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Commit aeb0e8a7 authored by PX4 Jenkins's avatar PX4 Jenkins
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Update PX4 Firmware metadata Mon Nov 27 04:41:42 UTC 2017

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src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
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......@@ -137,57 +137,6 @@
<min>0</min>
</parameter>
</group>
<group name="Attitude EKF estimator">
<parameter default="0.0018" name="ATT_J11" type="FLOAT">
<short_desc>Moment of inertia matrix diagonal entry (1, 1)</short_desc>
<unit>kg*m^2</unit>
<scope>examples/attitude_estimator_ekf</scope>
</parameter>
<parameter default="0.0018" name="ATT_J22" type="FLOAT">
<short_desc>Moment of inertia matrix diagonal entry (2, 2)</short_desc>
<unit>kg*m^2</unit>
<scope>examples/attitude_estimator_ekf</scope>
</parameter>
<parameter default="0.0037" name="ATT_J33" type="FLOAT">
<short_desc>Moment of inertia matrix diagonal entry (3, 3)</short_desc>
<unit>kg*m^2</unit>
<scope>examples/attitude_estimator_ekf</scope>
</parameter>
<parameter default="0" name="ATT_J_EN" type="INT32">
<short_desc>Moment of inertia enabled in estimator</short_desc>
<long_desc>If set to != 0 the moment of inertia will be used in the estimator</long_desc>
<boolean />
<scope>examples/attitude_estimator_ekf</scope>
</parameter>
<parameter default="1e-4" name="EKF_ATT_V3_Q0" type="FLOAT">
<short_desc>Body angular rate process noise</short_desc>
<scope>examples/attitude_estimator_ekf</scope>
</parameter>
<parameter default="0.08" name="EKF_ATT_V3_Q1" type="FLOAT">
<short_desc>Body angular acceleration process noise</short_desc>
<scope>examples/attitude_estimator_ekf</scope>
</parameter>
<parameter default="0.009" name="EKF_ATT_V3_Q2" type="FLOAT">
<short_desc>Acceleration process noise</short_desc>
<scope>examples/attitude_estimator_ekf</scope>
</parameter>
<parameter default="0.005" name="EKF_ATT_V3_Q3" type="FLOAT">
<short_desc>Magnet field vector process noise</short_desc>
<scope>examples/attitude_estimator_ekf</scope>
</parameter>
<parameter default="0.0008" name="EKF_ATT_V4_R0" type="FLOAT">
<short_desc>Gyro measurement noise</short_desc>
<scope>examples/attitude_estimator_ekf</scope>
</parameter>
<parameter default="10000.0" name="EKF_ATT_V4_R1" type="FLOAT">
<short_desc>Accel measurement noise</short_desc>
<scope>examples/attitude_estimator_ekf</scope>
</parameter>
<parameter default="100.0" name="EKF_ATT_V4_R2" type="FLOAT">
<short_desc>Mag measurement noise</short_desc>
<scope>examples/attitude_estimator_ekf</scope>
</parameter>
</group>
<group name="Attitude Q estimator">
<parameter default="1" name="ATT_ACC_COMP" type="INT32">
<short_desc>Acceleration compensation based on GPS
......@@ -4367,135 +4316,6 @@ default 1.5 turns per second</short_desc>
<increment>0.01</increment>
<scope>modules/mc_att_control</scope>
</parameter>
<parameter default="35.0" name="MPP_MAN_P_MAX" type="FLOAT">
<short_desc>Max manual pitch</short_desc>
<min>0.0</min>
<max>90.0</max>
<unit>deg</unit>
<scope>examples/mc_pos_control_multiplatform</scope>
</parameter>
<parameter default="35.0" name="MPP_MAN_R_MAX" type="FLOAT">
<short_desc>Max manual roll</short_desc>
<min>0.0</min>
<max>90.0</max>
<unit>deg</unit>
<scope>examples/mc_pos_control_multiplatform</scope>
</parameter>
<parameter default="120.0" name="MPP_MAN_Y_MAX" type="FLOAT">
<short_desc>Max manual yaw rate</short_desc>
<min>0.0</min>
<unit>deg/s</unit>
<scope>examples/mc_pos_control_multiplatform</scope>
</parameter>
<parameter default="35.0" name="MP_ACRO_P_MAX" type="FLOAT">
<short_desc>Max acro pitch rate</short_desc>
<min>0.0</min>
