From aeb0e8a7ab7e6cedd383f60e74f8ea34b71d77b6 Mon Sep 17 00:00:00 2001 From: PX4 Jenkins Date: Mon, 27 Nov 2017 04:41:42 +0000 Subject: [PATCH] Update PX4 Firmware metadata Mon Nov 27 04:41:42 UTC 2017 --- .../PX4/PX4ParameterFactMetaData.xml | 454 ------------------ 1 file changed, 454 deletions(-) diff --git a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml index 8c06eecd3..8e626f884 100644 --- a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml +++ b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml @@ -137,57 +137,6 @@ 0 - - - Moment of inertia matrix diagonal entry (1, 1) - kg*m^2 - examples/attitude_estimator_ekf - - - Moment of inertia matrix diagonal entry (2, 2) - kg*m^2 - examples/attitude_estimator_ekf - - - Moment of inertia matrix diagonal entry (3, 3) - kg*m^2 - examples/attitude_estimator_ekf - - - Moment of inertia enabled in estimator - If set to != 0 the moment of inertia will be used in the estimator - - examples/attitude_estimator_ekf - - - Body angular rate process noise - examples/attitude_estimator_ekf - - - Body angular acceleration process noise - examples/attitude_estimator_ekf - - - Acceleration process noise - examples/attitude_estimator_ekf - - - Magnet field vector process noise - examples/attitude_estimator_ekf - - - Gyro measurement noise - examples/attitude_estimator_ekf - - - Accel measurement noise - examples/attitude_estimator_ekf - - - Mag measurement noise - examples/attitude_estimator_ekf - - Acceleration compensation based on GPS @@ -4367,135 +4316,6 @@ default 1.5 turns per second 0.01 modules/mc_att_control - - Max manual pitch - 0.0 - 90.0 - deg - examples/mc_pos_control_multiplatform - - - Max manual roll - 0.0 - 90.0 - deg - examples/mc_pos_control_multiplatform - - - Max manual yaw rate - 0.0 - deg/s - examples/mc_pos_control_multiplatform - - - Max acro pitch rate - 0.0 - 360.0 - deg/s - examples/mc_att_control_multiplatform - - - Max acro roll rate - 0.0 - 360.0 - deg/s - examples/mc_att_control_multiplatform - - - Max acro yaw rate - 0.0 - deg/s - examples/mc_att_control_multiplatform - - - Pitch rate D gain - Pitch rate differential gain. Small values help reduce fast oscillations. If value is too big oscillations will appear again. - 0.0 - examples/mc_att_control_multiplatform - - - Pitch rate I gain - Pitch rate integral gain. Can be set to compensate static thrust difference or gravity center offset. - 0.0 - examples/mc_att_control_multiplatform - - - Pitch rate P gain - Pitch rate proportional gain, i.e. control output for angular speed error 1 rad/s. - 0.0 - examples/mc_att_control_multiplatform - - - Pitch P gain - Pitch proportional gain, i.e. desired angular speed in rad/s for error 1 rad. - 0.0 - 1/s - examples/mc_att_control_multiplatform - - - Roll rate D gain - Roll rate differential gain. Small values help reduce fast oscillations. If value is too big oscillations will appear again. - 0.0 - examples/mc_att_control_multiplatform - - - Roll rate I gain - Roll rate integral gain. Can be set to compensate static thrust difference or gravity center offset. - 0.0 - examples/mc_att_control_multiplatform - - - Roll rate P gain - Roll rate proportional gain, i.e. control output for angular speed error 1 rad/s. - 0.0 - examples/mc_att_control_multiplatform - - - Roll P gain - Roll proportional gain, i.e. desired angular speed in rad/s for error 1 rad. - 0.0 - examples/mc_att_control_multiplatform - - - Yaw rate D gain - Yaw rate differential gain. Small values help reduce fast oscillations. If value is too big oscillations will appear again. - 0.0 - examples/mc_att_control_multiplatform - - - Yaw rate I gain - Yaw rate integral gain. Can be set to compensate static thrust difference or gravity center offset. - 0.0 - examples/mc_att_control_multiplatform - - - Max yaw rate - Limit for yaw rate, has effect for large rotations in autonomous mode, to avoid large control output and mixer saturation. - 0.0 - 360.0 - deg/s - examples/mc_att_control_multiplatform - - - Yaw rate P gain - Yaw rate proportional gain, i.e. control output for angular speed error 1 rad/s. - 0.0 - examples/mc_att_control_multiplatform - - - Yaw feed forward - Feed forward weight for manual yaw control. 