Skip to content

Q
qgroundcontrol
Commit 86aacfb5 authored by PX4 Jenkins's avatar PX4 Jenkins Committed by Daniel Agar
Browse files
Options

Update PX4 Firmware metadata Wed Mar 21 04:41:16 UTC 2018

parent 89ebcb96
Hide whitespace changes
Inline Side-by-side
Showing with 73 additions and 21 deletions
src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
View file @ 86aacfb5
...@@ -1925,6 +1925,78 @@ This is the ratio of static pressure error to dynamic pressure generated by a wi ...@@ -1925,6 +1925,78 @@ This is the ratio of static pressure error to dynamic pressure generated by a wi
<boolean /> <boolean />
<scope>modules/fw_att_control</scope> <scope>modules/fw_att_control</scope>
</parameter> </parameter>
<parameter default="0.0" name="FW_DTRIM_P_FLPS" type="FLOAT">
<short_desc>Pitch trim increment for flaps configuration</short_desc>
<long_desc>This increment is added to the pitch trim whenever flaps are fully deployed.</long_desc>
<min>-0.25</min>
<max>0.25</max>
<decimal>2</decimal>
<increment>0.01</increment>
<scope>modules/fw_att_control</scope>
</parameter>
<parameter default="0.0" name="FW_DTRIM_P_VMAX" type="FLOAT">
<short_desc>Pitch trim increment at maximum airspeed</short_desc>
<long_desc>This increment is added to TRIM_PITCH when airspeed is FW_AIRSP_MAX.</long_desc>
<min>-0.25</min>
<max>0.25</max>
<decimal>2</decimal>
<increment>0.01</increment>
<scope>modules/fw_att_control</scope>
</parameter>
<parameter default="0.0" name="FW_DTRIM_P_VMIN" type="FLOAT">
<short_desc>Pitch trim increment at minimum airspeed</short_desc>
<long_desc>This increment is added to TRIM_PITCH when airspeed is FW_AIRSPD_MIN.</long_desc>
<min>-0.25</min>
<max>0.25</max>
<decimal>2</decimal>
<increment>0.01</increment>
<scope>modules/fw_att_control</scope>
</parameter>
<parameter default="0.0" name="FW_DTRIM_R_FLPS" type="FLOAT">
<short_desc>Roll trim increment for flaps configuration</short_desc>
<long_desc>This increment is added to TRIM_ROLL whenever flaps are fully deployed.</long_desc>
<min>-0.25</min>
<max>0.25</max>
<decimal>2</decimal>
<increment>0.01</increment>
<scope>modules/fw_att_control</scope>
</parameter>
<parameter default="0.0" name="FW_DTRIM_R_VMAX" type="FLOAT">
<short_desc>Roll trim increment at maximum airspeed</short_desc>
<long_desc>This increment is added to TRIM_ROLL when airspeed is FW_AIRSP_MAX.</long_desc>
<min>-0.25</min>
<max>0.25</max>
<decimal>2</decimal>
<increment>0.01</increment>
<scope>modules/fw_att_control</scope>
</parameter>
<parameter default="0.0" name="FW_DTRIM_R_VMIN" type="FLOAT">
<short_desc>Roll trim increment at minimum airspeed</short_desc>
<long_desc>This increment is added to TRIM_ROLL when airspeed is FW_AIRSPD_MIN.</long_desc>
<min>-0.25</min>
<max>0.25</max>
<decimal>2</decimal>
<increment>0.01</increment>
<scope>modules/fw_att_control</scope>
</parameter>
<parameter default="0.0" name="FW_DTRIM_Y_VMAX" type="FLOAT">
<short_desc>Yaw trim increment at maximum airspeed</short_desc>
<long_desc>This increment is added to TRIM_YAW when airspeed is FW_AIRSP_MAX.</long_desc>
<min>-0.25</min>
<max>0.25</max>
<decimal>2</decimal>
<increment>0.01</increment>
<scope>modules/fw_att_control</scope>
</parameter>
<parameter default="0.0" name="FW_DTRIM_Y_VMIN" type="FLOAT">
<short_desc>Yaw trim increment at minimum airspeed</short_desc>
<long_desc>This increment is added to TRIM_YAW when airspeed is FW_AIRSPD_MIN.</long_desc>
<min>-0.25</min>
<max>0.25</max>
<decimal>2</decimal>
<increment>0.01</increment>
<scope>modules/fw_att_control</scope>
</parameter>
<parameter default="0.0" name="FW_FLAPERON_SCL" type="FLOAT"> <parameter default="0.0" name="FW_FLAPERON_SCL" type="FLOAT">
<short_desc>Scale factor for flaperons</short_desc> <short_desc>Scale factor for flaperons</short_desc>
<min>0.0</min> <min>0.0</min>
...@@ -2406,7 +2478,7 @@ Set to 0 to disable heading hold</short_desc> ...@@ -2406,7 +2478,7 @@ Set to 0 to disable heading hold</short_desc>
