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| author | Thomas Gubler <thomasgubler@gmail.com> | 2013-12-29 16:35:52 +0100 |
|---|---|---|
| committer | Thomas Gubler <thomasgubler@gmail.com> | 2013-12-29 16:35:52 +0100 |
| commit | 6a9423b428c78e4c2ea295544df50f5b1f0cd49d (patch) | |
| tree | 3e6642c6d5646927569a2bb52927dce6b792b9c2 /src/modules/fw_att_control/fw_att_control_params.c | |
| parent | 70cc5413b43eaebc20ca5bda87dc8f66147b7501 (diff) | |
| download | px4-firmware-6a9423b428c78e4c2ea295544df50f5b1f0cd49d.tar.gz px4-firmware-6a9423b428c78e4c2ea295544df50f5b1f0cd49d.tar.bz2 px4-firmware-6a9423b428c78e4c2ea295544df50f5b1f0cd49d.zip | |
fw att ctrl: remove renamed parameters
Diffstat (limited to 'src/modules/fw_att_control/fw_att_control_params.c')
| -rw-r--r-- | src/modules/fw_att_control/fw_att_control_params.c | 13 |
1 files changed, 0 insertions, 13 deletions
diff --git a/src/modules/fw_att_control/fw_att_control_params.c b/src/modules/fw_att_control/fw_att_control_params.c index e129568bb..16227b62f 100644 --- a/src/modules/fw_att_control/fw_att_control_params.c +++ b/src/modules/fw_att_control/fw_att_control_params.c @@ -60,11 +60,6 @@ PARAM_DEFINE_FLOAT(FW_ATT_TC, 0.5f); // @Range 10 to 200, 1 increments PARAM_DEFINE_FLOAT(FW_PR_P, 0.05f); -// @DisplayName Damping gain. -// @Description This gain damps the airframe pitch rate. In particular relevant for flying wings. -// @Range 0.0 to 10.0, 0.1 increments -PARAM_DEFINE_FLOAT(FW_PR_D, 0.0f); //xxx: remove - // @DisplayName Pitch rate integrator gain. // @Description This gain defines how much control response will result out of a steady state error. It trims any constant error. // @Range 0 to 50.0 @@ -100,13 +95,6 @@ PARAM_DEFINE_FLOAT(FW_P_ROLLFF, 0.0f); // @User User PARAM_DEFINE_FLOAT(FW_RR_P, 0.05f); -// @DisplayName Damping Gain -// @Description Controls the roll rate to roll actuator output. It helps to reduce motions in turbulence. -// @Range 0.0 10.0 -// @Increment 1.0 -// @User User -PARAM_DEFINE_FLOAT(FW_RR_D, 0.0f); //xxx: remove - // @DisplayName Roll rate integrator Gain // @Description This gain defines how much control response will result out of a steady state error. It trims any constant error. // @Range 0.0 100.0 @@ -142,7 +130,6 @@ PARAM_DEFINE_FLOAT(FW_YR_I, 0.0f); // @Increment 0.1 PARAM_DEFINE_FLOAT(FW_YR_IMAX, 0.2f); -PARAM_DEFINE_FLOAT(FW_YR_D, 0); //xxx: remove PARAM_DEFINE_FLOAT(FW_Y_ROLLFF, 0); //xxx: remove // @DisplayName Maximum Yaw Rate |