0 will give slow responce and no overshot, 1 - fast responce and big overshot. - 0.0 - 1.0 - examples/mc_att_control_multiplatform - - - Yaw P gain - Yaw proportional gain, i.e. desired angular speed in rad/s for error 1 rad. - 0.0 - 1/s - examples/mc_att_control_multiplatform - @@ -4863,112 +4683,6 @@ the setpoint will be capped to MPC_XY_VEL_MAX 2 modules/mc_pos_control - - Landing descend rate - 0.0 - m/s - examples/mc_pos_control_multiplatform - - - Maximum thrust - Limit max allowed thrust. - 0.0 - 1.0 - examples/mc_pos_control_multiplatform - - - Minimum thrust - Minimum vertical thrust. It's recommended to set it > 0 to avoid free fall with zero thrust. - 0.0 - 1.0 - examples/mc_pos_control_multiplatform - - - Maximum tilt angle in air - Limits maximum tilt in AUTO and POSCTRL modes during flight. - 0.0 - 90.0 - deg - examples/mc_pos_control_multiplatform - - - Maximum tilt during landing - Limits maximum tilt angle on landing. - 0.0 - 90.0 - deg - examples/mc_pos_control_multiplatform - - - Horizontal velocity feed forward - 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. - 0.0 - 1.0 - examples/mc_pos_control_multiplatform - - - Proportional gain for horizontal position error - 0.0 - examples/mc_pos_control_multiplatform - - - Differential gain for horizontal velocity error. Small values help reduce fast oscillations. If value is too big oscillations will appear again - 0.0 - examples/mc_pos_control_multiplatform - - - Integral gain for horizontal velocity error - Non-zero value allows to resist wind. - 0.0 - examples/mc_pos_control_multiplatform - - - Maximum horizontal velocity - Maximum horizontal velocity in AUTO mode and endpoint for position stabilized mode (POSCTRL). - 0.0 - m/s - examples/mc_pos_control_multiplatform - - - Proportional gain for horizontal velocity error - 0.0 - examples/mc_pos_control_multiplatform - - - Vertical velocity feed forward - Feed forward weight for altitude control in stabilized modes (ALTCTRL). 0 will give slow responce and no overshot, 1 - fast responce and big overshot. - 0.0 - 1.0 - examples/mc_pos_control_multiplatform - - - Proportional gain for vertical position error - 0.0 - examples/mc_pos_control_multiplatform - - - Differential gain for vertical velocity error - 0.0 - examples/mc_pos_control_multiplatform - - - Integral gain for vertical velocity error - Non zero value allows hovering thrust estimation on stabilized or autonomous takeoff. - 0.0 - examples/mc_pos_control_multiplatform - - - Maximum vertical velocity - Maximum vertical velocity in AUTO mode and endpoint for stabilized modes (ALTCTRL). - 0.0 - m/s - examples/mc_pos_control_multiplatform - - - Proportional gain for vertical velocity error - 0.0 - examples/mc_pos_control_multiplatform - @@ -5439,167 +5153,6 @@ the setpoint will be capped to MPC_XY_VEL_MAX examples/bottle_drop - - - Accelerometer bias estimate process noise - Generic defaults: 0.00001f, multicopters: 0.00001f, ground vehicles: 0.00001f. Increasing this value makes the bias estimation faster and noisier. - 0.00001 - 0.001 - examples/ekf_att_pos_estimator - - - Accelerometer