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APM_Control: replace '@User: User' with '@User: Standard'

This commit is contained in:
Peter Barker 2020-09-14 08:42:53 +10:00 committed by Peter Barker
parent ffb87e68c5
commit d20c6ceb3b
3 changed files with 14 additions and 14 deletions
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10
libraries/APM_Control/AP_PitchController.cpp
View File

@ -37,7 +37,7 @@ const AP_Param::GroupInfo AP_PitchController::var_info[] = {
// @Description: Proportional gain from pitch angle demands to elevator. Higher values allow more servo response but can cause oscillations. Automatically set and adjusted by AUTOTUNE mode.
// @Range: 0.1 3.0
// @Increment: 0.1
// @User: User
// @User: Standard
AP_GROUPINFO("P", 1, AP_PitchController, gains.P, 1.0f),
// @Param: D
@ -45,7 +45,7 @@ const AP_Param::GroupInfo AP_PitchController::var_info[] = {
// @Description: Damping gain from pitch acceleration to elevator. Higher values reduce pitching in turbulence, but can cause oscillations. Automatically set and adjusted by AUTOTUNE mode.
// @Range: 0 0.2
// @Increment: 0.01
// @User: User
// @User: Standard
AP_GROUPINFO("D", 2, AP_PitchController, gains.D, 0.04f),
// @Param: I
@ -53,7 +53,7 @@ const AP_Param::GroupInfo AP_PitchController::var_info[] = {
// @Description: Integrator gain from long-term pitch angle offsets to elevator. Higher values "trim" out offsets faster but can cause oscillations. Automatically set and adjusted by AUTOTUNE mode.
// @Range: 0 0.5
// @Increment: 0.05
// @User: User
// @User: Standard
AP_GROUPINFO("I", 3, AP_PitchController, gains.I, 0.3f),
// @Param: RMAX_UP
@ -79,7 +79,7 @@ const AP_Param::GroupInfo AP_PitchController::var_info[] = {
// @Description: Gain added to pitch to keep aircraft from descending or ascending in turns. Increase in increments of 0.05 to reduce altitude loss. Decrease for altitude gain.
// @Range: 0.7 1.5
// @Increment: 0.05
// @User: User
// @User: Standard
AP_GROUPINFO("RLL", 6, AP_PitchController, _roll_ff, 1.0f),
// @Param: IMAX
@ -95,7 +95,7 @@ const AP_Param::GroupInfo AP_PitchController::var_info[] = {
// @Description: Gain from demanded rate to elevator output.
// @Range: 0.1 4.0
// @Increment: 0.1
// @User: User
// @User: Standard
AP_GROUPINFO("FF", 8, AP_PitchController, gains.FF, 0.0f),
// @Param: SRMAX

8
libraries/APM_Control/AP_RollController.cpp
View File

@ -37,7 +37,7 @@ const AP_Param::GroupInfo AP_RollController::var_info[] = {
// @Description: Proportional gain from roll angle demands to ailerons. Higher values allow more servo response but can cause oscillations. Automatically set and adjusted by AUTOTUNE mode.
// @Range: 0.1 4.0
// @Increment: 0.1
// @User: User
// @User: Standard
AP_GROUPINFO("P", 1, AP_RollController, gains.P, 1.0f),
// @Param: D
@ -45,7 +45,7 @@ const AP_Param::GroupInfo AP_RollController::var_info[] = {
// @Description: Damping gain from roll acceleration to ailerons. Higher values reduce rolling in turbulence, but can cause oscillations. Automatically set and adjusted by AUTOTUNE mode.
// @Range: 0 0.2
// @Increment: 0.01
// @User: User
// @User: Standard
AP_GROUPINFO("D", 2, AP_RollController, gains.D, 0.08f),
// @Param: I
@ -53,7 +53,7 @@ const AP_Param::GroupInfo AP_RollController::var_info[] = {
// @Description: Integrator gain from long-term roll angle offsets to ailerons. Higher values "trim" out offsets faster but can cause oscillations. Automatically set and adjusted by AUTOTUNE mode.
// @Range: 0 1.0
// @Increment: 0.05
// @User: User
// @User: Standard
AP_GROUPINFO("I", 3, AP_RollController, gains.I, 0.3f),
// @Param: RMAX
@ -78,7 +78,7 @@ const AP_Param::GroupInfo AP_RollController::var_info[] = {
// @Description: Gain from demanded rate to aileron output.
// @Range: 0.1 4.0
// @Increment: 0.1
// @User: User
// @User: Standard
AP_GROUPINFO("FF", 6, AP_RollController, gains.FF, 0.0f),
// @Param: SRMAX

10
libraries/APM_Control/AP_SteerController.cpp
View File

@ -38,7 +38,7 @@ const AP_Param::GroupInfo AP_SteerController::var_info[] = {
// @Description: The proportional gain for steering. This should be approximately equal to the diameter of the turning circle of the vehicle at low speed and maximum steering angle
// @Range: 0.1 10.0
// @Increment: 0.1
// @User: User
// @User: Standard
AP_GROUPINFO("P", 1, AP_SteerController, _K_P, 1.8f),
// @Param: I
@ -46,7 +46,7 @@ const AP_Param::GroupInfo AP_SteerController::var_info[] = {
// @Description: This is the gain from the integral of steering angle. Increasing this gain causes the controller to trim out steady offsets due to an out of trim vehicle.
// @Range: 0 1.0
// @Increment: 0.05
// @User: User
// @User: Standard
AP_GROUPINFO("I", 3, AP_SteerController, _K_I, 0.2f),
// @Param: D
@ -54,7 +54,7 @@ const AP_Param::GroupInfo AP_SteerController::var_info[] = {
// @Description: This adjusts the damping of the steering control loop. This gain helps to reduce steering jitter with vibration. It should be increased in 0.01 increments as too high a value can lead to a high frequency steering oscillation that could overstress the vehicle.
// @Range: 0 0.1
// @Increment: 0.01
// @User: User
// @User: Standard
AP_GROUPINFO("D", 4, AP_SteerController, _K_D, 0.005f),
// @Param: IMAX
@ -72,7 +72,7 @@ const AP_Param::GroupInfo AP_SteerController::var_info[] = {
// @Range: 0 5
// @Increment: 0.1
// @Units: m/s
// @User: User
// @User: Standard
AP_GROUPINFO("MINSPD", 6, AP_SteerController, _minspeed, 1.0f),
@ -81,7 +81,7 @@ const AP_Param::GroupInfo AP_SteerController::var_info[] = {
// @Description: The feed forward gain for steering this is the ratio of the achieved turn rate to applied steering. A value of 1 means that the vehicle would yaw at a rate of 45 degrees per second with full steering deflection at 1m/s ground speed.
// @Range: 0.0 10.0
// @Increment: 0.1
// @User: User
// @User: Standard
AP_GROUPINFO("FF", 7, AP_SteerController, _K_FF, 0),