text:qsTr("If the current draw reported by the vehicle is largely different than the current read externally using a current meter you can adjust the amps per volt value to correct this. Click the Calculate button for help with calculating a new value.")
visible:_showAdvanced
}
QGCLabel{
text:qsTr("Amps Offset:")
visible:_showAdvanced
}
FactTextField{
width:_fieldWidth
fact:battAmpOffset
visible:_showAdvanced
}
QGCLabel{
Layout.columnSpan:3
Layout.fillWidth:true
font.pointSize:ScreenTools.smallFontPointSize
wrapMode:Text.WordWrap
text:qsTr("If the vehicle reports a high current read when there is little or no current going through it, adjust the Amps Offset. It should be equal to the voltage reported by the sensor when the current is zero.")
<short_desc>Circuit breaker for disabling buzzer</short_desc>
<long_desc>Setting this parameter to 782097 will disable the buzzer audio notification. WARNING: ENABLING THIS CIRCUIT BREAKER IS AT OWN RISK</long_desc>
<long_desc>Setting this parameter to 782097 will disable the buzzer audio notification. Setting this parameter to 782090 will disable the startup tune, while keeping all others enabled.</long_desc>
<min>0</min>
<max>782097</max>
<reboot_required>true</reboot_required>
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@@ -653,7 +653,7 @@ Note: ekf2 will limit the delta velocity bias estimate magnitude to be less than
<long_desc>This is the minimum indicated airspeed at which the wing can produce 1g of lift. It is used by the airspeed sensor fault detection and failsafe calculation to detect a significant airspeed low measurement error condition and should be set based on flight test for reliable operation. The failsafe response is controlled by the COM_ASPD_FS_ACT parameter.</long_desc>
<short_desc>Time-out for auto disarm after landing</short_desc>
<long_desc>A non-zero, positive value specifies the time-out period in seconds after which the vehicle will be automatically disarmed in case a landing situation has been detected during this period. The vehicle will also auto-disarm right after arming if it has not even flown, however the time will always be 10 seconds such that the pilot has enough time to take off. A negative value means that automatic disarming triggered by landing detection is disabled.</long_desc>
<min>-1</min>
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@@ -2829,6 +2829,7 @@ but also ignore less noise</short_desc>
<long_desc>Global gain of the controller. This gain scales the P, I and D terms of the controller: output = MC_PITCHRATE_K * (MC_PITCHRATE_P * error + MC_PITCHRATE_I * error_integral + MC_PITCHRATE_D * error_derivative) Set MC_PITCHRATE_P=1 to implement a PID in the ideal form. Set MC_PITCHRATE_K=1 to implement a PID in the parallel form.</long_desc>
<long_desc>Limit for pitch rate in manual and auto modes (except acro). Has effect for large rotations in autonomous mode, to avoid large control output and mixer saturation. This is not only limited by the vehicle's properties, but also by the maximum measurement rate of the gyro.</long_desc>
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@@ -4204,6 +4218,14 @@ default 1.5 turns per second</short_desc>
<long_desc>Global gain of the controller. This gain scales the P, I and D terms of the controller: output = MC_ROLLRATE_K * (MC_ROLLRATE_P * error + MC_ROLLRATE_I * error_integral + MC_ROLLRATE_D * error_derivative) Set MC_ROLLRATE_P=1 to implement a PID in the ideal form. Set MC_ROLLRATE_K=1 to implement a PID in the parallel form.</long_desc>
<long_desc>Limit for roll rate in manual and auto modes (except acro). Has effect for large rotations in autonomous mode, to avoid large control output and mixer saturation. This is not only limited by the vehicle's properties, but also by the maximum measurement rate of the gyro.</long_desc>
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@@ -4306,6 +4328,14 @@ default 1.5 turns per second</short_desc>
<long_desc>Global gain of the controller. This gain scales the P, I and D terms of the controller: output = MC_YAWRATE_K * (MC_YAWRATE_P * error + MC_YAWRATE_I * error_integral + MC_YAWRATE_D * error_derivative) Set MC_YAWRATE_P=1 to implement a PID in the ideal form. Set MC_YAWRATE_K=1 to implement a PID in the parallel form.</long_desc>
<short_desc>Serial Configuration for RC Input Driver</short_desc>
<long_desc>Configure on which serial port to run RC Input Driver. Setting this to 'Disabled' will use a board-specific default port for RC input.</long_desc>
<short_desc>Baudrate for the GPS 1 Serial Port</short_desc>
<long_desc>Configure the Baudrate for the GPS 1 Serial Port. Note: certain drivers such as the GPS can determine the Baudrate automatically.</long_desc>
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@@ -9114,6 +9180,39 @@ is less than 50% of this value</short_desc>
<short_desc>Baudrate for the Radio Controller Serial Port</short_desc>
<long_desc>Configure the Baudrate for the Radio Controller Serial Port. Note: certain drivers such as the GPS can determine the Baudrate automatically.</long_desc>
<short_desc>Baudrate for the TELEM 1 Serial Port</short_desc>
<long_desc>Configure the Baudrate for the TELEM 1 Serial Port. Note: certain drivers such as the GPS can determine the Baudrate automatically.</long_desc>
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@@ -9616,6 +9715,7 @@ is less than 50% of this value</short_desc>
