fly316/PX4-Autopilot
7
0
Fork 0
mirror of https://gitee.com/mirrors_PX4/PX4-Autopilot.git synced 2026-04-28 07:44:07 +08:00
Code Issues Packages Projects Releases Wiki Activity

Consistent capital use

Browse Source
This commit is contained in:
sanderux 2017-08-08 15:33:17 +02:00 committed by Sander Smeets
parent e8a84b4faa
commit 2c4bbf3f44
1 changed files with 8 additions and 8 deletions
Show Stats Download Patch File Download Diff File Expand all files Collapse all files

16
src/modules/fw_att_control/fw_att_control_params.c
View File

@ -64,7 +64,7 @@
PARAM_DEFINE_FLOAT(FW_R_TC, 0.4f);
/**
* Attitude Pitch Time Constant
* Attitude pitch time constant
*
* This defines the latency between a pitch step input and the achieved setpoint
* (inverse to a P gain). Half a second is a good start value and fits for
@ -186,7 +186,7 @@ PARAM_DEFINE_FLOAT(FW_RR_P, 0.05f);
PARAM_DEFINE_FLOAT(FW_RR_I, 0.01f);
/**
* Roll Integrator Anti-Windup
* Roll integrator anti-windup
*
* The portion of the integrator part in the control surface deflection is limited to this value.
*
@ -199,7 +199,7 @@ PARAM_DEFINE_FLOAT(FW_RR_I, 0.01f);
PARAM_DEFINE_FLOAT(FW_RR_IMAX, 0.2f);
/**
* Maximum Roll Rate
* Maximum roll rate
*
* This limits the maximum roll rate the controller will output (in degrees per
* second). Setting a value of zero disables the limit.
@ -258,7 +258,7 @@ PARAM_DEFINE_FLOAT(FW_YR_I, 0.0f);
PARAM_DEFINE_FLOAT(FW_YR_IMAX, 0.2f);
/**
* Maximum Yaw Rate
* Maximum yaw rate
*
* This limits the maximum yaw rate the controller will output (in degrees per
* second). Setting a value of zero disables the limit.
@ -444,7 +444,7 @@ PARAM_DEFINE_FLOAT(FW_YCO_VMIN, 1000.0f);
PARAM_DEFINE_INT32(FW_YCO_METHOD, 0);
/**
* Roll Setpoint Offset
* Roll setpoint offset
*
* An airframe specific offset of the roll setpoint in degrees, the value is
* added to the roll setpoint and should correspond to the typical cruise speed
@ -460,7 +460,7 @@ PARAM_DEFINE_INT32(FW_YCO_METHOD, 0);
PARAM_DEFINE_FLOAT(FW_RSP_OFF, 0.0f);
/**
* Pitch Setpoint Offset
* Pitch setpoint offset
*
* An airframe specific offset of the pitch setpoint in degrees, the value is
* added to the pitch setpoint and should correspond to the typical cruise
@ -476,7 +476,7 @@ PARAM_DEFINE_FLOAT(FW_RSP_OFF, 0.0f);
PARAM_DEFINE_FLOAT(FW_PSP_OFF, 0.0f);
/**
* Max Manual Roll
* Max manual roll
*
* Max roll for manual control in attitude stabilized mode
*
@ -490,7 +490,7 @@ PARAM_DEFINE_FLOAT(FW_PSP_OFF, 0.0f);
PARAM_DEFINE_FLOAT(FW_MAN_R_MAX, 45.0f);
/**
* Max Manual Pitch
* Max manual pitch
*
* Max pitch for manual control in attitude stabilized mode
*