diff options
Diffstat (limited to 'src/modules/fw_pos_control_l1')
-rw-r--r-- | src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp | 8 |
1 files changed, 4 insertions, 4 deletions
diff --git a/src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp b/src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp index 9704eacb9..0127160fb 100644 --- a/src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp +++ b/src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp @@ -879,17 +879,17 @@ FixedwingPositionControl::control_position(const math::Vector2f ¤t_positio /* intersect glide slope: * if current position is higher or within 10m of slope follow the glide slope - * if current position is below slope -10m continue on previous wp altitude until the intersection with the slope + * if current position is below slope -10m continue on maximum of previous wp altitude or L_altitude until the intersection with the slope * */ float altitude_desired = _global_pos.alt; if (_global_pos.alt > landing_slope_alt_desired - 10.0f) { /* stay on slope */ altitude_desired = landing_slope_alt_desired; warnx("Landing: before L, stay on landing slope, alt_desired: %.1f (wp_distance: %.1f, L_wp_distance %.1f), calculate_target_airspeed(airspeed_land) %.1f, horizontal_slope_displacement %.1f", altitude_desired, wp_distance, L_wp_distance, calculate_target_airspeed(airspeed_land), horizontal_slope_displacement); - } else if (_global_pos.alt < landing_slope_alt_desired - 10.0f) { + } else { /* continue horizontally */ - altitude_desired = _global_triplet.previous.altitude; //xxx: dangerous, but we have the altitude < L_altitude protection - warnx("Landing: before L,continue horizontal at last wp alt: %.4f, (landing_slope_alt_desired %.4f, wp_distance: %.4f, L_altitude: %.4f L_wp_distance: %.4f)", altitude_desired, landing_slope_alt_desired, wp_distance, L_altitude, L_wp_distance); + altitude_desired = math::max(_global_pos.alt, L_altitude); + warnx("Landing: before L,continue at: %.4f, (landing_slope_alt_desired %.4f, wp_distance: %.4f, L_altitude: %.4f L_wp_distance: %.4f)", altitude_desired, landing_slope_alt_desired, wp_distance, L_altitude, L_wp_distance); } _tecs.update_pitch_throttle(_R_nb, _att.pitch, _global_pos.alt, altitude_desired, calculate_target_airspeed(airspeed_approach), |