<max>360.0</max>
<unit>deg/s</unit>
<scope>examples/mc_att_control_multiplatform</scope>
</parameter>
<parameter default="35.0" name="MP_ACRO_R_MAX" type="FLOAT">
<short_desc>Max acro roll rate</short_desc>
<min>0.0</min>
<max>360.0</max>
<unit>deg/s</unit>
<scope>examples/mc_att_control_multiplatform</scope>
</parameter>
<parameter default="120.0" name="MP_ACRO_Y_MAX" type="FLOAT">
<short_desc>Max acro yaw rate</short_desc>
<min>0.0</min>
<unit>deg/s</unit>
<scope>examples/mc_att_control_multiplatform</scope>
</parameter>
<parameter default="0.002" name="MP_PITCHRATE_D" type="FLOAT">
<short_desc>Pitch rate D gain</short_desc>
<long_desc>Pitch rate differential gain. Small values help reduce fast oscillations. If value is too big oscillations will appear again.</long_desc>
<min>0.0</min>
<scope>examples/mc_att_control_multiplatform</scope>
</parameter>
<parameter default="0.0" name="MP_PITCHRATE_I" type="FLOAT">
<short_desc>Pitch rate I gain</short_desc>
<long_desc>Pitch rate integral gain. Can be set to compensate static thrust difference or gravity center offset.</long_desc>
<min>0.0</min>
<scope>examples/mc_att_control_multiplatform</scope>
</parameter>
<parameter default="0.1" name="MP_PITCHRATE_P" type="FLOAT">
<short_desc>Pitch rate P gain</short_desc>
<long_desc>Pitch rate proportional gain, i.e. control output for angular speed error 1 rad/s.</long_desc>
<min>0.0</min>
<scope>examples/mc_att_control_multiplatform</scope>
</parameter>
<parameter default="6.0" name="MP_PITCH_P" type="FLOAT">
<short_desc>Pitch P gain</short_desc>
<long_desc>Pitch proportional gain, i.e. desired angular speed in rad/s for error 1 rad.</long_desc>
<min>0.0</min>
<unit>1/s</unit>
<scope>examples/mc_att_control_multiplatform</scope>
</parameter>
<parameter default="0.002" name="MP_ROLLRATE_D" type="FLOAT">
<short_desc>Roll rate D gain</short_desc>
<long_desc>Roll rate differential gain. Small values help reduce fast oscillations. If value is too big oscillations will appear again.</long_desc>
<min>0.0</min>
<scope>examples/mc_att_control_multiplatform</scope>
</parameter>
<parameter default="0.0" name="MP_ROLLRATE_I" type="FLOAT">
<short_desc>Roll rate I gain</short_desc>
<long_desc>Roll rate integral gain. Can be set to compensate static thrust difference or gravity center offset.</long_desc>
<min>0.0</min>
<scope>examples/mc_att_control_multiplatform</scope>
</parameter>
<parameter default="0.1" name="MP_ROLLRATE_P" type="FLOAT">
<short_desc>Roll rate P gain</short_desc>
<long_desc>Roll rate proportional gain, i.e. control output for angular speed error 1 rad/s.</long_desc>
<min>0.0</min>
<scope>examples/mc_att_control_multiplatform</scope>
</parameter>
<parameter default="6.0" name="MP_ROLL_P" type="FLOAT">
<short_desc>Roll P gain</short_desc>
<long_desc>Roll proportional gain, i.e. desired angular speed in rad/s for error 1 rad.</long_desc>
<min>0.0</min>
<scope>examples/mc_att_control_multiplatform</scope>
</parameter>
<parameter default="0.0" name="MP_YAWRATE_D" type="FLOAT">
<short_desc>Yaw rate D gain</short_desc>
<long_desc>Yaw rate differential gain. Small values help reduce fast oscillations. If value is too big oscillations will appear again.</long_desc>
<min>0.0</min>
<scope>examples/mc_att_control_multiplatform</scope>
</parameter>
<parameter default="0.0" name="MP_YAWRATE_I" type="FLOAT">
<short_desc>Yaw rate I gain</short_desc>
<long_desc>Yaw rate integral gain. Can be set to compensate static thrust difference or gravity center offset.</long_desc>
<min>0.0</min>
<scope>examples/mc_att_control_multiplatform</scope>
</parameter>
<parameter default="60.0" name="MP_YAWRATE_MAX" type="FLOAT">
<short_desc>Max yaw rate</short_desc>
