<long_desc>Turns the automatic airspeed scale (scale from IAS to CAS/EAS) on or off. It is recommended level (keeping altitude) while performing the estimation. Set to 1 to start estimation (best when already flying). Set to 0 to end scale estimation. The estimated scale is then saved in the ARSP_ARSP_SCALE parameter.</long_desc>
@ -225,7 +223,6 @@ Set to 2 to use heading from motion capture</short_desc>
@@ -225,7 +223,6 @@ Set to 2 to use heading from motion capture</short_desc>
@ -413,7 +410,6 @@ Set to 2 to use heading from motion capture</short_desc>
@@ -413,7 +410,6 @@ Set to 2 to use heading from motion capture</short_desc>
@ -595,7 +591,6 @@ Set to 2 to use heading from motion capture</short_desc>
@@ -595,7 +591,6 @@ Set to 2 to use heading from motion capture</short_desc>
<short_desc>Set avoidance system bootup timeout</short_desc>
@ -1063,7 +1055,6 @@ See COM_OBL_ACT and COM_OBL_RC_ACT to configure action</short_desc>
@@ -1063,7 +1055,6 @@ See COM_OBL_ACT and COM_OBL_RC_ACT to configure action</short_desc>
<short_desc>Enable RC stick override of auto modes</short_desc>
<long_desc>When an auto mode is active (except a critical battery reaction) moving the RC sticks gives control back to the pilot in manual position mode immediately. Only has an effect on multicopters and VTOLS in multicopter mode.</long_desc>
@ -1184,7 +1175,6 @@ See COM_OBL_ACT and COM_OBL_RC_ACT to configure action</short_desc>
@@ -1184,7 +1175,6 @@ See COM_OBL_ACT and COM_OBL_RC_ACT to configure action</short_desc>
@ -1462,7 +1452,6 @@ Sets the number of standard deviations used by the innovation consistency test</
@@ -1462,7 +1452,6 @@ Sets the number of standard deviations used by the innovation consistency test</
<short_desc>Whether to set the external vision observation noise from the parameter or from vision message</short_desc>
<long_desc>If set to true the observation noise is set from the parameters directly, if set to false the measurement noise is taken from the vision message and the parameter are used as a lower bound.</long_desc>
<short_desc>X position of VI sensor focal point in body frame</short_desc>
@ -1482,7 +1471,6 @@ Sets the number of standard deviations used by the innovation consistency test</
@@ -1482,7 +1471,6 @@ Sets the number of standard deviations used by the innovation consistency test</
<short_desc>Boolean determining if synthetic sideslip measurements should fused</short_desc>
<long_desc>A value of 1 indicates that fusion is active Both sideslip fusion and airspeed fusion must be active for the EKF to continue navigating after loss of GPS. Use EKF2_ARSP_THR to activate airspeed fusion.</long_desc>
@ -2064,13 +2052,11 @@ This is the ratio of static pressure error to dynamic pressure generated by a wi
@@ -2064,13 +2052,11 @@ This is the ratio of static pressure error to dynamic pressure generated by a wi
<long_desc>Enable/disable event task for RC Loss. When enabled, an alarm tune will be played via buzzer or ESCs, if supported. The alarm will sound after a disarm, if the vehicle was previously armed and only if the vehicle had RC signal at some point. Particularly useful for locating crashed drones without a GPS sensor.</long_desc>
<long_desc>Enable/disable event task for displaying the vehicle status using arm-mounted LEDs. When enabled and if the vehicle supports it, LEDs will flash indicating various vehicle status changes. Currently PX4 has not implemented any specific status events. -</long_desc>
<boolean/>
<reboot_required>true</reboot_required>
</parameter>
</group>
@ -2107,7 +2093,6 @@ This is the ratio of static pressure error to dynamic pressure generated by a wi
@@ -2107,7 +2093,6 @@ This is the ratio of static pressure error to dynamic pressure generated by a wi
<short_desc>Whether to scale throttle by battery power level</short_desc>
<long_desc>This compensates for voltage drop of the battery over time by attempting to normalize performance across the operating range of the battery. The fixed wing should constantly behave as if it was fully charged with reduced max thrust at lower battery percentages. i.e. if cruise speed is at 0.5 throttle at 100% battery, it will still be 0.5 at 60% battery.</long_desc>
