mirror of https://github.com/ArduPilot/ardupilot
SITL: Add simulator for tethered vehicle
This commit is contained in:
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af0fe69085
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@ -839,6 +839,11 @@ void Aircraft::update_dynamics(const Vector3f &rot_accel)
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sitl->models.slung_payload_sim.update(get_position_relhome(), velocity_ef, accel_earth, wind_ef);
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sitl->models.slung_payload_sim.update(get_position_relhome(), velocity_ef, accel_earth, wind_ef);
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#endif
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#endif
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// update tether
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#if AP_SIM_TETHER_ENABLED
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sitl->models.tether_sim.update(location);
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#endif
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// allow for changes in physics step
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// allow for changes in physics step
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adjust_frame_time(constrain_float(sitl->loop_rate_hz, rate_hz-1, rate_hz+1));
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adjust_frame_time(constrain_float(sitl->loop_rate_hz, rate_hz-1, rate_hz+1));
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}
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}
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@ -1273,18 +1278,26 @@ void Aircraft::add_twist_forces(Vector3f &rot_accel)
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}
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}
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}
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}
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#if AP_SIM_SLUNGPAYLOAD_ENABLED
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// add body-frame force due to slung payload and tether
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// add body-frame force due to slung payload
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void Aircraft::add_external_forces(Vector3f &body_accel)
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void Aircraft::add_slungpayload_forces(Vector3f &body_accel)
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{
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{
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Vector3f forces_ef;
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Vector3f total_force;
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sitl->models.slung_payload_sim.get_forces_on_vehicle(forces_ef);
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#if AP_SIM_SLUNGPAYLOAD_ENABLED
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Vector3f forces_ef_slung;
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sitl->models.slung_payload_sim.get_forces_on_vehicle(forces_ef_slung);
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total_force += forces_ef_slung;
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#endif
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#if AP_SIM_TETHER_ENABLED
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Vector3f forces_ef_tether;
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sitl->models.tether_sim.get_forces_on_vehicle(forces_ef_tether);
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total_force += forces_ef_tether;
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#endif
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// convert ef forces to body-frame accelerations (acceleration = force / mass)
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// convert ef forces to body-frame accelerations (acceleration = force / mass)
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const Vector3f accel_bf = dcm.transposed() * forces_ef / mass;
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const Vector3f accel_bf_tether = dcm.transposed() * total_force / mass;
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body_accel += accel_bf;
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body_accel += accel_bf_tether;
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}
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}
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#endif
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/*
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/*
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get position relative to home
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get position relative to home
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@ -322,10 +322,8 @@ protected:
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void add_shove_forces(Vector3f &rot_accel, Vector3f &body_accel);
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void add_shove_forces(Vector3f &rot_accel, Vector3f &body_accel);
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void add_twist_forces(Vector3f &rot_accel);
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void add_twist_forces(Vector3f &rot_accel);
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#if AP_SIM_SLUNGPAYLOAD_ENABLED
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// add body-frame force due to payload
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// add body-frame force due to slung payload
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void add_external_forces(Vector3f &body_accel);
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void add_slungpayload_forces(Vector3f &body_accel);
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#endif
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// get local thermal updraft
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// get local thermal updraft
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float get_local_updraft(const Vector3d ¤tPos);
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float get_local_updraft(const Vector3d ¤tPos);
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@ -49,10 +49,8 @@ void MultiCopter::calculate_forces(const struct sitl_input &input, Vector3f &rot
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add_shove_forces(rot_accel, body_accel);
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add_shove_forces(rot_accel, body_accel);
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add_twist_forces(rot_accel);
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add_twist_forces(rot_accel);
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#if AP_SIM_SLUNGPAYLOAD_ENABLED
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// add forces from slung payload or tether payload
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// add forces from slung payload
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add_external_forces(body_accel);
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add_slungpayload_forces(body_accel);
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#endif
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}
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}
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/*
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/*
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@ -0,0 +1,309 @@
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/*
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This program is free software: you can redistribute it and/or modify
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it under the terms of the GNU General Public License as published by
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the Free Software Foundation, either version 3 of the License, or
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(at your option) any later version.
