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https://github.com/ArduPilot/ardupilot
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AP_Landing: replace location_offset() and get_distance() function calls with Location object member function calls
This allows removing duplicated code
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@ -117,7 +117,7 @@ private:
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// same as land_slope but sampled once before a rangefinder changes the slope. This should be the original mission planned slope
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float initial_slope;
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// calculated approach slope during auto-landing: ((prev_WP_loc.alt - next_WP_loc.alt)*0.01f - flare_sec * sink_rate) / get_distance(prev_WP_loc, next_WP_loc)
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// calculated approach slope during auto-landing: ((prev_WP_loc.alt - next_WP_loc.alt)*0.01f - flare_sec * sink_rate) / prev_WP_loc.get_distance(next_WP_loc)
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float slope;
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AP_Mission &mission;
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@ -187,7 +187,7 @@ bool AP_Landing_Deepstall::verify_land(const Location &prev_WP_loc, Location &ne
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{
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switch (stage) {
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case DEEPSTALL_STAGE_FLY_TO_LANDING:
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if (get_distance(current_loc, landing_point) > abs(2 * landing.aparm.loiter_radius)) {
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if (current_loc.get_distance(landing_point) > abs(2 * landing.aparm.loiter_radius)) {
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landing.nav_controller->update_waypoint(current_loc, landing_point);
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return false;
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}
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@ -239,7 +239,7 @@ bool AP_Landing_Deepstall::verify_land(const Location &prev_WP_loc, Location &ne
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memcpy(&breakout_location, ¤t_loc, sizeof(Location));
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FALLTHROUGH;
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case DEEPSTALL_STAGE_FLY_TO_ARC:
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if (get_distance(current_loc, arc_entry) > 2 * landing.aparm.loiter_radius) {
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if (current_loc.get_distance(arc_entry) > 2 * landing.aparm.loiter_radius) {
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landing.nav_controller->update_waypoint(breakout_location, arc_entry);
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return false;
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}
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@ -100,7 +100,7 @@ bool AP_Landing::type_slope_verify_land(const Location &prev_WP_loc, Location &n
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gcs().send_text(MAV_SEVERITY_INFO, "Flare %.1fm sink=%.2f speed=%.1f dist=%.1f",
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(double)height, (double)sink_rate,
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(double)AP::gps().ground_speed(),
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(double)get_distance(current_loc, next_WP_loc));
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(double)current_loc.get_distance(next_WP_loc));
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}
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type_slope_stage = SLOPE_STAGE_FINAL;
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@ -139,14 +139,14 @@ bool AP_Landing::type_slope_verify_land(const Location &prev_WP_loc, Location &n
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int32_t land_bearing_cd = get_bearing_cd(prev_WP_loc, next_WP_loc);
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location_update(land_WP_loc,
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land_bearing_cd*0.01f,
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get_distance(prev_WP_loc, current_loc) + 200);
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prev_WP_loc.get_distance(current_loc) + 200);
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nav_controller->update_waypoint(prev_WP_loc, land_WP_loc);
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// once landed and stationary, post some statistics
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// this is done before disarm_if_autoland_complete() so that it happens on the next loop after the disarm
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if (type_slope_flags.post_stats && !is_armed) {
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type_slope_flags.post_stats = false;
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gcs().send_text(MAV_SEVERITY_INFO, "Distance from LAND point=%.2fm", (double)get_distance(current_loc, next_WP_loc));
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gcs().send_text(MAV_SEVERITY_INFO, "Distance from LAND point=%.2fm", (double)current_loc.get_distance(next_WP_loc));
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}
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// check if we should auto-disarm after a confirmed landing
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@ -179,7 +179,7 @@ void AP_Landing::type_slope_adjust_landing_slope_for_rangefinder_bump(AP_Vehicle
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rangefinder_state.last_stable_correction = rangefinder_state.correction;
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float corrected_alt_m = (adjusted_altitude_cm_fn() - next_WP_loc.alt)*0.01f - rangefinder_state.correction;
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float total_distance_m = get_distance(prev_WP_loc, next_WP_loc);
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float total_distance_m = prev_WP_loc.get_distance(next_WP_loc);
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float top_of_glide_slope_alt_m = total_distance_m * corrected_alt_m / wp_distance;
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prev_WP_loc.alt = top_of_glide_slope_alt_m*100 + next_WP_loc.alt;
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@ -229,7 +229,7 @@ bool AP_Landing::type_slope_request_go_around(void)
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*/
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void AP_Landing::type_slope_setup_landing_glide_slope(const Location &prev_WP_loc, const Location &next_WP_loc, const Location ¤t_loc, int32_t &target_altitude_offset_cm)
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{
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float total_distance = get_distance(prev_WP_loc, next_WP_loc);
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float total_distance = prev_WP_loc.get_distance(next_WP_loc);
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// If someone mistakenly puts all 0's in their LAND command then total_distance
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// will be calculated as 0 and cause a divide by 0 error below. Lets avoid that.
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