<short_desc>Pitch trim increment for flaps configuration</short_desc>
@ -2435,7 +2420,6 @@ This is the ratio of static pressure error to dynamic pressure generated by a wi
@@ -2435,7 +2420,6 @@ This is the ratio of static pressure error to dynamic pressure generated by a wi
@ -2545,7 +2529,6 @@ This is the ratio of static pressure error to dynamic pressure generated by a wi
@@ -2545,7 +2529,6 @@ This is the ratio of static pressure error to dynamic pressure generated by a wi
<long_desc>When disabled, the landing configuration (flaps, landing airspeed, etc.) is only activated on the final approach to landing. When enabled, it is already activated when entering the final loiter-down (loiter-to-alt) waypoint before the landing approach. This shifts the (often large) altitude and airspeed errors caused by the configuration change away from the ground such that these are not so critical. It also gives the controller enough time to adapt to the new configuration such that the landing approach starts with a cleaner initial state.</long_desc>
@ -3627,7 +3608,6 @@ Used to calculate increased terrain random walk nosie due to movement</short_des
@@ -3627,7 +3608,6 @@ Used to calculate increased terrain random walk nosie due to movement</short_des
<short_desc>Enable MAVLink Message forwarding for instance 0</short_desc>
<long_desc>If enabled, forward incoming MAVLink messages to other MAVLink ports if the message is either broadcast or the target is not the autopilot. This allows for example a GCS to talk to a camera that is connected to the autopilot via MAVLink (on a different link than the GCS).</long_desc>
@ -3671,7 +3651,6 @@ Used to calculate increased terrain random walk nosie due to movement</short_des
@@ -3671,7 +3651,6 @@ Used to calculate increased terrain random walk nosie due to movement</short_des
<short_desc>Enable MAVLink Message forwarding for instance 1</short_desc>
<long_desc>If enabled, forward incoming MAVLink messages to other MAVLink ports if the message is either broadcast or the target is not the autopilot. This allows for example a GCS to talk to a camera that is connected to the autopilot via MAVLink (on a different link than the GCS).</long_desc>
@ -3715,7 +3694,6 @@ Used to calculate increased terrain random walk nosie due to movement</short_des
@@ -3715,7 +3694,6 @@ Used to calculate increased terrain random walk nosie due to movement</short_des
<short_desc>Enable MAVLink Message forwarding for instance 2</short_desc>
<long_desc>If enabled, forward incoming MAVLink messages to other MAVLink ports if the message is either broadcast or the target is not the autopilot. This allows for example a GCS to talk to a camera that is connected to the autopilot via MAVLink (on a different link than the GCS).</long_desc>
@ -3758,22 +3736,18 @@ Used to calculate increased terrain random walk nosie due to movement</short_des
@@ -3758,22 +3736,18 @@ Used to calculate increased terrain random walk nosie due to movement</short_des
<long_desc>The mavlink hearbeat message will not be forwarded if this parameter is set to 'disabled'. The main reason for disabling heartbeats to be forwarded is because they confuse dronekit.</long_desc>
<long_desc>If set, it gets the data from 'vehicle_visual_odometry' instead of 'vehicle_odometry' serving as a loopback of the received ODOMETRY messages on the Mavlink receiver.</long_desc>
@ -3833,13 +3807,11 @@ Used to calculate increased terrain random walk nosie due to movement</short_des
@@ -3833,13 +3807,11 @@ Used to calculate increased terrain random walk nosie due to movement</short_des
<short_desc>Test mode (Identify) of MKBLCTRL Driver</short_desc>
<boolean/>
</parameter>
</group>
<groupname="MPU9x50 Configuration">
@ -3882,7 +3854,6 @@ Used to calculate increased terrain random walk nosie due to movement</short_des
@@ -3882,7 +3854,6 @@ Used to calculate increased terrain random walk nosie due to movement</short_des
