diff options
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.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 e43469b70..7fd7ed07f 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 @@ -386,7 +386,7 @@ private: bool climbout_mode, float climbout_pitch_min_rad, float altitude, const math::Vector<3> &ground_speed, - fwPosctrl::mTecs::tecs_mode mode = fwPosctrl::mTecs::TECS_MODE_NORMAL); + tecs_mode mode = TECS_MODE_NORMAL); }; @@ -1018,7 +1018,7 @@ FixedwingPositionControl::control_position(const math::Vector<2> ¤t_positi 0.0f, throttle_max, throttle_land, false, flare_pitch_angle_rad, _pos_sp_triplet.current.alt + relative_alt, ground_speed, - land_motor_lim ? fwPosctrl::mTecs::TECS_MODE_LAND_THROTTLELIM : fwPosctrl::mTecs::TECS_MODE_LAND); + land_motor_lim ? TECS_MODE_LAND_THROTTLELIM : TECS_MODE_LAND); if (!land_noreturn_vertical) { mavlink_log_info(_mavlink_fd, "#audio: Landing, flaring"); @@ -1111,7 +1111,7 @@ FixedwingPositionControl::control_position(const math::Vector<2> ¤t_positi math::radians(10.0f)), _global_pos.alt, ground_speed, - fwPosctrl::mTecs::TECS_MODE_TAKEOFF); + TECS_MODE_TAKEOFF); /* limit roll motion to ensure enough lift */ _att_sp.roll_body = math::constrain(_att_sp.roll_body, math::radians(-15.0f), math::radians(15.0f)); @@ -1449,7 +1449,7 @@ void FixedwingPositionControl::tecs_update_pitch_throttle(float alt_sp, float v_ bool climbout_mode, float climbout_pitch_min_rad, float altitude, const math::Vector<3> &ground_speed, - fwPosctrl::mTecs::tecs_mode mode) + tecs_mode mode) { if (_mTecs.getEnabled()) { /* Using mtecs library: prepare arguments for mtecs call */ |