/**************************************************************************** * * Copyright (c) 2013-2016 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions * are met: * * 1. Redistributions of source code must retain the above copyright * notice, this list of conditions and the following disclaimer. * 2. Redistributions in binary form must reproduce the above copyright * notice, this list of conditions and the following disclaimer in * the documentation and/or other materials provided with the * distribution. * 3. Neither the name PX4 nor the names of its contributors may be * used to endorse or promote products derived from this software * without specific prior written permission. * * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT * LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS * FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE * COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, * INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, * BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS * OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED * AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT * LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN * ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE * POSSIBILITY OF SUCH DAMAGE. * ****************************************************************************/ /** * @file mc_pos_control_params.c * Multicopter position controller parameters. * * @author Anton Babushkin <anton@px4.io> */ /** * Minimum thrust in auto thrust control * * It's recommended to set it > 0 to avoid free fall with zero thrust. * * @unit norm * @min 0.05 * @max 1.0 * @decimal 2 * @increment 0.01 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_THR_MIN, 0.12f); /** * Hover thrust * * Vertical thrust required to hover. * This value is mapped to center stick for manual throttle control. * With this value set to the thrust required to hover, transition * from manual to Altitude or Position mode while hovering will occur with the * throttle stick near center, which is then interpreted as (near) * zero demand for vertical speed. * * This parameter is also important for the landing detection to work correctly. * * @unit norm * @min 0.1 * @max 0.8 * @decimal 2 * @increment 0.01 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_THR_HOVER, 0.5f); /** * Thrust curve in Manual Mode * * This parameter defines how the throttle stick input is mapped to commanded thrust * in Manual/Stabilized flight mode. * * In case the default is used ('Rescale to hover thrust'), the stick input is linearly * rescaled, such that a centered stick corresponds to the hover throttle (see MPC_THR_HOVER). * * Select 'No Rescale' to directly map the stick 1:1 to the output. This can be useful * in case the hover thrust is very low and the default would lead to too much distortion * (e.g. if hover thrust is set to 20%, 80% of the upper thrust range is squeezed into the * upper half of the stick range). * * Note: in case MPC_THR_HOVER is set to 50%, the modes 0 and 1 are the same. * * @value 0 Rescale to hover thrust * @value 1 No Rescale * @group Multicopter Position Control */ PARAM_DEFINE_INT32(MPC_THR_CURVE, 0); /** * Maximum thrust in auto thrust control * * Limit max allowed thrust * * @unit norm * @min 0.0 * @max 1.0 * @decimal 2 * @increment 0.01 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_THR_MAX, 1.0f); /** * Minimum manual thrust * * Minimum vertical thrust. It's recommended to set it > 0 to avoid free fall with zero thrust. * With MC_AIRMODE set to 1, this can safely be set to 0. * * @unit norm * @min 0.0 * @max 1.0 * @decimal 2 * @increment 0.01 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_MANTHR_MIN, 0.08f); /** * Proportional gain for vertical position error * * @min 0.0 * @max 1.5 * @decimal 2 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_Z_P, 1.0f); /** * Proportional gain for vertical velocity error * * @min 0.1 * @max 0.4 * @decimal 2 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_Z_VEL_P, 0.2f); /** * Integral gain for vertical velocity error * * Non zero value allows hovering thrust estimation on stabilized or autonomous takeoff. * * @min 0.01 * @max 0.1 * @decimal 3 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_Z_VEL_I, 0.02f); /** * Differential gain for vertical velocity error * * @min 0.0 * @max 0.1 * @decimal 3 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_Z_VEL_D, 0.0f); /** * Maximum vertical ascent velocity * * Maximum vertical velocity in AUTO mode and endpoint for stabilized modes (ALTCTRL, POSCTRL). * * @unit m/s * @min 0.5 * @max 8.0 * @decimal 1 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_Z_VEL_MAX_UP, 3.0f); /** * Maximum vertical descent velocity * * Maximum vertical velocity in AUTO mode and endpoint for stabilized modes (ALTCTRL, POSCTRL). * * @unit m/s * @min 0.5 * @max 4.0 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_Z_VEL_MAX_DN, 1.0f); /** * Proportional gain for horizontal position error * * @min 0.0 * @max 2.0 * @decimal 2 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_XY_P, 0.95f); /** * Proportional gain for horizontal velocity error * * @min 0.06 * @max 0.15 * @decimal 2 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_XY_VEL_P, 0.09f); /** * Integral gain for horizontal velocity error * * Non-zero value allows to resist wind. * * @min 0.0 * @max 0.1 * @decimal 3 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_XY_VEL_I, 0.02f); /** * Differential gain for horizontal velocity error. Small values help reduce fast oscillations. If value is too big oscillations will appear again. * * @min 0.005 * @max 0.1 * @decimal 3 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_XY_VEL_D, 0.01f); /** * Maximum horizontal velocity in mission * * Normal horizontal velocity in AUTO modes (includes * also RTL / hold / etc.) and endpoint for * position stabilized mode (POSCTRL). * * @unit m/s * @min 3.0 * @max 20.0 * @increment 1 * @decimal 2 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_XY_CRUISE, 5.0f); /** * Proportional gain for horizontal trajectory position error * * @min 0.1 * @max 5.0 * @decimal 1 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_XY_TRAJ_P, 0.3f); /** * Proportional gain for vertical trajectory position error * * @min 0.1 * @max 5.0 * @decimal 1 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_Z_TRAJ_P, 0.3f); /** * Cruise speed when angle prev-current/current-next setpoint * is 90 degrees. It should be lower than MPC_XY_CRUISE. * * Applies only in AUTO modes (includes * also RTL / hold / etc.) * * @unit m/s * @min 1.0 * @max 20.0 * @increment 1 * @decimal 2 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_CRUISE_90, 3.0f); /** * Maximum horizontal velocity setpoint for manual controlled mode * If velocity setpoint larger than MPC_XY_VEL_MAX is set, then * the setpoint will be capped to MPC_XY_VEL_MAX * * @unit m/s * @min 3.0 * @max 20.0 * @increment 1 * @decimal 2 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_VEL_MANUAL, 10.0f); /** * Maximum horizontal velocity * * Maximum horizontal velocity in AUTO mode. If higher speeds * are commanded in a mission they will be capped to this velocity. * * @unit m/s * @min 0.0 * @max 20.0 * @increment 1 * @decimal 2 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_XY_VEL_MAX, 12.0f); /** * Maximum tilt angle in air * * Limits maximum tilt in AUTO and POSCTRL modes during flight. * * @unit deg * @min 0.0 * @max 90.0 * @decimal 1 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_TILTMAX_AIR, 45.0f); /** * Maximum tilt during landing * * Limits maximum tilt angle on landing. * * @unit deg * @min 0.0 * @max 90.0 * @decimal 1 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_TILTMAX_LND, 12.0f); /** * Landing descend rate * * @unit m/s * @min 0.6 * @decimal 1 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_LAND_SPEED, 0.7f); /** * Takeoff climb rate * * @unit m/s * @min 1 * @max 5 * @decimal 2 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_TKO_SPEED, 1.5f); /** * Maximal tilt angle in manual or altitude mode * * @unit deg * @min 0.0 * @max 90.0 * @decimal 1 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_MAN_TILT_MAX, 35.0f); /** * Max manual yaw rate * * @unit deg/s * @min 0.0 * @max 400 * @decimal 1 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_MAN_Y_MAX, 200.0f); /** * Deadzone of sticks where position hold is enabled * * @min 0.0 * @max 1.0 * @decimal 2 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_HOLD_DZ, 0.1f); /** * Maximum horizontal velocity for which position hold is enabled (use 0 to disable check) * * @unit m/s * @min 0.0 * @max 3.0 * @decimal 2 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_HOLD_MAX_XY, 0.8f); /** * Maximum vertical velocity for which position hold is enabled (use 0 to disable check) * * @unit m/s * @min 0.0 * @max 3.0 * @decimal 2 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_HOLD_MAX_Z, 0.6f); /** * Low pass filter cut freq. for numerical velocity derivative * * @unit Hz * @min 0.0 * @max 10 * @decimal 2 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_VELD_LP, 5.0f); /** * Maximum horizontal acceleration for auto mode and maximum deceleration for manual mode * * @unit m/s/s * @min 2.0 * @max 15.0 * @increment 1 * @decimal 2 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_ACC_HOR_MAX, 10.0f); /** * Acceleration for auto and for manual * * @unit m/s/s * @min 2.0 * @max 15.0 * @increment 1 * @decimal 2 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_ACC_HOR, 5.0f); /** * Slow horizontal manual deceleration for manual mode * * @unit m/s/s * @min 0.5 * @max 10.0 * @increment 1 * @decimal 2 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_DEC_HOR_SLOW, 5.0f); /** * Horizontal acceleration in manual modes when te estimator speed limit is removed. * If full stick is being applied and the estimator stops demanding a speed limit, * which it had been before (e.g if GPS is gained while flying on optical flow/vision only), * the vehicle will accelerate at this rate until the normal position control speed is achieved. * * @unit m/s/s * @min 0.2 * @max 2.0 * @increment 0.1 * @decimal 1 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_ACC_HOR_ESTM, 0.5f); /** * Maximum vertical acceleration in velocity controlled modes upward * * @unit m/s/s * @min 2.0 * @max 15.0 * @increment 1 * @decimal 2 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_ACC_UP_MAX, 10.0f); /** * Maximum vertical acceleration in velocity controlled modes down * * @unit m/s/s * @min 2.0 * @max 15.0 * @increment 1 * @decimal 2 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_ACC_DOWN_MAX, 10.0f); /** * Maximum jerk limit * * Limit the maximum jerk of the vehicle (how fast the acceleration can change). * A lower value leads to smoother vehicle motions, but it also limits its * agility (how fast it can change directions or break). * * Setting this to the maximum value essentially disables the limit. * * Note: this is only used when MPC_POS_MODE is set to a smoothing mode. * * @unit m/s/s/s * @min 0.5 * @max 500.0 * @increment 1 * @decimal 2 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_JERK_MAX, 20.0f); /** * Velocity-based jerk limit * * If this is not zero, a velocity-based maximum jerk limit is used: the applied * jerk limit linearly increases with the vehicle's velocity between * MPC_JERK_MIN (zero velocity) and MPC_JERK_MAX (maximum velocity). * * This means that the vehicle's motions are smooth for low velocities, but * still allows fast direction changes or breaking at higher velocities. * * Set this to zero to use a fixed maximum jerk limit (MPC_JERK_MAX). * * Note: this is only used when MPC_POS_MODE is set to a smoothing mode. * * @unit m/s/s/s * @min 0 * @max 30.0 * @increment 1 * @decimal 2 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_JERK_MIN, 8.0f); /** * Altitude control mode. * * Set to 0 to control height relative to the earth frame origin. This origin may move up and down in * flight due to sensor drift. * Set to 1 to control height relative to estimated distance to ground. The vehicle will move up and down * with terrain height variation. Requires a distance to ground sensor. The height controller will * revert to using height above origin if the distance to ground estimate becomes invalid as indicated * by the local_position.distance_bottom_valid message being false. * Set to 2 to control height relative to ground (requires a distance sensor) when stationary and relative * to earth frame origin when moving horizontally. * The speed threshold is controlled by the MPC_HOLD_MAX_XY parameter. * * @min 