<long_desc>Limit for yaw rate, has effect for large rotations in autonomous mode, to avoid large control output and mixer saturation.</long_desc>
<min>0.0</min>
<max>360.0</max>
<unit>deg/s</unit>
<scope>examples/mc_att_control_multiplatform</scope>
</parameter>
<parameter default="0.3" name="MP_YAWRATE_P" type="FLOAT">
<short_desc>Yaw rate P gain</short_desc>
<long_desc>Yaw rate proportional gain, i.e. control output for angular speed error 1 rad/s.</long_desc>
<min>0.0</min>
<scope>examples/mc_att_control_multiplatform</scope>
</parameter>
<parameter default="0.5" name="MP_YAW_FF" type="FLOAT">
<short_desc>Yaw feed forward</short_desc>
<long_desc>Feed forward weight for manual yaw control. 0 will give slow responce and no overshot, 1 - fast responce and big overshot.</long_desc>
<min>0.0</min>
<max>1.0</max>
<scope>examples/mc_att_control_multiplatform</scope>
</parameter>
<parameter default="2.0" name="MP_YAW_P" type="FLOAT">
<short_desc>Yaw P gain</short_desc>
<long_desc>Yaw proportional gain, i.e. desired angular speed in rad/s for error 1 rad.</long_desc>
<min>0.0</min>
<unit>1/s</unit>
<scope>examples/mc_att_control_multiplatform</scope>
</parameter>
</group>
<group name="Multicopter Position Control">
<parameter default="10.0" name="MPC_ACC_DOWN_MAX" type="FLOAT">
......@@ -4863,112 +4683,6 @@ the setpoint will be capped to MPC_XY_VEL_MAX</short_desc>
<decimal>2</decimal>
<scope>modules/mc_pos_control</scope>
</parameter>
<parameter default="1.0" name="MPP_LAND_SPEED" type="FLOAT">
<short_desc>Landing descend rate</short_desc>
<min>0.0</min>
<unit>m/s</unit>
<scope>examples/mc_pos_control_multiplatform</scope>
</parameter>
<parameter default="1.0" name="MPP_THR_MAX" type="FLOAT">
<short_desc>Maximum thrust</short_desc>
<long_desc>Limit max allowed thrust.</long_desc>
<min>0.0</min>
<max>1.0</max>
<scope>examples/mc_pos_control_multiplatform</scope>
</parameter>
<parameter default="0.1" name="MPP_THR_MIN" type="FLOAT">
<short_desc>Minimum thrust</short_desc>
<long_desc>Minimum vertical thrust. It's recommended to set it &gt; 0 to avoid free fall with zero thrust.</long_desc>
<min>0.0</min>
<max>1.0</max>
<scope>examples/mc_pos_control_multiplatform</scope>
</parameter>
<parameter default="45.0" name="MPP_TILTMAX_AIR" type="FLOAT">
<short_desc>Maximum tilt angle in air</short_desc>
<long_desc>Limits maximum tilt in AUTO and POSCTRL modes during flight.</long_desc>
<min>0.0</min>
<max>90.0</max>
<unit>deg</unit>
<scope>examples/mc_pos_control_multiplatform</scope>
</parameter>
<parameter default="15.0" name="MPP_TILTMAX_LND" type="FLOAT">
<short_desc>Maximum tilt during landing</short_desc>
<long_desc>Limits maximum tilt angle on landing.</long_desc>
<min>0.0</min>
<max>90.0</max>
<unit>deg</unit>
<scope>examples/mc_pos_control_multiplatform</scope>
</parameter>
<parameter default="0.5" name="MPP_XY_FF" type="FLOAT">
<short_desc>Horizontal velocity feed forward</short_desc>
<long_desc>Feed forward weight for position control in position control mode (POSCTRL). 0 will give slow responce and no overshot, 1 - fast responce and big overshot.</long_desc>
<min>0.0</min>
<max>1.0</max>
<scope>examples/mc_pos_control_multiplatform</scope>
</parameter>
<parameter default="1.0" name="MPP_XY_P" type="FLOAT">
<short_desc>Proportional gain for horizontal position error</short_desc>
<min>0.0</min>
<scope>examples/mc_pos_control_multiplatform</scope>
</parameter>
<parameter default="0.01" name="MPP_XY_VEL_D" type="FLOAT">
<short_desc>Differential gain for horizontal velocity error. Small values help reduce fast oscillations. If value is too big oscillations will appear again</short_desc>
<min>0.0</min>
<scope>examples/mc_pos_control_multiplatform</scope>
