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Move vtol standard params

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sanderux 2017-08-15 10:12:12 +02:00 committed by Sander Smeets
parent 7a8d3c4ab2
commit ff669ee645
2 changed files with 26 additions and 26 deletions
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26
src/modules/vtol_att_control/standard_params.c
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@ -84,3 +84,29 @@ PARAM_DEFINE_FLOAT(VT_FWD_THRUST_SC, 0.0f);
* @group VTOL Attitude Control
*/
PARAM_DEFINE_FLOAT(VT_B_TRANS_RAMP, 3.0f);
/**
* Output on airbrakes channel during back transition
* Used for airbrakes or with ESCs that have reverse thrust enabled on a seperate channel
* Airbrakes need to be enables for your selected model/mixer
*
* @min 0
* @max 1
* @increment 0.01
* @decimal 2
* @group VTOL Attitude Control
*/
PARAM_DEFINE_FLOAT(VT_B_REV_OUT, 0.0f);
/**
* Thottle output during back transition
* For ESCs and mixers that support reverse thrust on low PWM values set this to a negative value to apply active breaking
* For ESCs that support thrust reversal with a control channel please set VT_B_REV_OUT and set this to a positive value to apply active breaking
*
* @min -1
* @max 1
* @increment 0.01
* @decimal 2
* @group VTOL Attitude Control
*/
PARAM_DEFINE_FLOAT(VT_B_REV_THR, 0.0f);

26
src/modules/vtol_att_control/vtol_att_control_params.c
View File

@ -235,32 +235,6 @@ PARAM_DEFINE_FLOAT(VT_B_TRANS_DUR, 4.0f);
*/
PARAM_DEFINE_FLOAT(VT_B_DEC_MSS, 2.0f);
/**
* Output on airbrakes channel during back transition
* Used for airbrakes or with ESCs that have reverse thrust enabled on a seperate channel
* Airbrakes need to be enables for your selected model/mixer
*
* @min 0
* @max 1
* @increment 0.01
* @decimal 2
* @group VTOL Attitude Control
*/
PARAM_DEFINE_FLOAT(VT_B_REV_OUT, 0.0f);
/**
* Thottle output during back transition
* For ESCs and mixers that support reverse thrust on low PWM values set this to a negative value to apply active breaking
* For ESCs that support thrust reversal with a control channel please set VT_B_REV_OUT and set this to a positive value to apply active breaking
*
* @min -1
* @max 1
* @increment 0.01
* @decimal 2
* @group VTOL Attitude Control
*/
PARAM_DEFINE_FLOAT(VT_B_REV_THR, 0.0f);
/**
* Transition blending airspeed
*