aboutsummaryrefslogtreecommitdiff
path: root/src/lib/ecl/attitude_fw/ecl_yaw_controller.cpp
diff options
context:
space:
mode:
authorThomas Gubler <thomasgubler@gmail.com>2013-10-19 22:07:27 +0200
committerThomas Gubler <thomasgubler@gmail.com>2013-10-24 18:07:33 +0200
commitfeb75f08cba0d18267f9d463db49f7c1db310596 (patch)
treea5cbdc50f2342fcbcc014ae91e5d10f4385b0ac8 /src/lib/ecl/attitude_fw/ecl_yaw_controller.cpp
parentccc6dd73a02f83d8fb857ca25cfe998a3b1303d4 (diff)
downloadpx4-firmware-feb75f08cba0d18267f9d463db49f7c1db310596.tar.gz
px4-firmware-feb75f08cba0d18267f9d463db49f7c1db310596.tar.bz2
px4-firmware-feb75f08cba0d18267f9d463db49f7c1db310596.zip
wip, clean up pid in fw att
Diffstat (limited to 'src/lib/ecl/attitude_fw/ecl_yaw_controller.cpp')
-rw-r--r--src/lib/ecl/attitude_fw/ecl_yaw_controller.cpp16
1 files changed, 9 insertions, 7 deletions
diff --git a/src/lib/ecl/attitude_fw/ecl_yaw_controller.cpp b/src/lib/ecl/attitude_fw/ecl_yaw_controller.cpp
index e56a8d08d..5c9cc820f 100644
--- a/src/lib/ecl/attitude_fw/ecl_yaw_controller.cpp
+++ b/src/lib/ecl/attitude_fw/ecl_yaw_controller.cpp
@@ -106,8 +106,9 @@ float ECL_YawController::control_bodyrate(float roll, float pitch,
lock_integrator = true;
- float k_ff = math::max((_k_p - _k_i * _tc) * _tc - _k_d, 0.0f);
- float k_i_rate = _k_i * _tc;
+// float k_ff = math::max((_k_p - _k_i * _tc) * _tc - _k_d, 0.0f);
+ float k_ff = 0;
+
/* input conditioning */
if (!isfinite(airspeed)) {
@@ -127,13 +128,12 @@ float ECL_YawController::control_bodyrate(float roll, float pitch,
/* Calculate body angular rate error */
_rate_error = _bodyrate_setpoint - yaw_bodyrate; //body angular rate error
- if (!lock_integrator && k_i_rate > 0.0f && airspeed > 0.5f * airspeed_min) {
+ if (!lock_integrator && _k_i > 0.0f && airspeed > 0.5f * airspeed_min) {
float id = _rate_error * dt;
/*
- * anti-windup: do not allow integrator to increase into the
- * wrong direction if actuator is at limit
+ * anti-windup: do not allow integrator to increase if actuator is at limit
*/
if (_last_output < -_max_deflection_rad) {
/* only allow motion to center: increase value */
@@ -148,8 +148,10 @@ float ECL_YawController::control_bodyrate(float roll, float pitch,
/* integrator limit */
_integrator = math::constrain(_integrator, -_integrator_max, _integrator_max);
- /* store non-limited output */
- _last_output = ((_rate_error * _k_d * scaler) + _integrator * k_i_rate * scaler + (_rate_setpoint * k_ff)) * scaler;
+
+ /* 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
return math::constrain(_last_output, -_max_deflection_rad, _max_deflection_rad);
}