diff --git a/ArduCopter/Parameters.pde b/ArduCopter/Parameters.pde index 0c2dd3f9b5..87db708309 100644 --- a/ArduCopter/Parameters.pde +++ b/ArduCopter/Parameters.pde @@ -35,6 +35,7 @@ const AP_Param::Info var_info[] PROGMEM = { // @Param: SYSID_SW_TYPE // @DisplayName: Software Type // @Description: This is used by the ground station to recognise the software type (eg ArduPlane vs ArduCopter) + // @Values: 0:ArduPlane,4:AntennaTracker,10:Copter,20:Rover // @User: Advanced GSCALAR(software_type, "SYSID_SW_TYPE", Parameters::k_software_type), @@ -418,6 +419,7 @@ const AP_Param::Info var_info[] PROGMEM = { // @Param: ANGLE_MAX // @DisplayName: Angle Max // @Description: Maximum lean angle in all flight modes + // @Units: Centi-degrees // @Range 1000 8000 // @User: Advanced ASCALAR(angle_max, "ANGLE_MAX", DEFAULT_ANGLE_MAX), @@ -435,6 +437,7 @@ const AP_Param::Info var_info[] PROGMEM = { // @Param: PHLD_BRAKE_RATE // @DisplayName: PosHold braking rate // @Description: PosHold flight mode's rotation rate during braking in deg/sec + // @Units: deg/sec // @Range: 4 12 // @User: Advanced GSCALAR(poshold_brake_rate, "PHLD_BRAKE_RATE", POSHOLD_BRAKE_RATE_DEFAULT), @@ -574,7 +577,7 @@ const AP_Param::Info var_info[] PROGMEM = { // @Param: ACRO_BAL_ROLL // @DisplayName: Acro Balance Roll - // @Description: rate at which roll angle returns to level in acro mode + // @Description: rate at which roll angle returns to level in acro mode. A higher value causes the vehicle to return to level faster. // @Range: 0 3 // @Increment: 0.1 // @User: Advanced @@ -582,7 +585,7 @@ const AP_Param::Info var_info[] PROGMEM = { // @Param: ACRO_BAL_PITCH // @DisplayName: Acro Balance Pitch - // @Description: rate at which pitch angle returns to level in acro mode + // @Description: rate at which pitch angle returns to level in acro mode. A higher value causes the vehicle to return to level faster. // @Range: 0 3 // @Increment: 0.1 // @User: Advanced