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This program is distributed in the hope that it will be useful,
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but WITHOUT ANY WARRANTY; without even the implied warranty of
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MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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GNU General Public License for more details.
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You should have received a copy of the GNU General Public License
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along with this program. If not, see <http://www.gnu.org/licenses/>.
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*/
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/*
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simulate a static tether attached to the vehicle and ground
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*/
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#include "SIM_config.h"
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#if AP_SIM_TETHER_ENABLED
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#include "SIM_Tether.h"
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#include "SITL.h"
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#include <stdio.h>
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#include "SIM_Aircraft.h"
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#include <AP_HAL_SITL/SITL_State.h>
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#include <GCS_MAVLink/GCS.h>
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#include <AP_Logger/AP_Logger.h>
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using namespace SITL;
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// TetherSim parameters
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const AP_Param::GroupInfo TetherSim::var_info[] = {
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// @Param: ENABLE
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// @DisplayName: Tether Simulation Enable/Disable
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// @Description: Enable or disable the tether simulation
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// @Values: 0:Disabled,1:Enabled
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// @User: Advanced
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AP_GROUPINFO_FLAGS("ENABLE", 1, TetherSim, enable, 0, AP_PARAM_FLAG_ENABLE),
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// @Param: DENSITY
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// @DisplayName: Tether Wire Density
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// @Description: Linear mass density of the tether wire
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// @Range: 0 1
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// @User: Advanced
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AP_GROUPINFO("DENSITY", 2, TetherSim, tether_linear_density, 0.0167),
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// @Param: LINELEN
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// @DisplayName: Tether Maximum Line Length
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// @Description: Maximum length of the tether line in meters
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// @Units: m
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// @Range: 0 100
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// @User: Advanced
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AP_GROUPINFO("LINELEN", 3, TetherSim, max_line_length, 100.0),
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// @Param: SYSID
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// @DisplayName: Tether Simulation MAVLink System ID
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// @Description: MAVLink system ID for the tether simulation, used to distinguish it from other systems on the network
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// @Range: 0 255
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// @User: Advanced
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AP_GROUPINFO("SYSID", 4, TetherSim, sys_id, 2),
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// @Param: STUCK
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// @DisplayName: Tether Stuck Enable/Disable
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// @Description: Enable or disable a stuck tether simulation
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// @Values: 0:Disabled,1:Enabled
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// @User: Advanced
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AP_GROUPINFO("STUCK", 5, TetherSim, tether_stuck, 0),
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// @Param: SPGCNST
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// @DisplayName: Tether Spring Constant
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// @Description: Spring constant for the tether to simulate elastic forces when stretched beyond its maximum length
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// @Range: 0 255
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// @User: Advanced
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AP_GROUPINFO("SPGCNST", 6, TetherSim, tether_spring_constant, 100),
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AP_GROUPEND
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};
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// TetherSim handles interaction with main vehicle
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TetherSim::TetherSim()
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{
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AP_Param::setup_object_defaults(this, var_info);
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}
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void TetherSim::update(const Location& veh_pos)
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{
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if (!enable) {
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return;
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}
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if (veh_pos.is_zero()) {
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return;
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}
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// initialise fixed tether ground location
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const uint32_t now_us = AP_HAL::micros();
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if (!initialised) {
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// capture EKF origin
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auto *sitl = AP::sitl();
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const Location ekf_origin = sitl->state.home;
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if (ekf_origin.lat == 0 && ekf_origin.lng == 0) {
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return;
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}
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// more initialisation
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last_update_us = now_us;
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initialised = true;
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}
