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path: root/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp
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Diffstat (limited to 'src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp')
-rw-r--r--src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp11
1 files changed, 5 insertions, 6 deletions
diff --git a/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp b/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp
index 8b9ba9c62..531512493 100644
--- a/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp
+++ b/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp
@@ -51,8 +51,7 @@ ECL_PitchController::ECL_PitchController() :
_last_output(0.0f),
_integrator(0.0f),
_rate_error(0.0f),
- _rate_setpoint(0.0f),
- _max_deflection_rad(math::radians(45.0f))
+ _rate_setpoint(0.0f)
{
}
@@ -148,10 +147,10 @@ float ECL_PitchController::control_bodyrate(float roll, float pitch,
/*
* anti-windup: do not allow integrator to increase if actuator is at limit
*/
- if (_last_output < -_max_deflection_rad) {
+ if (_last_output < -1.0f) {
/* only allow motion to center: increase value */
id = math::max(id, 0.0f);
- } else if (_last_output > _max_deflection_rad) {
+ } else if (_last_output > 1.0f) {
/* only allow motion to center: decrease value */
id = math::min(id, 0.0f);
}
@@ -163,9 +162,9 @@ 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 */
- _last_output = (_rate_error * _k_p + _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 is proportional to 1/airspeed
- return math::constrain(_last_output, -_max_deflection_rad, _max_deflection_rad);
+ return math::constrain(_last_output, -1.0f, 1.0f);
}
void ECL_PitchController::reset_integrator()