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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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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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antenna-tracker simulator class
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*/ |
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#include "SIM_Tracker.h" |
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#if CONFIG_HAL_BOARD == HAL_BOARD_SITL |
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#include <stdio.h> |
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Tracker::Tracker(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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/*
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update function for position (normal) servos. |
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*/ |
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void Tracker::update_position_servos(float delta_time, float &yaw_rate, float &pitch_rate) |
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{ |
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float pitch_target = zero_pitch + pitch_input*pitch_range; |
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float yaw_target = zero_yaw + yaw_input*yaw_range; |
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while (yaw_target > 180) { |
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yaw_target -= 360; |
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} |
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float r, p, y; |
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dcm.to_euler(&r, &p, &y); |
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float pitch_current = degrees(p); |
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float yaw_current = degrees(y); |
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pitch_rate = constrain_float(pitch_target - pitch_current, -pitchrate, pitchrate); |
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float yaw_diff = yaw_target - yaw_current; |
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if (yaw_diff > 180) { |
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yaw_diff -= 360; |
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} |
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if (yaw_diff < -180) { |
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yaw_diff += 360; |
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} |
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yaw_rate = constrain_float(yaw_diff, -yawrate, yawrate); |
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} |
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|
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/*
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update function for onoff servos. |
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These servos either move at a constant rate or are still
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Returns (yaw_rate,pitch_rate) tuple |
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*/ |
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void Tracker::update_onoff_servos(float &yaw_rate, float &pitch_rate) |
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{ |
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if (fabsf(yaw_input) < 0.1) { |
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yaw_rate = 0; |
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} else if (yaw_input >= 0.1) { |
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yaw_rate = yawrate; |
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} else { |
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yaw_rate = -yawrate; |
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} |
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if (fabsf(pitch_input) < 0.1) { |
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pitch_rate = 0; |
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} else if (pitch_input >= 0.1) { |
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pitch_rate = pitchrate; |
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} else { |
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pitch_rate = -pitchrate; |
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} |
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} |
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|
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/*
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update state of tracker |
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*/ |
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void Tracker::update(const struct sitl_input &input) |
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{ |
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// how much time has passed?
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float delta_time = frame_time_us * 1.0e-6f; |
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float yaw_rate, pitch_rate; |
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yaw_input = (input.servos[0]-1500)/500.0f; |
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pitch_input = (input.servos[1]-1500)/500.0f; |
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if (onoff) { |
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update_onoff_servos(yaw_rate, pitch_rate); |
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} else { |
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update_position_servos(delta_time, yaw_rate, pitch_rate); |
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} |
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// implement yaw and pitch limits
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float r, p, y; |
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dcm.to_euler(&r, &p, &y); |
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float pitch_current_relative = degrees(p) - zero_pitch; |
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float yaw_current_relative = degrees(y) - zero_yaw; |
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float roll_current = degrees(r); |
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if (yaw_current_relative > 180) { |
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yaw_current_relative -= 360; |
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} |
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if (yaw_current_relative < -180) { |
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yaw_current_relative += 360; |
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} |
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if (yaw_rate > 0 && yaw_current_relative >= yaw_range) { |
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yaw_rate = 0; |
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} |
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if (yaw_rate < 0 && yaw_current_relative <= -yaw_range) { |
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yaw_rate = 0; |
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} |
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if (pitch_rate > 0 && pitch_current_relative >= pitch_range) { |
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pitch_rate = 0; |
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} |
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if (pitch_rate < 0 && pitch_current_relative <= -pitch_range) { |
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pitch_rate = 0; |
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} |
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// keep it level
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float roll_rate = 0 - roll_current; |
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if (time_now_us - last_debug_us > 2e6f && !onoff) { |
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last_debug_us = time_now_us; |
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printf("roll=%.1f pitch=%.1f yaw=%.1f rates=%.1f/%.1f/%.1f in=%.3f,%.3f\n", |
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roll_current, |
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pitch_current_relative,
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yaw_current_relative,
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roll_rate, pitch_rate, yaw_rate, |
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yaw_input, pitch_input); |
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} |
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gyro = Vector3f(radians(roll_rate),radians(pitch_rate),radians(yaw_rate)); |
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// update attitude
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dcm.rotate(gyro * delta_time); |
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dcm.normalize(); |
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Vector3f accel_earth = Vector3f(0, 0, -GRAVITY_MSS); |
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accel_body = dcm.transposed() * accel_earth; |
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// new velocity vector
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velocity_ef.zero(); |
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update_position(); |
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} |
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#endif |
@ -0,0 +1,58 @@
@@ -0,0 +1,58 @@
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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, |
||||
but WITHOUT ANY WARRANTY; without even the implied warranty of |
||||
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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antenna-tracker simulator class |
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*/ |
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#ifndef _SIM_TRACKER_H |
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#define _SIM_TRACKER_H |
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#include "SIM_Aircraft.h" |
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/*
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a antenna tracker simulator |
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*/ |
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class Tracker : public Aircraft |
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{ |
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public: |
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Tracker(const char *home_str, const char *frame_str); |
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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 Tracker(home_str, frame_str); |
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} |
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private: |
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const bool onoff = false; |
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const float yawrate = 9.0f; |
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const float pitchrate = 1.0f; |
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const float pitch_range = 45; |
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const float yaw_range = 170; |
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const float zero_yaw = 0; // yaw direction at startup
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const float zero_pitch = 0; // pitch at startup
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bool verbose = false; |
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uint64_t last_debug_us = 0; |
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float pitch_input; |
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float yaw_input; |
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void update_position_servos(float delta_time, float &yaw_rate, float &pitch_rate); |
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void update_onoff_servos(float &yaw_rate, float &pitch_rate); |
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}; |
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#endif |
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