process noise - 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. - 0.05 - 1.0 - examples/ekf_att_pos_estimator - - - Airspeed measurement noise - Increasing this value will make the filter trust this sensor less and trust other sensors more. - 0.5 - 5.0 - examples/ekf_att_pos_estimator - - - Gyro bias estimate process noise - Generic defaults: 1e-07f, multicopters: 1e-07f, ground vehicles: 1e-07f. Increasing this value will make the gyro bias converge faster but noisier. - 0.00000005 - 0.00001 - examples/ekf_att_pos_estimator - - - GPS vs. barometric altitude update weight - RE-CHECK this. - 0.0 - 1.0 - examples/ekf_att_pos_estimator - - - Gyro process noise - 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. - 0.001 - 0.05 - examples/ekf_att_pos_estimator - - - Height estimate delay - The delay in milliseconds of the height estimate from the barometer. - 0 - 1000 - ms - examples/ekf_att_pos_estimator - - - Magnetometer body frame offsets process noise - 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. - 0.0001 - 0.01 - examples/ekf_att_pos_estimator - - - Magnetometer X bias - The magnetometer bias. This bias is learnt by the filter over time and persists between boots. - -0.6 - 0.6 - examples/ekf_att_pos_estimator - - - Magnetometer Y bias - The magnetometer bias. This bias is learnt by the filter over time and persists between boots. - -0.6 - 0.6 - examples/ekf_att_pos_estimator - - - Magnetometer Z bias - The magnetometer bias. This bias is learnt by the filter over time and persists between boots. - -0.6 - 0.6 - examples/ekf_att_pos_estimator - - - Magnetometer earth frame offsets process noise - 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. - 0.0001 - 0.01 - examples/ekf_att_pos_estimator - - - Mag estimate delay - The delay in milliseconds of the magnetic field estimate from the magnetometer. - 0 - 1000 - ms - examples/ekf_att_pos_estimator - - - Magnetometer measurement noise - Generic defaults: 0.05, multicopters: 0.05, ground vehicles: 0.05 - 0.01 - 1.0 - examples/ekf_att_pos_estimator - - - Threshold for filter initialization - If the standard deviation of the GPS position estimate is below this threshold in meters, the filter will initialize. - 0.3 - 10.0 - examples/ekf_att_pos_estimator - - - Position noise in down (vertical) direction - Generic defaults: 1.25, multicopters: 1.0, ground vehicles: 1.0 - 0.5 - 3.0 - examples/ekf_att_pos_estimator - - - Position noise in north-east (horizontal) direction - Generic defaults: 0.5, multicopters: 0.5, ground vehicles: 0.5 - 0.1 - 10.0 - examples/ekf_att_pos_estimator - - - Position estimate delay - The delay in milliseconds of the position estimate from GPS. - 0 - 1000 - ms - examples/ekf_att_pos_estimator - - - True airspeeed estimate delay - The delay in milliseconds of the airspeed estimate. - 0 - 1000 - ms - examples/ekf_att_pos_estimator - - - Velocity noise in down (vertical) direction - Generic default: 0.3, multicopters: 0.4, ground vehicles: 0.7 - 0.2 - 3.0 - examples/ekf_att_pos_estimator - - - Velocity measurement noise in north-east (horizontal) direction - Generic default: 0.3, multicopters: 0.5, ground vehicles: 0.5 - 0.05 - 5.0 - examples/ekf_att_pos_estimator - - - Velocity estimate delay - The delay in milliseconds of the velocity estimate from GPS. - 0 - 1000 - ms - examples/ekf_att_pos_estimator - - Disable vision input @@ -8858,13 +8411,6 @@ This is used for gathering replay logs for the ekf2 module - - Threshold (of RMS) to warn about high vibration levels - 0.01 - 10 - 2 - modules/sensors - Bitfield selecting mag sides for calibration 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 -- 2.22.0