<short_desc>Scale throttle by pressure change</short_desc> <short_desc>Scale throttle by pressure change</short_desc>
<long_desc>Automatically adjust throttle to account for decreased air density at higher altitudes. Start with a scale factor of 1.0 and adjust for different propulsion systems. When flying without airspeed sensor this will help to keep a constant performance over large altitude ranges. The default value of 0 will disable scaling.</long_desc> <long_desc>Automatically adjust throttle to account for decreased air density at higher altitudes. Start with a scale factor of 1.0 and adjust for different propulsion systems. When flying without airspeed sensor this will help to keep a constant performance over large altitude ranges. The default value of 0 will disable scaling.</long_desc>
<min>0.0</min> <min>0.0</min>
<max>2.0</max> <max>10.0</max>
<decimal>1</decimal> <decimal>1</decimal>
<increment>0.1</increment> <increment>0.1</increment>
<scope>modules/fw_pos_control_l1</scope> <scope>modules/fw_pos_control_l1</scope>
...@@ -4251,16 +4323,6 @@ default 1.5 turns per second</short_desc> ...@@ -4251,16 +4323,6 @@ default 1.5 turns per second</short_desc>
<increment>0.1</increment> <increment>0.1</increment>
<scope>modules/mc_att_control</scope> <scope>modules/mc_att_control</scope>
</parameter> </parameter>
<parameter default="0.2" name="MC_PITCH_TC" type="FLOAT">
<short_desc>Pitch time constant</short_desc>
<long_desc>Reduce if the system is too twitchy, increase if the response is too slow and sluggish.</long_desc>
<min>0.15</min>
<max>0.25</max>
<unit>s</unit>
<decimal>2</decimal>
<increment>0.01</increment>
<scope>modules/mc_att_control</scope>
</parameter>
<parameter default="0.30" name="MC_PR_INT_LIM" type="FLOAT"> <parameter default="0.30" name="MC_PR_INT_LIM" type="FLOAT">
<short_desc>Pitch rate integrator limit</short_desc> <short_desc>Pitch rate integrator limit</short_desc>
<long_desc>Pitch rate integrator limit. Can be set to increase the amount of integrator available to counteract disturbances or reduced to improve settling time after large pitch moment trim changes.</long_desc> <long_desc>Pitch rate integrator limit. Can be set to increase the amount of integrator available to counteract disturbances or reduced to improve settling time after large pitch moment trim changes.</long_desc>
...@@ -4331,16 +4393,6 @@ default 1.5 turns per second</short_desc> ...@@ -4331,16 +4393,6 @@ default 1.5 turns per second</short_desc>
<increment>0.1</increment> <increment>0.1</increment>
<scope>modules/mc_att_control</scope> <scope>modules/mc_att_control</scope>
</parameter> </parameter>
<parameter default="0.2" name="MC_ROLL_TC" type="FLOAT">
<short_desc>Roll time constant</short_desc>
<long_desc>Reduce if the system is too twitchy, increase if the response is too slow and sluggish.</long_desc>
<min>0.15</min>
<max>0.25</max>
<unit>s</unit>
<decimal>2</decimal>
<increment>0.01</increment>
<scope>modules/mc_att_control</scope>
</parameter>
<parameter default="0.30" name="MC_RR_INT_LIM" type="FLOAT"> <parameter default="0.30" name="MC_RR_INT_LIM" type="FLOAT">
<short_desc>Roll rate integrator limit</short_desc> <short_desc>Roll rate integrator limit</short_desc>
<long_desc>Roll rate integrator limit. Can be set to increase the amount of integrator available to counteract disturbances or reduced to improve settling time after large roll moment trim changes.</long_desc> <long_desc>Roll rate integrator limit. Can be set to increase the amount of integrator available to counteract disturbances or reduced to improve settling time after large roll moment trim changes.</long_desc>
......
Markdown is supported
0% or
You are about to add 0 people to the discussion. Proceed with caution.
Finish editing this message first!
Please register or to comment