mirror of https://github.com/ArduPilot/ardupilot
APM track following change
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@ -190,18 +190,11 @@ static void calc_nav_pitch()
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static void calc_nav_roll()
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{
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// Adjust gain based on ground speed - We need lower nav gain going in to a headwind, etc.
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// This does not make provisions for wind speed in excess of airframe speed
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nav_gain_scaler = (float)g_gps->ground_speed / (STANDARD_SPEED * 100.0);
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nav_gain_scaler = constrain(nav_gain_scaler, 0.2, 1.4);
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// negative error = left turn
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// positive error = right turn
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// Calculate the required roll of the plane
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// ----------------------------------------
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nav_roll = g.pidNavRoll.get_pid(bearing_error, dTnav, nav_gain_scaler); //returns desired bank angle in degrees*100
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nav_roll = constrain(nav_roll, -g.roll_limit.get(), g.roll_limit.get());
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float psi_dot_cmd = g.pidNavRoll.kP() * (bearing_error / 100.0);
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nav_roll = (100 * ToDeg(atan((psi_dot_cmd * ((float)g_gps->ground_speed)) / 981.0)));
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//printf("nvrl %ld err %ld psi %f gps gs %ld COG %ld\n",nav_roll,bearing_error,psi_dot_cmd,g_gps->ground_speed,g_gps->ground_course);
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Vector3f omega;
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omega = dcm.get_gyro();
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@ -180,9 +180,9 @@ static void set_next_WP(struct Location *wp)
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scaleLongDown = cos(rads);
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scaleLongUp = 1.0f/cos(rads);
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// this is handy for the groundstation
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wp_totalDistance = get_distance(¤t_loc, &next_WP);
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wp_totalDistance = get_distance(&prev_WP, &next_WP);
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wp_distance = wp_totalDistance;
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target_bearing = get_bearing(¤t_loc, &next_WP);
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target_bearing = get_bearing(&prev_WP, &next_WP);
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nav_bearing = target_bearing;
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// to check if we have missed the WP
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@ -75,15 +75,15 @@ static void calc_airspeed_errors()
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}
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static void calc_bearing_error()
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{
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{/*
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if(takeoff_complete == true || g.compass_enabled == true) {
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bearing_error = nav_bearing - dcm.yaw_sensor;
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} else {
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*/
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// TODO: we need to use the Yaw gyro for in between GPS reads,
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// maybe as an offset from a saved gryo value.
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bearing_error = nav_bearing - g_gps->ground_course;
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}
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// }
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bearing_error = wrap_180(bearing_error);
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}
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