Andrew Tridgell
9 years ago
2 changed files with 147 additions and 0 deletions
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/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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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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singlecopter simulator class
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*/ |
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#include "SIM_SingleCopter.h" |
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#include <stdio.h> |
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using namespace SITL; |
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SingleCopter::SingleCopter(const char *home_str, const char *frame_str) : |
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Aircraft(home_str, frame_str) |
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{ |
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mass = 2.0f; |
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/*
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scaling from motor power to Newtons. Allows the copter |
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to hover against gravity when the motor is at hover_throttle |
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*/ |
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thrust_scale = (mass * GRAVITY_MSS) / hover_throttle; |
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frame_height = 0.1; |
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} |
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/*
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update the copter simulation by one time step |
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*/ |
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void SingleCopter::update(const struct sitl_input &input) |
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{ |
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// get wind vector setup
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update_wind(input); |
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float actuator[4]; |
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for (uint8_t i=0; i<4; i++) { |
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actuator[i] = constrain_float((input.servos[i]-1500) / 500.0f, -1, 1); |
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} |
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float thrust = constrain_float((input.servos[4]-1000) / 1000.0f, 0, 1); |
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float yaw_thrust = (actuator[0] + actuator[1] + actuator[2] + actuator[3]) * 0.25f * thrust; |
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float roll_thrust = (actuator[0] - actuator[2]) * 0.5f * thrust; |
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float pitch_thrust = (actuator[1] - actuator[3]) * 0.5f * thrust; |
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float torque_effect_accel = thrust * rotor_rot_accel; |
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// rotational acceleration, in rad/s/s, in body frame
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Vector3f rot_accel(roll_thrust * roll_rate_max, |
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pitch_thrust * pitch_rate_max, |
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yaw_thrust * yaw_rate_max + torque_effect_accel); |
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// rotational air resistance
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rot_accel.x -= gyro.x * radians(5000.0) / terminal_rotation_rate; |
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rot_accel.y -= gyro.y * radians(5000.0) / terminal_rotation_rate; |
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rot_accel.z -= gyro.z * radians(400.0) / terminal_rotation_rate; |
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// air resistance
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Vector3f air_resistance = -velocity_air_ef * (GRAVITY_MSS/terminal_velocity); |
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// scale thrust to newtons
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thrust *= thrust_scale; |
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accel_body = Vector3f(0, 0, -thrust / mass); |
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accel_body += dcm * air_resistance; |
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bool was_on_ground = on_ground(position); |
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update_dynamics(rot_accel); |
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// constrain height to the ground
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if (on_ground(position) && !was_on_ground) { |
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// zero roll/pitch, but keep yaw
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float r, p, y; |
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dcm.to_euler(&r, &p, &y); |
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dcm.from_euler(0, 0, y); |
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position.z = -(ground_level + frame_height - home.alt*0.01f); |
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velocity_ef.zero(); |
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} |
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// update lat/lon/altitude
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update_position(); |
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} |
@ -0,0 +1,53 @@ |
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/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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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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|
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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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|
|
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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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single copter simulator class |
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*/ |
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#pragma once |
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#include "SIM_Aircraft.h" |
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#include <AP_Motors/AP_Motors.h> |
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namespace SITL { |
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/*
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a single copter simulator |
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*/ |
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class SingleCopter : public Aircraft { |
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public: |
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SingleCopter(const char *home_str, const char *frame_str); |
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/* update model by one time step */ |
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void update(const struct sitl_input &input); |
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/* static object creator */ |
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static Aircraft *create(const char *home_str, const char *frame_str) { |
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return new SingleCopter(home_str, frame_str); |
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} |
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private: |
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float terminal_rotation_rate = 4*radians(360.0f); |
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float hover_throttle = 0.65f; |
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float terminal_velocity = 40; |
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float rotor_rot_accel = radians(20) * AP_MOTORS_MATRIX_YAW_FACTOR_CW; |
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float roll_rate_max = radians(700); |
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float pitch_rate_max = radians(700); |
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float yaw_rate_max = radians(700); |
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float thrust_scale; |
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}; |
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} // namespace SITL
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