</parameter>
<parameter default="0.02" name="MPP_XY_VEL_I" type="FLOAT">
<short_desc>Integral gain for horizontal velocity error</short_desc>
<long_desc>Non-zero value allows to resist wind.</long_desc>
<min>0.0</min>
<scope>examples/mc_pos_control_multiplatform</scope>
</parameter>
<parameter default="5.0" name="MPP_XY_VEL_MAX" type="FLOAT">
<short_desc>Maximum horizontal velocity</short_desc>
<long_desc>Maximum horizontal velocity in AUTO mode and endpoint for position stabilized mode (POSCTRL).</long_desc>
<min>0.0</min>
<unit>m/s</unit>
<scope>examples/mc_pos_control_multiplatform</scope>
</parameter>
<parameter default="0.1" name="MPP_XY_VEL_P" type="FLOAT">
<short_desc>Proportional gain for horizontal velocity error</short_desc>
<min>0.0</min>
<scope>examples/mc_pos_control_multiplatform</scope>
</parameter>
<parameter default="0.5" name="MPP_Z_FF" type="FLOAT">
<short_desc>Vertical velocity feed forward</short_desc>
<long_desc>Feed forward weight for altitude control in stabilized modes (ALTCTRL). 0 will give slow responce and no overshot, 1 - fast responce and big overshot.</long_desc>
<min>0.0</min>
<max>1.0</max>
<scope>examples/mc_pos_control_multiplatform</scope>
</parameter>
<parameter default="1.0" name="MPP_Z_P" type="FLOAT">
<short_desc>Proportional gain for vertical position error</short_desc>
<min>0.0</min>
<scope>examples/mc_pos_control_multiplatform</scope>
</parameter>
<parameter default="0.0" name="MPP_Z_VEL_D" type="FLOAT">
<short_desc>Differential gain for vertical velocity error</short_desc>
<min>0.0</min>
<scope>examples/mc_pos_control_multiplatform</scope>
</parameter>
<parameter default="0.02" name="MPP_Z_VEL_I" type="FLOAT">
<short_desc>Integral gain for vertical velocity error</short_desc>
<long_desc>Non zero value allows hovering thrust estimation on stabilized or autonomous takeoff.</long_desc>
<min>0.0</min>
<scope>examples/mc_pos_control_multiplatform</scope>
</parameter>
<parameter default="5.0" name="MPP_Z_VEL_MAX" type="FLOAT">
<short_desc>Maximum vertical velocity</short_desc>
<long_desc>Maximum vertical velocity in AUTO mode and endpoint for stabilized modes (ALTCTRL).</long_desc>
<min>0.0</min>
<unit>m/s</unit>
<scope>examples/mc_pos_control_multiplatform</scope>
</parameter>
<parameter default="0.1" name="MPP_Z_VEL_P" type="FLOAT">
<short_desc>Proportional gain for vertical velocity error</short_desc>
<min>0.0</min>
<scope>examples/mc_pos_control_multiplatform</scope>
</parameter>
</group>
<group name="PWM Outputs">
<parameter default="0.0" name="MOT_SLEW_MAX" type="FLOAT">
......@@ -5439,167 +5153,6 @@ the setpoint will be capped to MPC_XY_VEL_MAX</short_desc>
<scope>examples/bottle_drop</scope>
</parameter>
</group>
<group name="Position Estimator">
<parameter default="1e-05" name="PE_ABIAS_PNOISE" type="FLOAT">
<short_desc>Accelerometer bias estimate process noise</short_desc>
<long_desc>Generic defaults: 0.00001f, multicopters: 0.00001f, ground vehicles: 0.00001f. Increasing this value makes the bias estimation faster and noisier.</long_desc>
<min>0.00001</min>
<max>0.001</max>
<scope>examples/ekf_att_pos_estimator</scope>
</parameter>
<parameter default="0.125" name="PE_ACC_PNOISE" type="FLOAT">
<short_desc>Accelerometer process noise</short_desc>
<long_desc>Generic defaults: 0.25, multicopters: 0.25, ground vehicles: 0.25. Increasing this value makes the filter trust the accelerometer less and other sensors more.</long_desc>
<min>0.05</min>
<max>1.0</max>
<scope>examples/ekf_att_pos_estimator</scope>
</parameter>
<parameter default="1.4" name="PE_EAS_NOISE" type="FLOAT">
<short_desc>Airspeed measurement noise</short_desc>
