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FlightTaskOrbit: parameterize hardcoded maximum radius (#20012)
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@ -72,7 +72,7 @@ bool FlightTaskOrbit::applyCommandParameters(const vehicle_command_s &command)
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float new_velocity = signFromBool(new_is_clockwise) * new_absolute_velocity;
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if (math::isInRange(new_radius, _radius_min, _radius_max)) {
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if (math::isInRange(new_radius, _radius_min, _param_mc_orbit_rad_max.get())) {
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_started_clockwise = new_is_clockwise;
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_sanitizeParams(new_radius, new_velocity);
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_orbit_radius = new_radius;
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@ -146,7 +146,7 @@ bool FlightTaskOrbit::sendTelemetry()
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void FlightTaskOrbit::_sanitizeParams(float &radius, float &velocity) const
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{
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// clip the radius to be within range
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radius = math::constrain(radius, _radius_min, _radius_max);
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radius = math::constrain(radius, _radius_min, _param_mc_orbit_rad_max.get());
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velocity = math::constrain(velocity, -fabsf(_velocity_max), fabsf(_velocity_max));
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bool exceeds_maximum_acceleration = (velocity * velocity) >= _acceleration_max * radius;
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@ -70,7 +70,6 @@ protected:
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private:
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/* TODO: Should be controlled by params */
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static constexpr float _radius_min = 1.f;
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static constexpr float _radius_max = 1e3f;
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static constexpr float _velocity_max = 10.f;
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static constexpr float _acceleration_max = 2.f;
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static constexpr float _horizontal_acceptance_radius = 2.f;
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@ -132,6 +131,7 @@ private:
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uORB::PublicationMulti<orbit_status_s> _orbit_status_pub{ORB_ID(orbit_status)};
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DEFINE_PARAMETERS(
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(ParamFloat<px4::params::MC_ORBIT_RAD_MAX>) _param_mc_orbit_rad_max,
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(ParamFloat<px4::params::MPC_XY_CRUISE>) _param_mpc_xy_cruise, /**< cruise speed for circle approach */
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(ParamFloat<px4::params::MPC_YAWRAUTO_MAX>) _param_mpc_yawrauto_max,
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(ParamFloat<px4::params::MPC_XY_TRAJ_P>) _param_mpc_xy_traj_p,
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@ -0,0 +1,44 @@
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/****************************************************************************
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*
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* Copyright (c) 2022 PX4 Development Team. All rights reserved.
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*
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* Redistribution and use in source and binary forms, with or without
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* modification, are permitted provided that the following conditions
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* are met:
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*
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* 1. Redistributions of source code must retain the above copyright
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* notice, this list of conditions and the following disclaimer.
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* 2. Redistributions in binary form must reproduce the above copyright
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* notice, this list of conditions and the following disclaimer in
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* the documentation and/or other materials provided with the
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* distribution.
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* 3. Neither the name PX4 nor the names of its contributors may be
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* used to endorse or promote products derived from this software
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* without specific prior written permission.
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*
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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* POSSIBILITY OF SUCH DAMAGE.
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*
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****************************************************************************/
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/**
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* Maximum radius of orbit
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*
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* @unit m
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* @min 1.0
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* @max 10000.0
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* @increment 0.5
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* @decimal 1
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* @group FlightTaskOrbit
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*/
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PARAM_DEFINE_FLOAT(MC_ORBIT_RAD_MAX, 1000.0f);
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