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// calculate dt and update tether forces
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const float dt = (now_us - last_update_us)*1.0e-6;
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last_update_us = now_us;
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update_tether_force(veh_pos, dt);
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// send tether location to GCS at 5hz
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// TO-Do: add provision to make the tether movable
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const uint32_t now_ms = AP_HAL::millis();
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if (now_ms - last_report_ms >= reporting_period_ms) {
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last_report_ms = now_ms;
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send_report();
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write_log();
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}
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}
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// get earth-frame forces on the vehicle from the tether
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// returns true on success and fills in forces_ef argument, false on failure
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bool TetherSim::get_forces_on_vehicle(Vector3f& forces_ef) const
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{
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if (!enable) {
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return false;
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}
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forces_ef = veh_forces_ef;
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return true;
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}
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// send a report to the vehicle control code over MAVLink
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void TetherSim::send_report(void)
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{
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if (!mavlink_connected && mav_socket.connect(target_address, target_port)) {
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::printf("Tether System connected to %s:%u\n", target_address, (unsigned)target_port);
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mavlink_connected = true;
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}
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if (!mavlink_connected) {
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return;
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}
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// get current time
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uint32_t now_ms = AP_HAL::millis();
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// send heartbeat at 1hz
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const uint8_t component_id = MAV_COMP_ID_USER11;
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if (now_ms - last_heartbeat_ms >= 1000) {
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last_heartbeat_ms = now_ms;
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const mavlink_heartbeat_t heartbeat{
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custom_mode: 0,
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type : MAV_TYPE_GROUND_ROVER,
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autopilot : MAV_AUTOPILOT_INVALID,
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base_mode: 0,
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system_status: 0,
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mavlink_version: 0,
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};
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mavlink_message_t msg;
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mavlink_msg_heartbeat_encode_status(
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sys_id.get(),
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component_id,
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&mav_status,
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&msg,
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&heartbeat);
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uint8_t buf[300];
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const uint16_t len = mavlink_msg_to_send_buffer(buf, &msg);
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mav_socket.send(buf, len);
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}
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// send a GLOBAL_POSITION_INT messages
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{
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Location tether_anchor_loc;
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int32_t alt_amsl_cm, alt_rel_cm;
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if (!get_tether_ground_location(tether_anchor_loc) ||
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!tether_anchor_loc.get_alt_cm(Location::AltFrame::ABSOLUTE, alt_amsl_cm) ||
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!tether_anchor_loc.get_alt_cm(Location::AltFrame::ABOVE_HOME, alt_rel_cm)) {
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return;
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}
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const mavlink_global_position_int_t global_position_int{
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time_boot_ms: now_ms,
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lat: tether_anchor_loc.lat,
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lon: tether_anchor_loc.lng,
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alt: alt_amsl_cm * 10, // amsl alt in mm
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relative_alt: alt_rel_cm * 10, // relative alt in mm
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vx: 0, // velocity in cm/s
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vy: 0, // velocity in cm/s
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vz: 0, // velocity in cm/s
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hdg: 0 // heading in centi-degrees
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};
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mavlink_message_t msg;
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mavlink_msg_global_position_int_encode_status(sys_id, component_id, &mav_status, &msg, &global_position_int);
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uint8_t buf[300];
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const uint16_t len = mavlink_msg_to_send_buffer(buf, &msg);
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if (len > 0) {
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mav_socket.send(buf, len);
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}
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}
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}
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void TetherSim::write_log()
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{
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#if HAL_LOGGING_ENABLED
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// write log of tether state
