2011-03-19 07:20:11 -03:00
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// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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2010-12-19 12:40:33 -04:00
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//****************************************************************
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// Function that will calculate the desired direction to fly and distance
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//****************************************************************
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void navigate()
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{
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// do not navigate with corrupt data
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// ---------------------------------
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2011-02-24 01:56:59 -04:00
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if (g_gps->fix == 0){
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2011-02-17 05:36:33 -04:00
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g_gps->new_data = false;
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2010-12-19 12:40:33 -04:00
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return;
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}
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2011-02-17 05:36:33 -04:00
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2010-12-19 12:40:33 -04:00
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if(next_WP.lat == 0){
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return;
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}
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2011-02-17 05:36:33 -04:00
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2011-01-11 17:15:08 -04:00
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// waypoint distance from plane
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// ----------------------------
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2011-03-02 22:32:50 -04:00
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wp_distance = get_distance(¤t_loc, &next_WP);
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2011-01-11 17:15:08 -04:00
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2011-02-24 01:56:59 -04:00
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if (wp_distance < 0){
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2011-03-19 07:14:15 -03:00
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gcs.send_text_P(SEVERITY_HIGH,PSTR("<navigate> WP error - distance < 0"));
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2011-01-11 17:15:08 -04:00
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//Serial.println(wp_distance,DEC);
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//print_current_waypoints();
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return;
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}
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2011-02-17 05:36:33 -04:00
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// target_bearing is where we should be heading
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2011-01-11 17:15:08 -04:00
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// --------------------------------------------
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target_bearing = get_bearing(¤t_loc, &next_WP);
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2011-02-24 01:56:59 -04:00
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// nav_bearing will includes xtrac correction
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// ------------------------------------------
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2011-01-11 17:15:08 -04:00
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nav_bearing = target_bearing;
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2011-04-25 02:12:59 -03:00
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}
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2011-02-24 01:56:59 -04:00
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2011-04-25 02:12:59 -03:00
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bool check_missed_wp()
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{
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long temp = target_bearing - saved_target_bearing;
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temp = wrap_180(temp);
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return (abs(temp) > 10000); //we pased the waypoint by 10 °
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2011-01-11 17:15:08 -04:00
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}
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2010-12-19 12:40:33 -04:00
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2011-07-10 21:47:08 -03:00
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int
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get_nav_throttle(long error)
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{
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int throttle;
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// limit error
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throttle = g.pid_throttle.get_pid(error, delta_ms_medium_loop, 1.0);
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throttle = g.throttle_cruise + constrain(throttle, -80, 80);
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//int tem = alt_hold_velocity();
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//throttle -= tem;
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return throttle;
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}
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2011-05-27 15:21:55 -03:00
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#define DIST_ERROR_MAX 1800
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2011-03-14 03:04:07 -03:00
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void calc_loiter_nav()
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2011-01-11 17:15:08 -04:00
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{
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/*
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Becuase we are using lat and lon to do our distance errors here's a quick chart:
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100 = 1m
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2011-05-20 02:23:12 -03:00
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1000 = 11m = 36 feet
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2011-04-16 17:44:23 -03:00
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1800 = 19.80m = 60 feet
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2011-01-12 21:31:05 -04:00
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3000 = 33m
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2011-01-11 17:15:08 -04:00
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10000 = 111m
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pitch_max = 22° (2200)
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2011-02-17 05:36:33 -04:00
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*/
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2011-04-25 02:12:59 -03:00
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2011-04-16 17:44:23 -03:00
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// X ROLL
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long_error = (float)(next_WP.lng - current_loc.lng) * scaleLongDown; // 500 - 0 = 500 roll EAST
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// Y PITCH
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lat_error = current_loc.lat - next_WP.lat; // 0 - 500 = -500 pitch NORTH
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2011-01-12 21:31:05 -04:00
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2011-07-02 19:44:59 -03:00
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// constrain input, not output to let I term ramp up and do it's job again wind
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long_error = constrain(long_error, -loiter_error_max, loiter_error_max); // +- 20m max error
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lat_error = constrain(lat_error, -loiter_error_max, loiter_error_max); // +- 20m max error
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2011-02-17 05:36:33 -04:00
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2011-05-20 02:23:12 -03:00
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nav_lon = g.pid_nav_lon.get_pid(long_error, dTnav, 1.0); // X 700 * 2.5 = 1750,
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nav_lat = g.pid_nav_lat.get_pid(lat_error, dTnav, 1.0); // Y invert lat (for pitch)
