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Valentin Platzgummer
qgroundcontrol
Commits
b2d58a51
Commit
b2d58a51
authored
Feb 08, 2018
by
PX4 Jenkins
Committed by
Daniel Agar
Feb 08, 2018
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Update PX4 Firmware metadata Thu Feb 8 23:37:07 EST 2018
parent
4c339fa5
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PX4ParameterFactMetaData.xml
src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
+19
-13
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src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
View file @
b2d58a51
...
...
@@ -2483,7 +2483,7 @@ Set to 0 to disable heading hold</short_desc>
<parameter
default=
"0"
name=
"LAUN_ALL_ON"
type=
"INT32"
>
<short_desc>
Launch detection
</short_desc>
<boolean
/>
<scope>
lib
/launchdetection
</scope>
<scope>
modules/fw_pos_control_l1
/launchdetection
</scope>
</parameter>
<parameter
default=
"30.0"
name=
"LAUN_CAT_A"
type=
"FLOAT"
>
<short_desc>
Catapult accelerometer threshold
</short_desc>
...
...
@@ -2492,7 +2492,7 @@ Set to 0 to disable heading hold</short_desc>
<unit>
m/s/s
</unit>
<decimal>
1
</decimal>
<increment>
0.5
</increment>
<scope>
lib
/launchdetection
</scope>
<scope>
modules/fw_pos_control_l1
/launchdetection
</scope>
</parameter>
<parameter
default=
"0.0"
name=
"LAUN_CAT_MDEL"
type=
"FLOAT"
>
<short_desc>
Motor delay
</short_desc>
...
...
@@ -2502,7 +2502,7 @@ Set to 0 to disable heading hold</short_desc>
<unit>
s
</unit>
<decimal>
1
</decimal>
<increment>
0.5
</increment>
<scope>
lib
/launchdetection
</scope>
<scope>
modules/fw_pos_control_l1
/launchdetection
</scope>
</parameter>
<parameter
default=
"30.0"
name=
"LAUN_CAT_PMAX"
type=
"FLOAT"
>
<short_desc>
Maximum pitch before the throttle is powered up (during motor delay phase)
</short_desc>
...
...
@@ -2512,7 +2512,7 @@ Set to 0 to disable heading hold</short_desc>
<unit>
deg
</unit>
<decimal>
1
</decimal>
<increment>
0.5
</increment>
<scope>
lib
/launchdetection
</scope>
<scope>
modules/fw_pos_control_l1
/launchdetection
</scope>
</parameter>
<parameter
default=
"0.05"
name=
"LAUN_CAT_T"
type=
"FLOAT"
>
<short_desc>
Catapult time threshold
</short_desc>
...
...
@@ -2522,7 +2522,7 @@ Set to 0 to disable heading hold</short_desc>
<unit>
s
</unit>
<decimal>
2
</decimal>
<increment>
0.05
</increment>
<scope>
lib
/launchdetection
</scope>
<scope>
modules/fw_pos_control_l1
/launchdetection
</scope>
</parameter>
</group>
<group
name=
"FW TECS"
>
...
...
@@ -7267,14 +7267,14 @@ FW_AIRSPD_MIN * RWTO_AIRSPD_SCL</short_desc>
<unit>
norm
</unit>
<decimal>
2
</decimal>
<increment>
0.01
</increment>
<scope>
lib
/runway_takeoff
</scope>
<scope>
modules/fw_pos_control_l1
/runway_takeoff
</scope>
</parameter>
<parameter
default=
"0"
name=
"RWTO_HDG"
type=
"INT32"
>
<short_desc>
Specifies which heading should be held during runnway takeoff
</short_desc>
<long_desc>
0: airframe heading, 1: heading towards takeoff waypoint
</long_desc>
<min>
0
</min>
<max>
1
</max>
<scope>
lib
/runway_takeoff
</scope>
<scope>
modules/fw_pos_control_l1
/runway_takeoff
</scope>
<values>
<value
code=
"0"
>
Airframe
</value>
<value
code=
"1"
>
Waypoint
</value>
...
...
@@ -7289,7 +7289,7 @@ pitch of 10 degrees during takeoff, so this must be larger if set</short_desc>
<unit>
deg
</unit>
<decimal>
1
</decimal>
<increment>
0.5
</increment>
<scope>
lib
/runway_takeoff
</scope>
<scope>
modules/fw_pos_control_l1
/runway_takeoff
</scope>
</parameter>
<parameter
default=
"25.0"
name=
"RWTO_MAX_ROLL"
type=
"FLOAT"
>
<short_desc>
Max roll during climbout.
...
...
@@ -7300,7 +7300,7 @@ navigation before we're on a safe height</short_desc>
<unit>
deg
</unit>
<decimal>
1
</decimal>
<increment>
0.5
</increment>
<scope>
lib
/runway_takeoff
</scope>
<scope>
modules/fw_pos_control_l1
/runway_takeoff
</scope>
</parameter>
<parameter
default=
"1.0"
name=
"RWTO_MAX_THR"
type=
"FLOAT"
>
<short_desc>
Max throttle during runway takeoff.
...
...
@@ -7310,7 +7310,7 @@ navigation before we're on a safe height</short_desc>
<unit>
norm
</unit>
<decimal>
2
</decimal>
<increment>
0.01
</increment>
<scope>
lib
/runway_takeoff
</scope>
<scope>
modules/fw_pos_control_l1
/runway_takeoff
</scope>
</parameter>
<parameter
default=
"5.0"
name=
"RWTO_NAV_ALT"
type=
"FLOAT"
>
<short_desc>
Altitude AGL at which we have enough ground clearance to allow some roll.
...
...
@@ -7322,7 +7322,7 @@ FW_CLMBOUT_DIFF if FW_CLMBOUT_DIFF > 0</short_desc>
<unit>
m
</unit>
<decimal>
1
</decimal>
<increment>
1
</increment>
<scope>
lib
/runway_takeoff
</scope>
<scope>
modules/fw_pos_control_l1
/runway_takeoff
</scope>
</parameter>
<parameter
default=
"0.0"
name=
"RWTO_PSP"
type=
"FLOAT"
>
<short_desc>
Pitch setpoint during taxi / before takeoff airspeed is reached.
...
...
@@ -7334,12 +7334,12 @@ to takeoff is reached</short_desc>
<unit>
deg
</unit>
<decimal>
1
</decimal>
<increment>
0.5
</increment>
<scope>
lib
/runway_takeoff
</scope>
<scope>
modules/fw_pos_control_l1
/runway_takeoff
</scope>
</parameter>
<parameter
default=
"0"
name=
"RWTO_TKOFF"
type=
"INT32"
>
<short_desc>
Runway takeoff with landing gear
</short_desc>
<boolean
/>
<scope>
lib
/runway_takeoff
</scope>
<scope>
modules/fw_pos_control_l1
/runway_takeoff
</scope>
</parameter>
</group>
<group
name=
"SD Logging"
>
...
...
@@ -8076,6 +8076,12 @@ This is used for gathering replay logs for the ekf2 module</short_desc>
<unit>
deg
</unit>
<scope>
modules/sensors
</scope>
</parameter>
<parameter
default=
"0"
name=
"SENS_EN_LEDDAR1"
type=
"INT32"
>
<short_desc>
LeddarOne rangefinder
</short_desc>
<boolean
/>
<reboot_required>
true
</reboot_required>
<scope>
modules/sensors
</scope>
</parameter>
<parameter
default=
"0"
name=
"SENS_EN_LL40LS"
type=
"INT32"
>
<short_desc>
Lidar-Lite (LL40LS)
</short_desc>
<min>
0
</min>
...
...
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