mirror of https://github.com/ArduPilot/ardupilot
AntennaTracker: fixed ballerina and more accurate tracking
implement new parameter options
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262f8b9f48
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3a3a074fab
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@ -106,6 +106,7 @@ static struct {
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float altitude_difference;
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} nav_status;
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static uint32_t start_time_ms;
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////////////////////////////////////////////////////////////////////////////////
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// prototypes
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@ -73,14 +73,24 @@ static void init_tracker()
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channel_yaw.calc_pwm();
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channel_pitch.calc_pwm();
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current_loc = get_home_eeprom(); // GPS may update this later
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// use given start positions - useful for indoor testing, and
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// while waiting for GPS lock
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current_loc.lat = g.start_latitude * 1.0e7f;
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current_loc.lng = g.start_longitude * 1.0e7f;
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arm_servos();
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// see if EEPROM has a default location as well
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get_home_eeprom(current_loc);
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gcs_send_text_P(SEVERITY_LOW,PSTR("\nReady to track."));
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hal.scheduler->delay(1000); // Why????
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set_mode(AUTO); // tracking
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if (g.startup_delay > 0) {
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// arm servos with trim value to allow them to start up (required
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// for some servos)
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prepare_servos();
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}
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}
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// Level the tracker by calibrating the INS
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@ -127,31 +137,30 @@ static uint32_t map_baudrate(int8_t rate, uint32_t default_baud)
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/*
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fetch HOME from EEPROM
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*/
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static struct Location get_home_eeprom()
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static bool get_home_eeprom(struct Location &loc)
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{
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struct Location temp;
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uint16_t mem;
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// Find out proper location in memory by using the start_byte position + the index
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// --------------------------------------------------------------------------------
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if (g.command_total.get() == 0) {
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memset(&temp, 0, sizeof(temp));
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}else{
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// read WP position
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mem = WP_START_BYTE;
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temp.options = hal.storage->read_byte(mem);
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mem++;
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temp.alt = hal.storage->read_dword(mem);
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mem += 4;
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temp.lat = hal.storage->read_dword(mem);
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mem += 4;
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temp.lng = hal.storage->read_dword(mem);
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return false;
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}
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return temp;
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// read WP position
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mem = WP_START_BYTE;
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loc.options = hal.storage->read_byte(mem);
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mem++;
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loc.alt = hal.storage->read_dword(mem);
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mem += 4;
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loc.lat = hal.storage->read_dword(mem);
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mem += 4;
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loc.lng = hal.storage->read_dword(mem);
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return true;
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}
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static void set_home_eeprom(struct Location temp)
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@ -182,7 +191,7 @@ static void set_home(struct Location temp)
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}
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static void arm_servos()
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{
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{
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channel_yaw.enable_out();
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channel_pitch.enable_out();
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}
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@ -193,6 +202,18 @@ static void disarm_servos()
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channel_pitch.disable_out();
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}
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/*
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setup servos to trim value after initialising
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*/
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static void prepare_servos()
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{
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start_time_ms = hal.scheduler->millis();
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channel_yaw.radio_out = channel_yaw.radio_trim;
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channel_pitch.radio_out = channel_pitch.radio_trim;
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channel_yaw.output();
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channel_pitch.output();
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}
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static void set_mode(enum ControlMode mode)
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{
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if(control_mode == mode) {
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@ -200,5 +221,17 @@ static void set_mode(enum ControlMode mode)
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return;
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}
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control_mode = mode;
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switch (control_mode) {
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case AUTO:
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case MANUAL:
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arm_servos();
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break;
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case STOP:
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case INITIALISING:
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disarm_servos();
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break;
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}
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}
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@ -41,6 +41,18 @@ static void update_pitch_servo(float pitch)
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// PITCH2SRV_IMAX 4000.000000
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int32_t new_servo_out = channel_pitch.servo_out - g.pidPitch2Srv.get_pid(err);
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channel_pitch.servo_out = constrain_float(new_servo_out, -9000, 9000);
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// add slew rate limit
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if (g.pitch_slew_time > 0.02f) {
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uint16_t max_change = 0.02f * 18000 / g.yaw_slew_time;
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if (max_change < 1) {
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max_change = 1;
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}
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new_servo_out = constrain_float(new_servo_out,
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channel_yaw.servo_out - max_change,
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channel_yaw.servo_out + max_change);
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}
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channel_pitch.calc_pwm();
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channel_pitch.output();
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}
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@ -93,14 +105,25 @@ static void update_yaw_servo(float yaw)
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Use our current yawspeed to determine if we are moving in the
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right direction
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*/
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static int8_t slew_dir = 0;
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static int8_t slew_dir;