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// @LoggerMessage: TETH
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// @Description: Tether state
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// @Field: TimeUS: Time since system startup
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// @Field: Len: Tether length
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// @Field: VFN: Force on vehicle in North direction
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// @Field: VFE: Force on vehicle in East direction
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// @Field: VFD: Force on vehicle in Down direction
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AP::logger().WriteStreaming("TETH",
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"TimeUS,Len,VFN,VFE,VFD", // labels
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"s----", // units
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"F----", // multipliers
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"Qffff", // format
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AP_HAL::micros64(),
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(float)tether_length,
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(double)veh_forces_ef.x,
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(double)veh_forces_ef.y,
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(double)veh_forces_ef.z);
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#endif
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}
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// returns true on success and fills in tether_ground_loc argument, false on failure
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bool TetherSim::get_tether_ground_location(Location& tether_ground_loc) const
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{
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// get EKF origin
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auto *sitl = AP::sitl();
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if (sitl == nullptr) {
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return false;
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}
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const Location ekf_origin = sitl->state.home;
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if (ekf_origin.lat == 0 && ekf_origin.lng == 0) {
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return false;
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}
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tether_ground_loc = ekf_origin;
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return true;
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}
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void TetherSim::update_tether_force(const Location& veh_pos, float dt)
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{
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Location tether_anchor_loc;
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if (!get_tether_ground_location(tether_anchor_loc)) {
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return;
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}
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// Step 1: Calculate the vector from the tether anchor to the vehicle
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Vector3f tether_vector = veh_pos.get_distance_NED(tether_anchor_loc);
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tether_length = tether_vector.length();
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// Step 2: Check if tether is taut (length exceeds maximum allowed length) or stuck
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if (tether_length > max_line_length) {
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// Calculate the stretch beyond the maximum length
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float stretch = MAX(tether_length - max_line_length, 0.0f);
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// Apply a spring-like penalty force proportional to the stretch
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float penalty_force_magnitude = tether_spring_constant * stretch;
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// Direction of force is along the tether, pulling toward the anchor
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veh_forces_ef = tether_vector.normalized() * penalty_force_magnitude;
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GCS_SEND_TEXT(MAV_SEVERITY_WARNING, "Tether: Exceeded maximum length.");
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return;
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}
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if (tether_stuck) {
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// Calculate the stretch beyond the maximum length
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float stretch = MAX(tether_length - tether_not_stuck_length, 0.0f);
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// Apply a spring-like penalty force proportional to the stretch
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float penalty_force_magnitude = tether_spring_constant * stretch;
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// Direction of force is directly along the tether, towards the tether anchor point
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veh_forces_ef = tether_vector.normalized() * penalty_force_magnitude;
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GCS_SEND_TEXT(MAV_SEVERITY_WARNING, "Tether: Stuck.");
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return;
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} else {
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tether_not_stuck_length = tether_length;
|
||||||
|
}
|
||||||
|
|
||||||
|
// Step 3: Calculate the weight of the tether being lifted
|
||||||
|
// The weight is proportional to the current tether length
|
||||||
|
const float tether_weight_force = tether_linear_density * tether_length * GRAVITY_MSS;
|
||||||
|
|
||||||
|
// Step 4: Calculate the tension force
|
||||||
|
Vector3f tension_force_NED = tether_vector.normalized() * tether_weight_force;
|
||||||
|
|
||||||
|
// Step 5: Apply the force to the vehicle
|
||||||
|
veh_forces_ef = tension_force_NED;
|
||||||
|
}
|
||||||
|
|
||||||
|
#endif
|
|
@ -0,0 +1,95 @@
|
||||||
|
/*
|
||||||
|
This program is free software: you can redistribute it and/or modify
|
||||||
|
it under the terms of the GNU General Public License as published by
|
||||||
|
the Free Software Foundation, either version 3 of the License, or
|
||||||
|
(at your option) any later version.
|
||||||
|
|
||||||
|
This program is distributed in the hope that it will be useful,
|
||||||
|
but WITHOUT ANY WARRANTY; without even the implied warranty of
|
||||||
|
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
|
||||||
|
GNU General Public License for more details.
|
||||||
|
|
||||||
|
You should have received a copy of the GNU General Public License
|
||||||
|
along with this program. If not, see <http://www.gnu.org/licenses/>.
|
||||||
|
*/
|
||||||
|
|
||||||
|
/*
|
||||||
|
Simulate a tethered vehicle.
|
||||||
|
Models the forces exerted by the tether and reports them to the vehicle simulation. The dynamics are not accurate but provide a very rough approximation intended to test a "stuck tether".