<long_desc>Increasing this value will make the filter trust this sensor less and trust other sensors more.</long_desc>
<min>0.5</min>
<max>5.0</max>
<scope>examples/ekf_att_pos_estimator</scope>
</parameter>
<parameter default="1e-07" name="PE_GBIAS_PNOISE" type="FLOAT">
<short_desc>Gyro bias estimate process noise</short_desc>
<long_desc>Generic defaults: 1e-07f, multicopters: 1e-07f, ground vehicles: 1e-07f. Increasing this value will make the gyro bias converge faster but noisier.</long_desc>
<min>0.00000005</min>
<max>0.00001</max>
<scope>examples/ekf_att_pos_estimator</scope>
</parameter>
<parameter default="0.9" name="PE_GPS_ALT_WGT" type="FLOAT">
<short_desc>GPS vs. barometric altitude update weight</short_desc>
<long_desc>RE-CHECK this.</long_desc>
<min>0.0</min>
<max>1.0</max>
<scope>examples/ekf_att_pos_estimator</scope>
</parameter>
<parameter default="0.015" name="PE_GYRO_PNOISE" type="FLOAT">
<short_desc>Gyro process noise</short_desc>
<long_desc>Generic defaults: 0.015, multicopters: 0.015, ground vehicles: 0.015. This noise controls how much the filter trusts the gyro measurements. Increasing it makes the filter trust the gyro less and other sensors more.</long_desc>
<min>0.001</min>
<max>0.05</max>
<scope>examples/ekf_att_pos_estimator</scope>
</parameter>
<parameter default="350" name="PE_HGT_DELAY_MS" type="INT32">
<short_desc>Height estimate delay</short_desc>
<long_desc>The delay in milliseconds of the height estimate from the barometer.</long_desc>
<min>0</min>
<max>1000</max>
<unit>ms</unit>
<scope>examples/ekf_att_pos_estimator</scope>
</parameter>
<parameter default="0.0003" name="PE_MAGB_PNOISE" type="FLOAT">
<short_desc>Magnetometer body frame offsets process noise</short_desc>
<long_desc>Generic defaults: 0.0003, multicopters: 0.0003, ground vehicles: 0.0003. Increasing this value makes the magnetometer body bias estimate converge faster but also noisier.</long_desc>
<min>0.0001</min>
<max>0.01</max>
<scope>examples/ekf_att_pos_estimator</scope>
</parameter>
<parameter default="0.0" name="PE_MAGB_X" type="FLOAT">
<short_desc>Magnetometer X bias</short_desc>
<long_desc>The magnetometer bias. This bias is learnt by the filter over time and persists between boots.</long_desc>
<min>-0.6</min>
<max>0.6</max>
<scope>examples/ekf_att_pos_estimator</scope>
</parameter>
<parameter default="0.0" name="PE_MAGB_Y" type="FLOAT">
<short_desc>Magnetometer Y bias</short_desc>
<long_desc>The magnetometer bias. This bias is learnt by the filter over time and persists between boots.</long_desc>
<min>-0.6</min>
<max>0.6</max>
<scope>examples/ekf_att_pos_estimator</scope>
</parameter>
<parameter default="0.0" name="PE_MAGB_Z" type="FLOAT">
<short_desc>Magnetometer Z bias</short_desc>
<long_desc>The magnetometer bias. This bias is learnt by the filter over time and persists between boots.</long_desc>
<min>-0.6</min>
<max>0.6</max>
<scope>examples/ekf_att_pos_estimator</scope>
</parameter>
<parameter default="0.0003" name="PE_MAGE_PNOISE" type="FLOAT">
<short_desc>Magnetometer earth frame offsets process noise</short_desc>
<long_desc>Generic defaults: 0.0001, multicopters: 0.0001, ground vehicles: 0.0001. Increasing this value makes the magnetometer earth bias estimate converge faster but also noisier.</long_desc>
<min>0.0001</min>
<max>0.01</max>
<scope>examples/ekf_att_pos_estimator</scope>
</parameter>
<parameter default="30" name="PE_MAG_DELAY_MS" type="INT32">
<short_desc>Mag estimate delay</short_desc>
<long_desc>The delay in milliseconds of the magnetic field estimate from the magnetometer.</long_desc>
<min>0</min>
<max>1000</max>
<unit>ms</unit>
<scope>examples/ekf_att_pos_estimator</scope>
</parameter>
<parameter default="0.05" name="PE_MAG_NOISE" type="FLOAT">
