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-rw-r--r--src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp3
1 files changed, 1 insertions, 2 deletions
diff --git a/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp b/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp
index 5b8897eaa..8b9ba9c62 100644
--- a/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp
+++ b/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp
@@ -163,8 +163,7 @@ float ECL_PitchController::control_bodyrate(float roll, float pitch,
_integrator = math::constrain(_integrator, -_integrator_max, _integrator_max);
/* Apply PI rate controller and store non-limited output */
- //xxx: naming of gain variables (k_d <--> k_p)
- _last_output = (_rate_error * _k_d + _integrator * _k_i * _rate_setpoint * k_ff) * scaler * scaler; //scaler^2 is proportional to 1/airspeed^2
+ _last_output = (_rate_error * _k_p + _integrator * _k_i * _rate_setpoint * k_ff) * scaler * scaler; //scaler^2 is proportional to 1/airspeed^2
return math::constrain(_last_output, -_max_deflection_rad, _max_deflection_rad);
}