|
||||||
|
*/
|
||||||
|
|
||||||
|
#pragma once
|
||||||
|
|
||||||
|
#include "SIM_config.h"
|
||||||
|
|
||||||
|
#if AP_SIM_TETHER_ENABLED
|
||||||
|
|
||||||
|
#include <AP_HAL/utility/Socket_native.h>
|
||||||
|
#include <AP_Math/AP_Math.h>
|
||||||
|
#include <AP_Common/Location.h>
|
||||||
|
#include <GCS_MAVLink/GCS_MAVLink.h>
|
||||||
|
|
||||||
|
namespace SITL {
|
||||||
|
|
||||||
|
// TetherSim simulates a tethered to a vehicle
|
||||||
|
class TetherSim {
|
||||||
|
public:
|
||||||
|
// constructor
|
||||||
|
TetherSim();
|
||||||
|
|
||||||
|
// Update the tether simulation state using the vehicle's earth-frame position
|
||||||
|
void update(const Location& veh_pos);
|
||||||
|
|
||||||
|
// Retrieve earth-frame forces on the vehicle due to the tether
|
||||||
|
// Returns true on success and fills in the forces_ef argument; false on failure
|
||||||
|
bool get_forces_on_vehicle(Vector3f& forces_ef) const;
|
||||||
|
|
||||||
|
// Parameter table for configuration
|
||||||
|
static const struct AP_Param::GroupInfo var_info[];
|
||||||
|
|
||||||
|
private:
|
||||||
|
// Parameters
|
||||||
|
AP_Int8 enable; // Enable or disable the tether simulation
|
||||||
|
AP_Float tether_linear_density; // Linear mass density of the tether in kg/m
|
||||||
|
AP_Float max_line_length; // Maximum allowed tether length in meters
|
||||||
|
AP_Int8 sys_id; // MAVLink system ID for GCS reporting
|
||||||
|
AP_Int8 tether_stuck; // Set to 1 to simulate a stuck tether
|
||||||
|
AP_Float tether_spring_constant; // Spring constant for modeling tether stretch
|
||||||
|
|
||||||
|
// Send MAVLink messages to the GCS
|
||||||
|
void send_report();
|
||||||
|
|
||||||
|
// Write tether simulation state to onboard log
|
||||||
|
void write_log();
|
||||||
|
|
||||||
|
// Retrieve the location of the tether anchor point on the ground
|
||||||
|
// Returns true on success and fills in the tether_anchor_loc argument; false on failure
|
||||||
|
bool get_tether_ground_location(Location& tether_anchor_loc) const;
|
||||||
|
|
||||||
|
// Update forces exerted by the tether based on the vehicle's position
|
||||||
|
// Takes the vehicle's position and the simulation time step (dt) as inputs
|
||||||
|
void update_tether_force(const Location& veh_pos, float dt);
|
||||||
|
|
||||||
|
// Socket connection variables for MAVLink communication
|
||||||
|
const char *target_address = "127.0.0.1"; // Address for MAVLink socket communication
|
||||||
|
const uint16_t target_port = 5763; // Port for MAVLink socket communication
|
||||||
|
SocketAPM_native mav_socket { false }; // Socket for MAVLink communication
|
||||||
|
bool initialised; // True if the simulation class is initialized
|
||||||
|
uint32_t last_update_us; // Timestamp of the last update in microseconds
|
||||||
|
|
||||||
|
// MAVLink reporting variables
|
||||||
|
const float reporting_period_ms = 100; // Reporting period in milliseconds
