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Fix parameter description from review comments 

This commit makes the parameter description of the fixewing attitude controller more descriptive
This commit is contained in:
Jaeyoung Lim 2022-08-16 18:52:48 +02:00 committed by Silvan Fuhrer
parent 70d7070307
commit 70134296ed
1 changed files with 6 additions and 12 deletions
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18
src/modules/fw_att_control/fw_att_control_params.c
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@ -84,8 +84,7 @@ PARAM_DEFINE_FLOAT(FW_P_TC, 0.4f);
/**
* Pitch rate proportional gain.
*
* This defines how much the elevator input will be commanded depending on the
* current body angular rate error.
* Pitch rate proportional gain, i.e. control output for angular speed error 1 rad/s.
*
* @unit %/rad/s
* @min 0.0
@ -99,8 +98,7 @@ PARAM_DEFINE_FLOAT(FW_PR_P, 0.08f);
/**
* Pitch rate derivative gain.
*
* This defines how much the elevator input will be commanded depending on the
* current body angular acceleration error.
* Pitch rate differential gain. Small values help reduce fast oscillations. If value is too big oscillations will appear again.
*
* @unit %/rad/s
* @min 0.0
@ -173,8 +171,7 @@ PARAM_DEFINE_FLOAT(FW_PR_IMAX, 0.4f);
/**
* Roll rate proportional Gain
*
* This defines how much the aileron input will be commanded depending on the
* current body angular rate error.
* Roll rate proportional gain, i.e. control output for angular speed error 1 rad/s.
*
* @unit %/rad/s
* @min 0.0
@ -188,8 +185,7 @@ PARAM_DEFINE_FLOAT(FW_RR_P, 0.05f);
/**
* Roll rate derivative Gain
*
* This defines how much the aileron input will be commanded depending on the
* current body angular acceleration error.
* Roll rate differential gain. Small values help reduce fast oscillations. If value is too big oscillations will appear again.
*
* @unit %/rad/s
* @min 0.0
@ -246,8 +242,7 @@ PARAM_DEFINE_FLOAT(FW_R_RMAX, 70.0f);
/**
* Yaw rate proportional gain
*
* This defines how much the rudder input will be commanded depending on the
* current body angular rate error.
* Yaw rate proportional gain, i.e. control output for angular speed error 1 rad/s.
*
* @unit %/rad/s
* @min 0.0
@ -261,8 +256,7 @@ PARAM_DEFINE_FLOAT(FW_YR_P, 0.05f);
/**
* Yaw rate derivative gain
*
* This defines how much the rudder input will be commanded depending on the
* current body angular acceleration error.
* Yaw rate differential gain. Small values help reduce fast oscillations. If value is too big oscillations will appear again.
*
* @unit %/rad/s
* @min 0.0