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Copter: 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
This commit is contained in:
Dr.-Ing. Amilcar Do Carmo Lucas 2017-05-02 15:36:10 +02:00 committed by Andrew Tridgell
parent e6a7adb9a6
commit f366095113
1 changed files with 15 additions and 15 deletions
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30
ArduCopter/Parameters.cpp
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@ -80,7 +80,7 @@ const AP_Param::Info Copter::var_info[] = {
// @DisplayName: Pilot takeoff altitude
// @Description: Altitude that altitude control modes will climb to when a takeoff is triggered with the throttle stick.
// @User: Standard
// @Units: Centimeters
// @Units: cm
// @Range: 0.0 1000.0
// @Increment: 10
GSCALAR(pilot_takeoff_alt, "PILOT_TKOFF_ALT", PILOT_TKOFF_ALT_DEFAULT),
@ -109,7 +109,7 @@ const AP_Param::Info Copter::var_info[] = {
// @DisplayName: Telemetry startup delay
// @Description: The amount of time (in seconds) to delay radio telemetry to prevent an Xbee bricking on power up
// @User: Advanced
// @Units: seconds
// @Units: s
// @Range: 0 30
// @Increment: 1
GSCALAR(telem_delay, "TELEM_DELAY", 0),
@ -125,7 +125,7 @@ const AP_Param::Info Copter::var_info[] = {
// @Param: RTL_ALT
// @DisplayName: RTL Altitude
// @Description: The minimum relative altitude the model will move to before Returning to Launch. Set to zero to return at current altitude.
// @Units: Centimeters
// @Units: cm
// @Range: 0 8000
// @Increment: 1
// @User: Standard
@ -167,7 +167,7 @@ const AP_Param::Info Copter::var_info[] = {
// @Param: FS_BATT_VOLTAGE
// @DisplayName: Failsafe battery voltage
// @Description: Battery voltage to trigger failsafe. Set to 0 to disable battery voltage failsafe. If the battery voltage drops below this voltage then the copter will RTL
// @Units: Volts
// @Units: V
// @Increment: 0.1
// @User: Standard
GSCALAR(fs_batt_voltage, "FS_BATT_VOLTAGE", FS_BATT_VOLTAGE_DEFAULT),
@ -175,7 +175,7 @@ const AP_Param::Info Copter::var_info[] = {
// @Param: FS_BATT_MAH
// @DisplayName: Failsafe battery milliAmpHours
// @Description: Battery capacity remaining to trigger failsafe. Set to 0 to disable battery remaining failsafe. If the battery remaining drops below this level then the copter will RTL
// @Units: mAh
// @Units: mA.h
// @Increment: 50
// @User: Standard
GSCALAR(fs_batt_mah, "FS_BATT_MAH", FS_BATT_MAH_DEFAULT),
@ -211,7 +211,7 @@ const AP_Param::Info Copter::var_info[] = {
// @Param: RTL_ALT_FINAL
// @DisplayName: RTL Final Altitude
// @Description: This is the altitude the vehicle will move to as the final stage of Returning to Launch or after completing a mission. Set to zero to land.
// @Units: Centimeters
// @Units: cm
// @Range: -1 1000
// @Increment: 1
// @User: Standard
@ -220,7 +220,7 @@ const AP_Param::Info Copter::var_info[] = {
// @Param: RTL_CLIMB_MIN
// @DisplayName: RTL minimum climb
// @Description: The vehicle will climb this many cm during the initial climb portion of the RTL
// @Units: Centimeters
// @Units: cm
// @Range: 0 3000
// @Increment: 10
// @User: Standard
@ -263,7 +263,7 @@ const AP_Param::Info Copter::var_info[] = {
// @Param: PILOT_VELZ_MAX
// @DisplayName: Pilot maximum vertical speed
// @Description: The maximum vertical velocity the pilot may request in cm/s
// @Units: Centimeters/Second
// @Units: cm/s
// @Range: 50 500
// @Increment: 10
// @User: Standard
@ -289,7 +289,7 @@ const AP_Param::Info Copter::var_info[] = {
// @DisplayName: Throttle Failsafe Value
// @Description: The PWM level on channel 3 below which throttle failsafe triggers
// @Range: 925 1100
// @Units: pwm
// @Units: PWM
// @Increment: 1
// @User: Standard
GSCALAR(failsafe_throttle_value, "FS_THR_VALUE", FS_THR_VALUE_DEFAULT),
@ -299,7 +299,7 @@ const AP_Param::Info Copter::var_info[] = {
// @Description: The deadzone above and below mid throttle. Used in AltHold, Loiter, PosHold flight modes
// @User: Standard
// @Range: 0 300
// @Units: pwm
// @Units: PWM
// @Increment: 1
GSCALAR(throttle_deadzone, "THR_DZ", THR_DZ_DEFAULT),
@ -444,7 +444,7 @@ const AP_Param::Info Copter::var_info[] = {
// @Param: DISARM_DELAY
// @DisplayName: Disarm delay
// @Description: Delay before automatic disarm in seconds. A value of zero disables auto disarm.
// @Units: Seconds
// @Units: s
// @Range: 0 127
// @User: Advanced
GSCALAR(disarm_delay, "DISARM_DELAY", AUTO_DISARMING_DELAY),
@ -452,7 +452,7 @@ const AP_Param::Info Copter::var_info[] = {
// @Param: ANGLE_MAX
// @DisplayName: Angle Max
// @Description: Maximum lean angle in all flight modes
// @Units: Centi-degrees
// @Units: cdeg
// @Range: 1000 8000
// @User: Advanced
ASCALAR(angle_max, "ANGLE_MAX", DEFAULT_ANGLE_MAX),
@ -470,7 +470,7 @@ const AP_Param::Info Copter::var_info[] = {
// @Param: PHLD_BRAKE_RATE
// @DisplayName: PosHold braking rate
// @Description: PosHold flight mode's rotation rate during braking in deg/sec
// @Units: deg/sec
// @Units: deg/s
// @Range: 4 12
// @User: Advanced
GSCALAR(poshold_brake_rate, "PHLD_BRAKE_RATE", POSHOLD_BRAKE_RATE_DEFAULT),
@ -478,7 +478,7 @@ const AP_Param::Info Copter::var_info[] = {
// @Param: PHLD_BRAKE_ANGLE
// @DisplayName: PosHold braking angle max
// @Description: PosHold flight mode's max lean angle during braking in centi-degrees
// @Units: Centi-degrees
// @Units: cdeg
// @Range: 2000 4500
// @User: Advanced
GSCALAR(poshold_brake_angle_max, "PHLD_BRAKE_ANGLE", POSHOLD_BRAKE_ANGLE_DEFAULT),
@ -613,7 +613,7 @@ const AP_Param::Info Copter::var_info[] = {
// @DisplayName: Throttle acceleration controller I gain maximum
// @Description: Throttle acceleration controller I gain maximum. Constrains the maximum pwm that the I term will generate
// @Range: 0 1000
// @Units: Percent*10
// @Units: d%
// @User: Standard
// @Param: ACCEL_Z_D