|
||||||
|
uint32_t last_report_ms; // Timestamp of the last MAVLink report sent to GCS
|
||||||
|
uint32_t last_heartbeat_ms; // Timestamp of the last MAVLink heartbeat sent to GCS
|
||||||
|
bool mavlink_connected; // True if MAVLink connection is established
|
||||||
|
mavlink_status_t mav_status; // Status of MAVLink communication
|
||||||
|
|
||||||
|
// Tether simulation variables
|
||||||
|
Vector3f veh_forces_ef; // Earth-frame forces on the vehicle due to the tether
|
||||||
|
float tether_length = 0.0f; // Current tether length in meters
|
||||||
|
float tether_not_stuck_length = 0.0f; // Tether length when the tether is not stuck
|
||||||
|
};
|
||||||
|
|
||||||
|
} // namespace SITL
|
||||||
|
|
||||||
|
#endif // AP_SIM_TETHER_ENABLED
|
|
@ -57,6 +57,10 @@
|
||||||
#define AP_SIM_SLUNGPAYLOAD_ENABLED (CONFIG_HAL_BOARD == HAL_BOARD_SITL)
|
#define AP_SIM_SLUNGPAYLOAD_ENABLED (CONFIG_HAL_BOARD == HAL_BOARD_SITL)
|
||||||
#endif
|
#endif
|
||||||
|
|
||||||
|
#ifndef AP_SIM_TETHER_ENABLED
|
||||||
|
#define AP_SIM_TETHER_ENABLED (CONFIG_HAL_BOARD == HAL_BOARD_SITL)
|
||||||
|
#endif
|
||||||
|
|
||||||
#ifndef AP_SIM_FLIGHTAXIS_ENABLED
|
#ifndef AP_SIM_FLIGHTAXIS_ENABLED
|
||||||
#define AP_SIM_FLIGHTAXIS_ENABLED (CONFIG_HAL_BOARD == HAL_BOARD_SITL)
|
#define AP_SIM_FLIGHTAXIS_ENABLED (CONFIG_HAL_BOARD == HAL_BOARD_SITL)
|
||||||
#endif
|
#endif
|
||||||
|
|
|
@ -1367,6 +1367,12 @@ const AP_Param::GroupInfo SIM::ModelParm::var_info[] = {
|
||||||
AP_SUBGROUPPTR(flightaxis_ptr, "RFL_", 5, SIM::ModelParm, FlightAxis),
|
AP_SUBGROUPPTR(flightaxis_ptr, "RFL_", 5, SIM::ModelParm, FlightAxis),
|
||||||
#endif
|
#endif
|
||||||
|
|
||||||
|
#if AP_SIM_TETHER_ENABLED
|
||||||
|
// @Group: TETH_
|
||||||
|
// @Path: ./SIM_Tether.cpp
|
||||||
|
AP_SUBGROUPINFO(tether_sim, "TETH_", 6, SIM::ModelParm, TetherSim),
|
||||||
|
#endif
|
||||||
|
|
||||||
AP_GROUPEND
|
AP_GROUPEND
|
||||||
};
|
};
|
||||||
|
|
||||||
|
|
|
@ -28,6 +28,7 @@
|
||||||
#include "SIM_IntelligentEnergy24.h"
|
#include "SIM_IntelligentEnergy24.h"
|
||||||
#include "SIM_Ship.h"
|
#include "SIM_Ship.h"
|
||||||
#include "SIM_SlungPayload.h"
|
#include "SIM_SlungPayload.h"
|
||||||
|
#include "SIM_Tether.h"
|
||||||
#include "SIM_GPS.h"
|
#include "SIM_GPS.h"
|
||||||
#include "SIM_DroneCANDevice.h"
|
#include "SIM_DroneCANDevice.h"
|
||||||
#include "SIM_ADSB_Sagetech_MXS.h"
|
#include "SIM_ADSB_Sagetech_MXS.h"
|
||||||
|
@ -338,6 +339,9 @@ public:
|
||||||
#if AP_SIM_SLUNGPAYLOAD_ENABLED
|
#if AP_SIM_SLUNGPAYLOAD_ENABLED
|
||||||
SlungPayloadSim slung_payload_sim;
|
SlungPayloadSim slung_payload_sim;
|
||||||
#endif
|
#endif
|
||||||
|
#if AP_SIM_TETHER_ENABLED
|
||||||
|
TetherSim tether_sim;
|
||||||
|
#endif
|
||||||
#if AP_SIM_FLIGHTAXIS_ENABLED
|
#if AP_SIM_FLIGHTAXIS_ENABLED
|
||||||
FlightAxis *flightaxis_ptr;
|
FlightAxis *flightaxis_ptr;
|
||||||
#endif
|
#endif
|
||||||
|
|
Loading…
Reference in New Issue