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authorThomas Gubler <thomasgubler@gmail.com>2013-12-29 16:42:31 +0100
committerThomas Gubler <thomasgubler@gmail.com>2013-12-29 16:42:39 +0100
commit95bdc1a9bd364ce95abe06b097579cc8a9162e33 (patch)
tree2b93a7b41fff5d719e240babf54ad22871c3f223 /src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp
parent6a9423b428c78e4c2ea295544df50f5b1f0cd49d (diff)
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fw att ctrl: removed unused parameter
Diffstat (limited to 'src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp')
-rw-r--r--src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp1
1 files changed, 1 insertions, 0 deletions
diff --git a/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp b/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp
index 882fac02b..b66d1dba5 100644
--- a/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp
+++ b/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp
@@ -90,6 +90,7 @@ float ECL_PitchController::control_attitude(float pitch_setpoint, float roll, fl
}
/* calculate the offset in the rate resulting from rolling */
+ //xxx needs explanation and conversion to body angular rates or should be removed
float turn_offset = fabsf((CONSTANTS_ONE_G / airspeed) *
tanf(roll) * sinf(roll)) * _roll_ff;
if (inverted)