>
<decimal>2</decimal>
<increment>0.01</increment>
<scope>modules/vtol_att_control</scope>
</parameter>
<parameter default="0" name="VT_FW_QC_P" type="INT32"> <parameter default="0" name="VT_FW_QC_P" type="INT32">
<short_desc>QuadChute Max Pitch</short_desc> <short_desc>QuadChute Max Pitch</short_desc>
<long_desc>Maximum pitch angle before QuadChute engages Above this the vehicle will transition back to MC mode and enter failsafe RTL</long_desc> <long_desc>Maximum pitch angle before QuadChute engages Above this the vehicle will transition back to MC mode and enter failsafe RTL</long_desc>
...@@ -9444,6 +9436,16 @@ to accelerate forward if necessary</short_desc> ...@@ -9444,6 +9436,16 @@ to accelerate forward if necessary</short_desc>
<increment>1</increment> <increment>1</increment>
<scope>modules/vtol_att_control</scope> <scope>modules/vtol_att_control</scope>
</parameter> </parameter>
<parameter default="1.0" name="VT_F_TRANS_THR" type="FLOAT">
<short_desc>Target throttle value for the transition to fixed wing flight.
standard vtol: pusher
tailsitter, tiltrotor: main throttle</short_desc>
<min>0.0</min>
<max>1.0</max>
<decimal>3</decimal>
<increment>0.01</increment>
<scope>modules/vtol_att_control</scope>
</parameter>
<parameter default="6.0" name="VT_F_TR_OL_TM" type="FLOAT"> <parameter default="6.0" name="VT_F_TR_OL_TM" type="FLOAT">
<short_desc>Airspeed less front transition time (open loop)</short_desc> <short_desc>Airspeed less front transition time (open loop)</short_desc>
<long_desc>The duration of the front transition when there is no airspeed feedback available.</long_desc> <long_desc>The duration of the front transition when there is no airspeed feedback available.</long_desc>
...@@ -9474,6 +9476,14 @@ to accelerate forward if necessary</short_desc> ...@@ -9474,6 +9476,14 @@ to accelerate forward if necessary</short_desc>
<boolean /> <boolean />
<scope>modules/vtol_att_control</scope> <scope>modules/vtol_att_control</scope>
</parameter> </parameter>
<parameter default="3.0" name="VT_PSHER_RMP_DT" type="FLOAT">
<short_desc>Defines the time window during which the pusher throttle will be ramped up linearly to VT_F_TRANS_THR during a transition
to fixed wing mode. Zero or negative values will produce an instant throttle rise to VT_F_TRANS_THR</short_desc>
<max>20</max>
<decimal>2</decimal>
<increment>0.01</increment>
<scope>modules/vtol_att_control</scope>
</parameter>
<parameter default="1.0" name="VT_TILT_FW" type="FLOAT"> <parameter default="1.0" name="VT_TILT_FW" type="FLOAT">
<short_desc>Position of tilt servo in fw mode</short_desc> <short_desc>Position of tilt servo in fw mode</short_desc>
<min>0.0</min> <min>0.0</min>
...@@ -9516,14 +9526,6 @@ to accelerate forward if necessary</short_desc> ...@@ -9516,14 +9526,6 @@ to accelerate forward if necessary</short_desc>
<increment>0.01</increment> <increment>0.01</increment>
<scope>modules/vtol_att_control</scope> <scope>modules/vtol_att_control</scope>
</parameter> </parameter>
<parameter default="0.6" name="VT_TRANS_THR" type="FLOAT">
<short_desc>Target throttle value for pusher/puller motor during the transition to fw mode</short_desc>
<min>0.0</min>
<max>1.0</max>
<decimal>3</decimal>
<increment>0.01</increment>
<scope>modules/vtol_att_control</scope>
</parameter>
<parameter default="15.0" name="VT_TRANS_TIMEOUT" type="FLOAT"> <parameter default="15.0" name="VT_TRANS_TIMEOUT" type="FLOAT">
<short_desc>Front transition timeout</short_desc> <short_desc>Front transition timeout</short_desc>
<long_desc>Time in seconds after which transition will be cancelled. Disabled if set to 0.</long_desc> <long_desc>Time in seconds after which transition will be cancelled. Disabled if set to 0.</long_desc>
......
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