<short_desc>Action after TAKEOFF has been accepted</short_desc>
@ -3951,7 +3922,6 @@ Used to calculate increased terrain random walk nosie due to movement</short_des
@@ -3951,7 +3922,6 @@ Used to calculate increased terrain random walk nosie due to movement</short_des
<short_desc>Max yaw error in degrees needed for waypoint heading acceptance</short_desc>
@ -4007,7 +3977,6 @@ Used to calculate increased terrain random walk nosie due to movement</short_des
@@ -4007,7 +3977,6 @@ Used to calculate increased terrain random walk nosie due to movement</short_des
<short_desc>FW Altitude Acceptance Radius before a landing</short_desc>
@ -4099,7 +4068,6 @@ Used to calculate increased terrain random walk nosie due to movement</short_des
@@ -4099,7 +4068,6 @@ Used to calculate increased terrain random walk nosie due to movement</short_des
<short_desc>Battery power level scaler</short_desc>
<long_desc>This compensates for voltage drop of the battery over time by attempting to normalize performance across the operating range of the battery. The copter should constantly behave as if it was fully charged with reduced max acceleration at lower battery percentages. i.e. if hover is at 0.5 throttle at 100% battery, it will still be 0.5 at 60% battery.</long_desc>
<short_desc>Angle left/right from the commanded setpoint by which the collision prevention algorithm can choose to change the setpoint direction</short_desc>
@ -4915,7 +4881,6 @@ the setpoint will be capped to MPC_XY_VEL_MAX</short_desc>
@@ -4915,7 +4881,6 @@ the setpoint will be capped to MPC_XY_VEL_MAX</short_desc>
<short_desc>Minimum roll angle setpoint for weathervane controller to demand a yaw-rate</short_desc>
@ -5240,42 +5205,34 @@ the setpoint will be capped to MPC_XY_VEL_MAX</short_desc>
@@ -5240,42 +5205,34 @@ the setpoint will be capped to MPC_XY_VEL_MAX</short_desc>
<short_desc>Invert direction of auxiliary output channel 1</short_desc>
<long_desc>Enable to invert the channel. Warning: Use this parameter when connected to a servo only. For a brushless motor, invert manually two phases to reverse the direction.</long_desc>
<short_desc>Invert direction of auxiliary output channel 2</short_desc>
<long_desc>Enable to invert the channel. Warning: Use this parameter when connected to a servo only. For a brushless motor, invert manually two phases to reverse the direction.</long_desc>
<short_desc>Invert direction of auxiliary output channel 3</short_desc>
<long_desc>Enable to invert the channel. Warning: Use this parameter when connected to a servo only. For a brushless motor, invert manually two phases to reverse the direction.</long_desc>
<short_desc>Invert direction of auxiliary output channel 4</short_desc>
<long_desc>Enable to invert the channel. Warning: Use this parameter when connected to a servo only. For a brushless motor, invert manually two phases to reverse the direction.</long_desc>
<short_desc>Invert direction of auxiliary output channel 5</short_desc>
<long_desc>Enable to invert the channel. Warning: Use this parameter when connected to a servo only. For a brushless motor, invert manually two phases to reverse the direction.</long_desc>
<short_desc>Invert direction of auxiliary output channel 6</short_desc>
<long_desc>Enable to invert the channel. Warning: Use this parameter when connected to a servo only. For a brushless motor, invert manually two phases to reverse the direction.</long_desc>
<short_desc>Invert direction of auxiliary output channel 7</short_desc>
<long_desc>Enable to invert the channel. Warning: Use this parameter when connected to a servo only. For a brushless motor, invert manually two phases to reverse the direction.</long_desc>
<short_desc>Invert direction of auxiliary output channel 8</short_desc>
<long_desc>Enable to invert the channel. Warning: Use this parameter when connected to a servo only. For a brushless motor, invert manually two phases to reverse the direction.</long_desc>
<short_desc>Trim value for auxiliary output channel 1</short_desc>
@ -5600,42 +5557,34 @@ the setpoint will be capped to MPC_XY_VEL_MAX</short_desc>