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static uint32_t slew_start_ms;
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int8_t new_slew_dir = slew_dir;
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Vector3f omega = ahrs.get_gyro();
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if (abs(channel_yaw.servo_out) == 18000 && abs(err) > margin && err * omega.z >= 0) {
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Vector3f earth_rotation = ahrs.get_gyro() * ahrs.get_dcm_matrix();
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bool making_progress;
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if (slew_dir != 0) {
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making_progress = (-slew_dir * earth_rotation.z >= 0);
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} else {
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making_progress = (err * earth_rotation.z >= 0);
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}
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if (abs(channel_yaw.servo_out) == 18000 &&
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abs(err) > margin &&
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making_progress &&
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hal.scheduler->millis() - slew_start_ms > g.min_reverse_time*1000) {
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// we are at the limit of the servo and are not moving in the
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// right direction, so slew the other way
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new_slew_dir = -channel_yaw.servo_out / 18000;
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slew_start_ms = hal.scheduler->millis();
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}
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/*
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@ -111,10 +134,13 @@ static void update_yaw_servo(float yaw)
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new_slew_dir = 0;
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}
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#if 0
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::printf("err=%d slew_dir=%d new_slew_dir=%d servo=%d\n",
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err, slew_dir, new_slew_dir, channel_yaw.servo_out);
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#endif
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if (new_slew_dir != slew_dir) {
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gcs_send_text_fmt(PSTR("SLEW: %d/%d err=%ld servo=%ld ez=%.3f"),
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(int)slew_dir, (int)new_slew_dir,
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(long)err,
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(long)channel_yaw.servo_out,
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degrees(ahrs.get_gyro().z));
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}
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slew_dir = new_slew_dir;
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@ -128,28 +154,50 @@ static void update_yaw_servo(float yaw)
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new_servo_out = constrain_float(channel_yaw.servo_out - servo_change, -18000, 18000);
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}
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if (new_servo_out - channel_yaw.servo_out > 100) {
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new_servo_out = channel_yaw.servo_out + 100;
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} else if (new_servo_out - channel_yaw.servo_out < -100) {
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new_servo_out = channel_yaw.servo_out - 100;
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// add slew rate limit
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if (g.yaw_slew_time > 0.02f) {
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uint16_t max_change = 0.02f * 36000.0f / g.yaw_slew_time;
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if (max_change < 1) {
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max_change = 1;
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}
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new_servo_out = constrain_float(new_servo_out,
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channel_yaw.servo_out - max_change,
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channel_yaw.servo_out + max_change);
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}
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channel_yaw.servo_out = new_servo_out;
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{
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// Normal tracking
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// You will need to tune the yaw PID to suit your antenna and servos
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// For my servos, suitable PID settings are:
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// param set YAW2SRV_P 0.1
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// param set YAW2SRV_I 0.05
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// param set YAW2SRV_D 0
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// param set YAW2SRV_IMAX 4000
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}
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channel_yaw.calc_pwm();
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channel_yaw.output();
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}
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/*
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control servos for AUTO mode
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*/
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static void update_auto(void)
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{
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if (g.startup_delay > 0 &&
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hal.scheduler->millis() - start_time_ms < g.startup_delay*1000) {
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return;
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}
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update_pitch_servo(nav_status.pitch);
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update_yaw_servo(nav_status.bearing);
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}
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/*
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control servos for MANUAL mode
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*/
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static void update_manual(void)
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{
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channel_yaw.radio_out = channel_yaw.radio_in;
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channel_pitch.radio_out = channel_pitch.radio_in;
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channel_yaw.output();
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channel_pitch.output();
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}
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/**
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main antenna tracking code, called at 50Hz
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*/
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@ -169,23 +217,29 @@ static void update_tracking(void)
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current_loc.options = 0; // Absolute altitude
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}
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if (control_mode == AUTO)
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{
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// calculate the bearing to the vehicle
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float bearing = get_bearing_cd(current_loc, vehicle.location) * 0.01f;
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float distance = get_distance(current_loc, vehicle.location);
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float pitch = degrees(atan2f(nav_status.altitude_difference, distance));
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// calculate the bearing to the vehicle
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float bearing = get_bearing_cd(current_loc, vehicle.location) * 0.01f;
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float distance = get_distance(current_loc, vehicle.location);
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float pitch = degrees(atan2f(nav_status.altitude_difference, distance));
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// update the servos
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update_pitch_servo(pitch);
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update_yaw_servo(bearing);
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// update nav_status for NAV_CONTROLLER_OUTPUT
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nav_status.bearing = bearing;
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nav_status.pitch = pitch;
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nav_status.distance = distance;
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// update nav_status for NAV_CONTROLLER_OUTPUT
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nav_status.bearing = bearing;
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nav_status.pitch = pitch;
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nav_status.distance = distance;
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switch (control_mode) {
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case AUTO:
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update_auto();
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break;
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case MANUAL:
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update_manual();
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break;
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case STOP:
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case INITIALISING:
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break;
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}
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}
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/**
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