0 * @max 2 * @value 0 Altitude following * @value 1 Terrain following * @value 2 Terrain hold * @group Multicopter Position Control */ PARAM_DEFINE_INT32(MPC_ALT_MODE, 0); /** * Manual control stick exponential curve sensitivity attenuation with small velocity setpoints * * The higher the value the less sensitivity the stick has around zero * while still reaching the maximum value with full stick deflection. * * 0 Purely linear input curve (default) * 1 Purely cubic input curve * * @min 0 * @max 1 * @decimal 2 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_XY_MAN_EXPO, 0.0f); /** * Manual control stick vertical exponential curve * * The higher the value the less sensitivity the stick has around zero * while still reaching the maximum value with full stick deflection. * * 0 Purely linear input curve (default) * 1 Purely cubic input curve * * @min 0 * @max 1 * @decimal 2 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_Z_MAN_EXPO, 0.0f); /** * Manual control stick yaw rotation exponential curve * * The higher the value the less sensitivity the stick has around zero * while still reaching the maximum value with full stick deflection. * * 0 Purely linear input curve (default) * 1 Purely cubic input curve * * @min 0 * @max 1 * @decimal 2 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_YAW_EXPO, 0.0f); /** * Altitude for 1. step of slow landing (descend) * * Below this altitude descending velocity gets limited * to a value between "MPC_Z_VEL_MAX" and "MPC_LAND_SPEED" * to enable a smooth descent experience * Value needs to be higher than "MPC_LAND_ALT2" * * @unit m * @min 0 * @max 122 * @decimal 1 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_LAND_ALT1, 10.0f); /** * Altitude for 2. step of slow landing (landing) * * Below this altitude descending velocity gets limited to "MPC_LAND_SPEED" * Value needs to be lower than "MPC_LAND_ALT1" * * @unit m * @min 0 * @max 122 * @decimal 1 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_LAND_ALT2, 5.0f); /** * Position control smooth takeoff ramp time constant * * Increasing this value will make automatic and manual takeoff slower. * If it's too slow the drone might scratch the ground and tip over. * * @min 0.1 * @max 1 * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_TKO_RAMP_T, 0.4f); /** * Manual-Position control sub-mode. * * The supported sub-modes are: * 0 Default position control where sticks map to position/velocity directly. Maximum speeds * is MPC_VEL_MANUAL. * 1 Smooth position control where setpoints are adjusted based on acceleration limits * and jerk limits. * 2 Sport mode that is the same Default position control but with velocity limits set to * the maximum allowed speeds (MPC_XY_VEL_MAX) * 3 Smooth position control with maximum acceleration and jerk limits (different algorithm * than 1). * * @value 0 Default position control * @value 1 Smooth position control * @value 2 Sport position control * @value 3 Smooth position control (Velocity) * @group Multicopter Position Control */ PARAM_DEFINE_INT32(MPC_POS_MODE, 1); /** * Auto sub-mode. * * The supported sub-modes are: * 0 Direct line tracking, no smoothing * * 1 Not used * * 2 Not used * * 3 Jerk-limited trajectory * * @value 0 Default line tracking * @value 1 N/A * @value 2 N/A * @value 3 Jerk-limited trajectory * @group Multicopter Position Control */ PARAM_DEFINE_INT32(MPC_AUTO_MODE, 3); /** * Delay from idle state to arming state. * * For altitude controlled modes, the transition from * idle to armed state is delayed by MPC_IDLE_TKO time to ensure * that the propellers have reached idle speed before attempting a * takeoff. This delay is particularly useful for vehicles with large * propellers. * * @min 0 * @max 10 * @unit sec * @group Multicopter Position Control */ PARAM_DEFINE_FLOAT(MPC_IDLE_TKO, 0.0f); /** * Flag to enable obstacle avoidance * Temporary Parameter to enable interface testing * * @boolean * @group Multicopter Position Control */ PARAM_DEFINE_INT32(MPC_OBS_AVOID, 0); /** * Yaw mode. * * Specifies the heading in Auto. * * @min 0 * @max 2 * @value 0 towards waypoint * @value 1 towards home * @value 2 away from home * @value 3 along trajectory * @group Mission */ PARAM_DEFINE_INT32(MPC_YAW_MODE, 0);