@@ -5600,42 +5557,34 @@ the setpoint will be capped to MPC_XY_VEL_MAX</short_desc>
<short_desc>Invert direction of main output channel 1</short_desc>
<long_desc>Enable to invert the channel. Warning: Use this parameter when connected to a servo only. For a brushless motor, invert manually two phases to reverse the direction.</long_desc>
<short_desc>Invert direction of main output channel 2</short_desc>
<long_desc>Enable to invert the channel. Warning: Use this parameter when connected to a servo only. For a brushless motor, invert manually two phases to reverse the direction.</long_desc>
<short_desc>Invert direction of main output channel 3</short_desc>
<long_desc>Enable to invert the channel. Warning: Use this parameter when connected to a servo only. For a brushless motor, invert manually two phases to reverse the direction.</long_desc>
<short_desc>Invert direction of main output channel 4</short_desc>
<long_desc>Enable to invert the channel. Warning: Use this parameter when connected to a servo only. For a brushless motor, invert manually two phases to reverse the direction.</long_desc>
<short_desc>Invert direction of main output channel 5</short_desc>
<long_desc>Enable to invert the channel. Warning: Use this parameter when connected to a servo only. For a brushless motor, invert manually two phases to reverse the direction.</long_desc>
<short_desc>Invert direction of main output channel 6</short_desc>
<long_desc>Enable to invert the channel. Warning: Use this parameter when connected to a servo only. For a brushless motor, invert manually two phases to reverse the direction.</long_desc>
<short_desc>Invert direction of main output channel 7</short_desc>
<long_desc>Enable to invert the channel. Warning: Use this parameter when connected to a servo only. For a brushless motor, invert manually two phases to reverse the direction.</long_desc>
<short_desc>Invert direction of main output channel 8</short_desc>
<long_desc>Enable to invert the channel. Warning: Use this parameter when connected to a servo only. For a brushless motor, invert manually two phases to reverse the direction.</long_desc>
<short_desc>Trim value for main output channel 1</short_desc>
@ -5720,7 +5669,6 @@ the setpoint will be capped to MPC_XY_VEL_MAX</short_desc>
@@ -5720,7 +5669,6 @@ the setpoint will be capped to MPC_XY_VEL_MAX</short_desc>
<short_desc>Thrust to motor control signal model parameter</short_desc>
@ -5774,7 +5722,6 @@ the setpoint will be capped to MPC_XY_VEL_MAX</short_desc>
@@ -5774,7 +5722,6 @@ the setpoint will be capped to MPC_XY_VEL_MAX</short_desc>
<long_desc>If enabled, update the bootloader on the next boot. WARNING: do not cut the power during an update process, otherwise you will have to recover using some alternative method (e.g. JTAG). Instructions: - Insert an SD card - Enable this parameter - Reboot the board (plug the power or send a reboot command) - Wait until the board comes back up (or at least 2 minutes) - If it does not come back, check the file bootlog.txt on the SD card</long_desc>
<short_desc>Control if the vehicle has a barometer</short_desc>
<long_desc>Disable this if the board has no barometer, such as some of the the Omnibus F4 SD variants. If disabled, the preflight checks will not check for the presence of a barometer.</long_desc>
<short_desc>Control if the vehicle has a magnetometer</short_desc>
<long_desc>Disable this if the board has no magnetometer, such as the Omnibus F4 SD. If disabled, the preflight checks will not check for the presence of a magnetometer.</long_desc>
<boolean/>
<reboot_required>true</reboot_required>
</parameter>
<parameterdefault="0"name="SYS_HITL"type="INT32">
@ -9745,14 +9672,12 @@ is less than 50% of this value</short_desc>
@@ -9745,14 +9672,12 @@ is less than 50% of this value</short_desc>
<short_desc>Permanent stabilization in fw mode</short_desc>
<long_desc>If set to one this parameter will cause permanent attitude stabilization in fw mode. This parameter has been introduced for pure convenience sake.</long_desc>
PX4BuildBot
6 years ago