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2011-05-16 01:59:06 -03:00
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}
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2011-04-16 17:44:23 -03:00
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2011-05-16 01:59:06 -03:00
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void calc_loiter_output()
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{
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2011-02-17 05:36:33 -04:00
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// rotate the vector
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2011-04-16 17:44:23 -03:00
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nav_roll = (float)nav_lon * sin_yaw_y - (float)nav_lat * -cos_yaw_x;
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// BAD
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//NORTH -1000 * 1 - 1000 * 0 = -1000 // roll left
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//WEST -1000 * 0 - 1000 * -1 = 1000 // roll right - Backwards
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//EAST -1000 * 0 - 1000 * 1 = -1000 // roll left - Backwards
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//SOUTH -1000 * -1 - 1000 * 0 = 1000 // roll right
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// GOOD
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//NORTH -1000 * 1 - 1000 * 0 = -1000 // roll left
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//WEST -1000 * 0 - 1000 * 1 = -1000 // roll right
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//EAST -1000 * 0 - 1000 * -1 = 1000 // roll left
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//SOUTH -1000 * -1 - 1000 * 0 = 1000 // roll right
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nav_pitch = ((float)nav_lon * -cos_yaw_x + (float)nav_lat * sin_yaw_y);
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// BAD
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//NORTH -1000 * 0 + 1000 * 1 = 1000 // pitch back
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//WEST -1000 * -1 + 1000 * 0 = 1000 // pitch back - Backwards
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//EAST -1000 * 1 + 1000 * 0 = -1000 // pitch forward - Backwards
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//SOUTH -1000 * 0 + 1000 * -1 = -1000 // pitch forward
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// GOOD
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//NORTH -1000 * 0 + 1000 * 1 = 1000 // pitch back
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//WEST -1000 * 1 + 1000 * 0 = -1000 // pitch forward
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//EAST -1000 * -1 + 1000 * 0 = 1000 // pitch back
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//SOUTH -1000 * 0 + 1000 * -1 = -1000 // pitch forward
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2010-12-19 12:40:33 -04:00
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}
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2011-04-25 02:12:59 -03:00
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void calc_simple_nav()
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2011-03-14 03:04:07 -03:00
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{
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2011-04-25 02:12:59 -03:00
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// no dampening here in SIMPLE mode
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2011-07-02 19:44:59 -03:00
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nav_lat = constrain((wp_distance * 100), -4500, 4500); // +- 20m max error
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2011-04-25 02:12:59 -03:00
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// Scale response by kP
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2011-07-02 19:44:59 -03:00
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//nav_lat *= g.pid_nav_lat.kP(); // 1800 * 2 = 3600 or 36°
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2011-04-25 02:12:59 -03:00
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}
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2011-04-27 02:08:24 -03:00
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void calc_nav_output()
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{
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// get the sin and cos of the bearing error - rotated 90°
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2011-06-27 14:01:53 -03:00
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float sin_nav_y = sin(radians((float)(9000 - bearing_error) / 100));
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float cos_nav_x = cos(radians((float)(bearing_error - 9000) / 100));
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2011-04-27 02:08:24 -03:00
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// rotate the vector
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nav_roll = (float)nav_lat * cos_nav_x;
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nav_pitch = -(float)nav_lat * sin_nav_y;
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}
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2011-04-30 13:01:57 -03:00
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2011-04-25 02:12:59 -03:00
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// called after we get GPS read
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2011-04-27 02:08:24 -03:00
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void calc_rate_nav()
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2011-04-25 02:12:59 -03:00
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{
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// which direction are we moving?
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long target_error = target_bearing - g_gps->ground_course;
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target_error = wrap_180(target_error);
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2011-05-16 01:59:06 -03:00
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// calc the cos of the error to tell how fast we are moving towards the target in cm
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2011-05-05 02:19:45 -03:00
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int groundspeed = (float)g_gps->ground_speed * cos(radians((float)target_error/100));
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2011-07-10 21:47:08 -03:00
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// Reduce speed on RTL
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if(control_mode == RTL){
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waypoint_speed = min((wp_distance * 100), 600);
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waypoint_speed = max(g.waypoint_speed_max.get(), 30);
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}else{
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waypoint_speed = g.waypoint_speed_max.get();
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}
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int error = constrain(waypoint_speed - groundspeed, -1000, 1000);
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2011-04-25 02:12:59 -03:00
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// Scale response by kP
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2011-05-31 02:29:06 -03:00
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nav_lat = nav_lat + g.pid_nav_wp.get_pid(error, dTnav, 1.0);
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nav_lat >>= 1; // divide by two
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2011-05-18 20:38:24 -03:00
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2011-05-31 02:29:06 -03:00
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//Serial.printf("dTnav: %ld, gs: %d, err: %d, int: %d, pitch: %ld", dTnav, groundspeed, error, (int)g.pid_nav_wp.get_integrator(), (long)nav_lat);
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2011-04-25 02:12:59 -03:00
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// limit our output
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2011-05-16 01:59:06 -03:00
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nav_lat = constrain(nav_lat, -4000, 4000); // +- max error
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2011-03-14 03:04:07 -03:00
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}
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2010-12-19 12:40:33 -04:00
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void calc_bearing_error()
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{
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2011-01-25 01:53:36 -04:00
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bearing_error = nav_bearing - dcm.yaw_sensor;
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2010-12-19 12:40:33 -04:00
