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@ -14,10 +14,6 @@ static void navigate()
@@ -14,10 +14,6 @@ static void navigate()
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// -------------------------------------------- |
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target_bearing = get_bearing(¤t_loc, &next_WP); |
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home_to_copter_bearing = get_bearing(&home, ¤t_loc); |
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// nav_bearing will includes xtrac correction |
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// ------------------------------------------ |
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nav_bearing = target_bearing; |
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} |
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static bool check_missed_wp() |
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@ -30,16 +26,12 @@ static bool check_missed_wp()
@@ -30,16 +26,12 @@ static bool check_missed_wp()
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// ------------------------------ |
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static void calc_XY_velocity(){ |
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// called after GPS read |
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// offset calculation of GPS speed: |
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// used for estimations below 1.5m/s |
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// our GPS is about 1m per |
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static int32_t last_longitude = 0; |
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static int32_t last_latitude = 0; |
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static int16_t x_speed_old = 0; |
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static int16_t y_speed_old = 0; |
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// called after GPS read |
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// offset calculation of GPS speed: |
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// used for estimations below 1.5m/s |
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// y_GPS_speed positve = Up |
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// x_GPS_speed positve = Right |
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@ -55,25 +47,22 @@ static void calc_XY_velocity(){
@@ -55,25 +47,22 @@ static void calc_XY_velocity(){
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x_actual_speed = (float)(g_gps->longitude - last_longitude) * scaleLongDown * tmp; |
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y_actual_speed = (float)(g_gps->latitude - last_latitude) * tmp; |
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x_actual_speed = (x_actual_speed + x_speed_old ) / 2; |
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y_actual_speed = (y_actual_speed + y_speed_old ) / 2; |
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x_speed_old = x_actual_speed; |
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y_speed_old = y_actual_speed; |
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last_longitude = g_gps->longitude; |
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last_latitude = g_gps->latitude; |
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if(g_gps->ground_speed > 150){ |
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float temp = radians((float)g_gps->ground_course/100.0); |
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x_actual_speed = (float)g_gps->ground_speed * sin(temp); |
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y_actual_speed = (float)g_gps->ground_speed * cos(temp); |
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} |
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#if INERTIAL_NAV == ENABLED |
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// inertial_nav |
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xy_error_correction(); |
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#endif |
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/*if(g_gps->ground_speed > 150){ |
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float temp = radians((float)g_gps->ground_course/100.0); |
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x_actual_speed = (float)g_gps->ground_speed * sin(temp); |
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y_actual_speed = (float)g_gps->ground_speed * cos(temp); |
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}*/ |
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current_loc.lng = xLeadFilter.get_position(g_gps->longitude, x_actual_speed); |
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current_loc.lat = yLeadFilter.get_position(g_gps->latitude, y_actual_speed); |
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} |
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static void calc_location_error(struct Location *next_loc) |
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@ -185,20 +174,33 @@ static void calc_loiter(int x_error, int y_error)
@@ -185,20 +174,33 @@ static void calc_loiter(int x_error, int y_error)
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static void calc_nav_rate(int max_speed) |
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{ |
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float temp, temp_x, temp_y; |
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// push us towards the original track |
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update_crosstrack(); |
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// nav_bearing includes crosstrack |
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float temp = (9000l - nav_bearing) * RADX100; |
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int16_t cross_speed = crosstrack_error * -g.crosstrack_gain; // scale down crosstrack_error in cm |
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// XXX replace above with crosstrack gain. |
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cross_speed = constrain(cross_speed, -200, 200); |
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// rotate by 90 to deal with trig functions |
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temp = (9000l - target_bearing) * RADX100; |
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temp_x = cos(temp); |
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temp_y = sin(temp); |
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// rotate desired spped vector: |
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int16_t x_target_speed = max_speed * temp_x - cross_speed * temp_y; |
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int16_t y_target_speed = cross_speed * temp_x + max_speed * temp_y; |
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// East / West |
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x_rate_error = (cos(temp) * max_speed) - x_actual_speed; // 413 |
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x_rate_error = x_target_speed - x_actual_speed; // 413 |
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x_rate_error = constrain(x_rate_error, -1000, 1000); |
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nav_lon = g.pid_nav_lon.get_pid(x_rate_error, dTnav); |
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nav_lon = constrain(nav_lon, -3000, 3000); |
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// North / South |
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y_rate_error = (sin(temp) * max_speed) - y_actual_speed; // 413 |
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y_rate_error = y_target_speed - y_actual_speed; // 413 |
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y_rate_error = constrain(y_rate_error, -1000, 1000); // added a rate error limit to keep pitching down to a minimum |
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nav_lat = g.pid_nav_lat.get_pid(y_rate_error, dTnav); |
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nav_lat = constrain(nav_lat, -3000, 3000); |
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@ -206,9 +208,9 @@ static void calc_nav_rate(int max_speed)
@@ -206,9 +208,9 @@ static void calc_nav_rate(int max_speed)
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// copy over I term to Loiter_Rate |
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g.pid_loiter_rate_lon.set_integrator(g.pid_nav_lon.get_integrator()); |
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g.pid_loiter_rate_lat.set_integrator(g.pid_nav_lat.get_integrator()); |
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} |
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// this calculation rotates our World frame of reference to the copter's frame of reference |
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// We use the DCM's matrix to precalculate these trig values at 50hz |
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static void calc_loiter_pitch_roll() |
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@ -257,14 +259,9 @@ static void update_crosstrack(void)
@@ -257,14 +259,9 @@ static void update_crosstrack(void)
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{ |
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// Crosstrack Error |
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// ---------------- |
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if (abs(wrap_180(target_bearing - original_target_bearing)) < 4500) { // If we are too far off or too close we don't do track following |
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// If we are too far off or too close we don't do track following |
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float temp = (target_bearing - original_target_bearing) * RADX100; |
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crosstrack_error = sin(temp) * (wp_distance * g.crosstrack_gain); // Meters we are off track line |
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nav_bearing = target_bearing + constrain(crosstrack_error, -3000, 3000); |
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nav_bearing = wrap_360(nav_bearing); |
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}else{ |
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nav_bearing = target_bearing; |
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} |
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crosstrack_error = sin(temp) * wp_distance; // Meters we are off track line |
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} |
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static int32_t get_altitude_error() |
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