mirror of https://github.com/ArduPilot/ardupilot
AC_AttitudeControl: Use SI units conventions in parameter units
Follow the rules from: http://physics.nist.gov/cuu/Units/units.html http://physics.nist.gov/cuu/Units/outside.html and http://physics.nist.gov/cuu/Units/checklist.html one further constrain is that only printable (7bit) ASCII characters are allowed
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@ -10,7 +10,7 @@ const AP_Param::GroupInfo AC_AttitudeControl::var_info[] = {
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// @Param: SLEW_YAW
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// @DisplayName: Yaw target slew rate
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// @Description: Maximum rate the yaw target can be updated in Loiter, RTL, Auto flight modes
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// @Units: Centi-Degrees/Sec
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// @Units: cdeg/s
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// @Range: 500 18000
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// @Increment: 100
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// @User: Advanced
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@ -21,7 +21,7 @@ const AP_Param::GroupInfo AC_AttitudeControl::var_info[] = {
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// @Param: ACCEL_Y_MAX
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// @DisplayName: Acceleration Max for Yaw
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// @Description: Maximum acceleration in yaw axis
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// @Units: Centi-Degrees/Sec/Sec
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// @Units: cdeg/s/s
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// @Range: 0 72000
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// @Values: 0:Disabled, 18000:Slow, 36000:Medium, 54000:Fast
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// @Increment: 1000
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@ -38,7 +38,7 @@ const AP_Param::GroupInfo AC_AttitudeControl::var_info[] = {
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// @Param: ACCEL_R_MAX
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// @DisplayName: Acceleration Max for Roll
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// @Description: Maximum acceleration in roll axis
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// @Units: Centi-Degrees/Sec/Sec
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// @Units: cdeg/s/s
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// @Range: 0 180000
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// @Increment: 1000
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// @Values: 0:Disabled, 72000:Slow, 108000:Medium, 162000:Fast
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@ -48,7 +48,7 @@ const AP_Param::GroupInfo AC_AttitudeControl::var_info[] = {
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// @Param: ACCEL_P_MAX
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// @DisplayName: Acceleration Max for Pitch
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// @Description: Maximum acceleration in pitch axis
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// @Units: Centi-Degrees/Sec/Sec
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// @Units: cdeg/s/s
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// @Range: 0 180000
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// @Increment: 1000
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// @Values: 0:Disabled, 72000:Slow, 108000:Medium, 162000:Fast
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@ -16,7 +16,7 @@ const AP_Param::GroupInfo AC_AttitudeControl_Heli::var_info[] = {
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// @Param: HOVR_ROL_TRM
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// @DisplayName: Hover Roll Trim
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// @Description: Trim the hover roll angle to counter tail rotor thrust in a hover
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// @Units: Centi-Degrees
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// @Units: cdeg
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// @Range: 0 1000
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// @User: Advanced
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AP_GROUPINFO("HOVR_ROL_TRM", 1, AC_AttitudeControl_Heli, _hover_roll_trim, AC_ATTITUDE_HELI_HOVER_ROLL_TRIM_DEFAULT),
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@ -26,7 +26,7 @@ const AP_Param::GroupInfo AC_AttitudeControl_Multi::var_info[] = {
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// @Description: Roll axis rate controller I gain maximum. Constrains the maximum motor output that the I gain will output
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// @Range: 0 1
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// @Increment: 0.01
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// @Units: Percent
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// @Units: %
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// @User: Standard
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// @Param: RAT_RLL_D
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@ -71,7 +71,7 @@ const AP_Param::GroupInfo AC_AttitudeControl_Multi::var_info[] = {
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// @Description: Pitch axis rate controller I gain maximum. Constrains the maximum motor output that the I gain will output
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// @Range: 0 1
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// @Increment: 0.01
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// @Units: Percent
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// @Units: %
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// @User: Standard
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// @Param: RAT_PIT_D
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@ -116,7 +116,7 @@ const AP_Param::GroupInfo AC_AttitudeControl_Multi::var_info[] = {
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// @Description: Yaw axis rate controller I gain maximum. Constrains the maximum motor output that the I gain will output
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// @Range: 0 1
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// @Increment: 0.01
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// @Units: Percent
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// @Units: %
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// @User: Standard
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// @Param: RAT_YAW_D
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@ -26,7 +26,7 @@ const AP_Param::GroupInfo AC_AttitudeControl_Sub::var_info[] = {
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// @Description: Roll axis rate controller I gain maximum. Constrains the maximum motor output that the I gain will output
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// @Range: 0 1
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// @Increment: 0.01
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// @Units: Percent
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// @Units: %
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// @User: Standard
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// @Param: RAT_RLL_D
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@ -71,7 +71,7 @@ const AP_Param::GroupInfo AC_AttitudeControl_Sub::var_info[] = {
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// @Description: Pitch axis rate controller I gain maximum. Constrains the maximum motor output that the I gain will output
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// @Range: 0 1
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// @Increment: 0.01
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// @Units: Percent
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// @Units: %
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// @User: Standard
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// @Param: RAT_PIT_D
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@ -116,7 +116,7 @@ const AP_Param::GroupInfo AC_AttitudeControl_Sub::var_info[] = {
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// @Description: Yaw axis rate controller I gain maximum. Constrains the maximum motor output that the I gain will output
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// @Range: 0 1
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// @Increment: 0.01
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// @Units: Percent
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// @Units: %
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// @User: Standard
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// @Param: RAT_YAW_D
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