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bearing_error = wrap_180(bearing_error);
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}
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2011-02-17 05:36:33 -04:00
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void calc_altitude_error()
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2010-12-19 12:40:33 -04:00
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{
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2011-03-09 02:37:09 -04:00
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altitude_error = next_WP.alt - current_loc.alt;
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}
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void calc_altitude_smoothing_error()
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{
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// limit climb rates - we draw a straight line between first location and edge of waypoint_radius
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target_altitude = next_WP.alt - ((wp_distance * (next_WP.alt - prev_WP.alt)) / (wp_totalDistance - g.waypoint_radius));
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2011-03-05 01:12:16 -04:00
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2011-03-09 02:37:09 -04:00
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// stay within a certain range
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if(prev_WP.alt > next_WP.alt){
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target_altitude = constrain(target_altitude, next_WP.alt, prev_WP.alt);
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2011-03-05 00:56:58 -04:00
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}else{
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2011-03-09 02:37:09 -04:00
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target_altitude = constrain(target_altitude, prev_WP.alt, next_WP.alt);
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2011-01-21 01:28:01 -04:00
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}
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2010-12-19 12:40:33 -04:00
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2011-01-21 01:28:01 -04:00
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altitude_error = target_altitude - current_loc.alt;
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2010-12-19 12:40:33 -04:00
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}
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long wrap_360(long error)
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{
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if (error > 36000) error -= 36000;
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if (error < 0) error += 36000;
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return error;
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}
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long wrap_180(long error)
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{
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if (error > 18000) error -= 36000;
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if (error < -18000) error += 36000;
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return error;
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}
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void update_crosstrack(void)
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{
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// Crosstrack Error
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// ----------------
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2011-05-31 02:29:06 -03:00
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if (cross_track_test() < 9000) { // If we are too far off or too close we don't do track following
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2010-12-19 12:40:33 -04:00
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crosstrack_error = sin(radians((target_bearing - crosstrack_bearing) / 100)) * wp_distance; // Meters we are off track line
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2011-07-10 21:47:08 -03:00
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long xtrack = g.pid_crosstrack.get_pid(crosstrack_error, dTnav, 1.0) * 100;
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nav_bearing += constrain(xtrack, -g.crosstrack_entry_angle.get(), g.crosstrack_entry_angle.get());
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2010-12-19 12:40:33 -04:00
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nav_bearing = wrap_360(nav_bearing);
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}
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}
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2011-04-21 20:07:31 -03:00
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long cross_track_test()
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{
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long temp = target_bearing - crosstrack_bearing;
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temp = wrap_180(temp);
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return abs(temp);
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}
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2010-12-19 12:40:33 -04:00
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void reset_crosstrack()
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{
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crosstrack_bearing = get_bearing(¤t_loc, &next_WP); // Used for track following
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}
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2011-02-24 01:56:59 -04:00
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long get_altitude_above_home(void)
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2010-12-19 12:40:33 -04:00
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{
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// This is the altitude above the home location
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// The GPS gives us altitude at Sea Level
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// if you slope soar, you should see a negative number sometimes
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// -------------------------------------------------------------
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return current_loc.alt - home.alt;
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}
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2011-03-26 03:35:52 -03:00
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// distance is returned in meters
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2011-03-02 22:32:50 -04:00
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long get_distance(struct Location *loc1, struct Location *loc2)
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2010-12-19 12:40:33 -04:00
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{
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2011-03-15 02:54:48 -03:00
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//if(loc1->lat == 0 || loc1->lng == 0)
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// return -1;
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//if(loc2->lat == 0 || loc2->lng == 0)
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// return -1;
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2010-12-19 12:40:33 -04:00
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float dlat = (float)(loc2->lat - loc1->lat);
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float dlong = ((float)(loc2->lng - loc1->lng)) * scaleLongDown;
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return sqrt(sq(dlat) + sq(dlong)) * .01113195;
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}
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long get_alt_distance(struct Location *loc1, struct Location *loc2)
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{
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return abs(loc1->alt - loc2->alt);
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}
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long get_bearing(struct Location *loc1, struct Location *loc2)
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{
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long off_x = loc2->lng - loc1->lng;
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long off_y = (loc2->lat - loc1->lat) * scaleLongUp;
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long bearing = 9000 + atan2(-off_y, off_x) * 5729.57795;
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if (bearing < 0) bearing += 36000;
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return bearing;
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}
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