<short_desc>Magnetometer measurement noise</short_desc>
<long_desc>Generic defaults: 0.05, multicopters: 0.05, ground vehicles: 0.05</long_desc>
<min>0.01</min>
<max>1.0</max>
<scope>examples/ekf_att_pos_estimator</scope>
</parameter>
<parameter default="5.0" name="PE_POSDEV_INIT" type="FLOAT">
<short_desc>Threshold for filter initialization</short_desc>
<long_desc>If the standard deviation of the GPS position estimate is below this threshold in meters, the filter will initialize.</long_desc>
<min>0.3</min>
<max>10.0</max>
<scope>examples/ekf_att_pos_estimator</scope>
</parameter>
<parameter default="1.25" name="PE_POSD_NOISE" type="FLOAT">
<short_desc>Position noise in down (vertical) direction</short_desc>
<long_desc>Generic defaults: 1.25, multicopters: 1.0, ground vehicles: 1.0</long_desc>
<min>0.5</min>
<max>3.0</max>
<scope>examples/ekf_att_pos_estimator</scope>
</parameter>
<parameter default="0.5" name="PE_POSNE_NOISE" type="FLOAT">
<short_desc>Position noise in north-east (horizontal) direction</short_desc>
<long_desc>Generic defaults: 0.5, multicopters: 0.5, ground vehicles: 0.5</long_desc>
<min>0.1</min>
<max>10.0</max>
<scope>examples/ekf_att_pos_estimator</scope>
</parameter>
<parameter default="210" name="PE_POS_DELAY_MS" type="INT32">
<short_desc>Position estimate delay</short_desc>
<long_desc>The delay in milliseconds of the position estimate from GPS.</long_desc>
<min>0</min>
<max>1000</max>
<unit>ms</unit>
<scope>examples/ekf_att_pos_estimator</scope>
</parameter>
<parameter default="210" name="PE_TAS_DELAY_MS" type="INT32">
<short_desc>True airspeeed estimate delay</short_desc>
<long_desc>The delay in milliseconds of the airspeed estimate.</long_desc>
<min>0</min>
<max>1000</max>
<unit>ms</unit>
<scope>examples/ekf_att_pos_estimator</scope>
</parameter>
<parameter default="0.3" name="PE_VELD_NOISE" type="FLOAT">
<short_desc>Velocity noise in down (vertical) direction</short_desc>
<long_desc>Generic default: 0.3, multicopters: 0.4, ground vehicles: 0.7</long_desc>
<min>0.2</min>
<max>3.0</max>
<scope>examples/ekf_att_pos_estimator</scope>
</parameter>
<parameter default="0.3" name="PE_VELNE_NOISE" type="FLOAT">
<short_desc>Velocity measurement noise in north-east (horizontal) direction</short_desc>
<long_desc>Generic default: 0.3, multicopters: 0.5, ground vehicles: 0.5</long_desc>
<min>0.05</min>
<max>5.0</max>
<scope>examples/ekf_att_pos_estimator</scope>
</parameter>
<parameter default="230" name="PE_VEL_DELAY_MS" type="INT32">
<short_desc>Velocity estimate delay</short_desc>
<long_desc>The delay in milliseconds of the velocity estimate from GPS.</long_desc>
<min>0</min>
<max>1000</max>
<unit>ms</unit>
<scope>examples/ekf_att_pos_estimator</scope>
</parameter>
</group>
<group name="Position Estimator INAV">
<parameter default="0" name="CBRK_NO_VISION" type="INT32">
<short_desc>Disable vision input</short_desc>
......@@ -8858,13 +8411,6 @@ This is used for gathering replay logs for the ekf2 module</short_desc>
</parameter>
</group>
<group name="Sensors">
<parameter default="0.2" name="ATT_VIBE_THRESH" type="FLOAT">
<short_desc>Threshold (of RMS) to warn about high vibration levels</short_desc>
<min>0.01</min>
<max>10</max>
<decimal>2</decimal>
<scope>modules/sensors</scope>
</parameter>
<parameter default="63" name="CAL_MAG_SIDES" type="INT32">
<short_desc>Bitfield selecting mag sides for calibration</short_desc>
<long_desc>DETECT_ORIENTATION_TAIL_DOWN = 1 DETECT_ORIENTATION_NOSE_DOWN = 2 DETECT_ORIENTATION_LEFT = 4 DETECT_ORIENTATION_RIGHT = 8 DETECT_ORIENTATION_UPSIDE_DOWN = 16 DETECT_ORIENTATION_RIGHTSIDE_UP = 32</long_desc>
......
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