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https://github.com/ArduPilot/ardupilot
synced 2025-01-12 10:58:30 -04:00
made the last step of landing stop navigating so we can drop straight down.
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66c974a949
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@ -1244,9 +1244,19 @@ static void update_navigation()
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// switch passthrough to LOITER
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// switch passthrough to LOITER
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case LOITER:
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case LOITER:
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case POSITION:
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case POSITION:
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wp_control = LOITER_MODE;
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// calculates the desired Roll and Pitch
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update_nav_wp();
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break;
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case LAND:
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case LAND:
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wp_control = LOITER_MODE;
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wp_control = LOITER_MODE;
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if (current_loc.alt < 250){
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wp_control = NO_NAV_MODE;
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next_WP.alt = -200; // force us down
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}
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// calculates the desired Roll and Pitch
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// calculates the desired Roll and Pitch
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update_nav_wp();
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update_nav_wp();
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break;
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break;
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@ -1589,11 +1599,16 @@ static void update_nav_wp()
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//int nroll = nav_roll;
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//int nroll = nav_roll;
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//int npitch = nav_pitch;
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//int npitch = nav_pitch;
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//Serial.printf("CIRCLE: angle:%d, dist:%d, X:%d, Y:%d, P:%d, R:%d \n", angleTest, (int)wp_distance , (int)long_error, (int)lat_error, npitch, nroll);
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//Serial.printf("CIRCLE: angle:%d, dist:%d, X:%d, Y:%d, P:%d, R:%d \n", angleTest, (int)wp_distance , (int)long_error, (int)lat_error, npitch, nroll);
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} else {
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}else if(wp_control == WP_MODE){
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// use error as the desired rate towards the target
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// use error as the desired rate towards the target
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calc_nav_rate(g.waypoint_speed_max);
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calc_nav_rate(g.waypoint_speed_max);
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// rotate pitch and roll to the copter frame of reference
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// rotate pitch and roll to the copter frame of reference
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calc_nav_pitch_roll();
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calc_nav_pitch_roll();
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}else if(wp_control == NO_NAV_MODE){
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nav_roll = 0;
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nav_pitch = 0;
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}
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}
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}
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}
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