diff options
Diffstat (limited to 'src/modules/fw_att_control')
| -rw-r--r-- | src/modules/fw_att_control/fw_att_control_main.cpp | 5 |
1 files changed, 5 insertions, 0 deletions
diff --git a/src/modules/fw_att_control/fw_att_control_main.cpp b/src/modules/fw_att_control/fw_att_control_main.cpp index 8d18ae68c..d8377899c 100644 --- a/src/modules/fw_att_control/fw_att_control_main.cpp +++ b/src/modules/fw_att_control/fw_att_control_main.cpp @@ -824,6 +824,7 @@ FixedwingAttitudeControl::task_main() float roll_sp = _parameters.rollsp_offset_rad; float pitch_sp = _parameters.pitchsp_offset_rad; + float yaw_manual = 0.0f; float throttle_sp = 0.0f; /* Read attitude setpoint from uorb if @@ -884,6 +885,8 @@ FixedwingAttitudeControl::task_main() + _parameters.rollsp_offset_rad; pitch_sp = -(_manual.x * _parameters.man_pitch_max - _parameters.trim_pitch) + _parameters.pitchsp_offset_rad; + // allow manual control of rudder deflection + yaw_manual = _manual.r; throttle_sp = _manual.z; _actuators.control[4] = _manual.flaps; @@ -983,6 +986,8 @@ FixedwingAttitudeControl::task_main() _pitch_ctrl.get_desired_rate(), _parameters.airspeed_min, _parameters.airspeed_max, airspeed, airspeed_scaling, lock_integrator); _actuators.control[2] = (isfinite(yaw_u)) ? yaw_u + _parameters.trim_yaw : _parameters.trim_yaw; + // add in manual rudder control + _actuators.control[2] += yaw_manual; if (!isfinite(yaw_u)) { _yaw_ctrl.reset_integrator(); perf_count(_nonfinite_output_perf); |