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path: root/src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp
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Diffstat (limited to 'src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp')
-rw-r--r--src/modules/fw_pos_control_l1/fw_pos_control_l1_main.cpp2
1 files changed, 1 insertions, 1 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 5f91eb61d..50a54c792 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
@@ -800,7 +800,7 @@ FixedwingPositionControl::control_position(const math::Vector2f &current_positio
/* apply minimum pitch (flare) and limit roll if close to touch down, altitude error is negative (going down) */
// XXX this could make a great param
- float flare_angle_rad = math::radians(10.0f);//math::radians(global_triplet.current.param1)
+ float flare_angle_rad = -math::radians(5.0f);//math::radians(global_triplet.current.param1)
float land_pitch_min = math::radians(5.0f);
float throttle_land = _parameters.throttle_min + (_parameters.throttle_max - _parameters.throttle_min) * 0.1f;
float airspeed_land = _parameters.airspeed_min;