chore(templates): Update vehicle templates with latest parameters

amilcarlucas · amilcarlucas · commit 2598c8eef051 · 2026-04-09T22:16:24.000+02:00
diff --git a/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/AirCar_v1/08_batt1.param b/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/AirCar_v1/08_batt1.param
@@ -2,13 +2,13 @@ BATT_AMP_PERVLT,0.02
 BATT_ARM_VOLT,86.801  # Only arm above this voltage, to avoid taking off with insufficient battery capacity
 BATT_CAPACITY,30000  # Total battery capacity specified in the component editor
 BATT_CRT_MAH,0
-BATT_CRT_VOLT,78.1  # (Critical voltage + 0.0) x no. of cells
+BATT_CRT_VOLT,78.1  # Critical failsafe voltage x nr. of cells
 BATT_FS_CRT_ACT,1  # Land ASAP
 BATT_FS_LOW_ACT,2  # Return and land at home or rally point
 BATT_FS_VOLTSRC,0
 BATT_I2C_BUS,0  # Selected in component editor window
 BATT_LOW_MAH,0
-BATT_LOW_VOLT,79.2  # (Low voltage + 0.0) x no. of cells
+BATT_LOW_VOLT,79.2  # Low failsafe voltage x nr. of cells
 BATT_MONITOR,4  # Selected in component editor window
 BATT_VOLT_MULT,12.17
 MOT_BAT_VOLT_MAX,92.4  # Scale the PIDs up when battery voltage is below this threshold
diff --git a/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/Big_Owl/08_batt1.param b/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/Big_Owl/08_batt1.param
@@ -1,12 +1,12 @@
 BATT_ARM_VOLT,50.3004  # Only arm above this voltage, to avoid taking off with insufficient battery capacity
 BATT_CAPACITY,17000  # Total battery capacity specified in the component editor
 BATT_CRT_MAH,0  # Energy consumption not measured
-BATT_CRT_VOLT,45.6  # (Critical voltage + 0.0) x no. of cells
+BATT_CRT_VOLT,45.6  # Critical failsafe voltage x nr. of cells
 BATT_FS_CRT_ACT,1  # Land ASAP
 BATT_FS_LOW_ACT,2  # Return and land at home or rally point
 BATT_FS_VOLTSRC,0  # Using only RAW voltage
 BATT_LOW_MAH,0  # Energy consumption not measured
-BATT_LOW_VOLT,46.8  # (Low voltage + 0.0) x no. of cells
+BATT_LOW_VOLT,46.8  # Low failsafe voltage x nr. of cells
 BATT_MONITOR,3  # Selected in component editor window
 BATT_VOLT_MULT,18.55167  # calibrated using a battery tester device
 MOT_BAT_VOLT_MAX,52.2  # Scale the PIDs up when battery voltage is below this threshold
diff --git a/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/Chimera7/08_batt1.param b/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/Chimera7/08_batt1.param
@@ -2,13 +2,13 @@ BATT_AMP_PERVLT,52.706  # new calibrated value for Mamba F45_128k 4in1 ESC
 BATT_ARM_VOLT,23.5998  # Only arm above this voltage, to avoid taking off with insufficient battery capacity
 BATT_CAPACITY,3000  # Total battery capacity specified in the component editor
 BATT_CRT_MAH,0  # When only 0mAh out of the total 3000mAh remain, trigger critical failsafe
-BATT_CRT_VOLT,21.3  # (Critical voltage + 0.0) x no. of cells
+BATT_CRT_VOLT,21.3  # Critical failsafe voltage x nr. of cells
 BATT_FS_CRT_ACT,1  # Land ASAP
 BATT_FS_LOW_ACT,2  # Return and land at home or rally point
 BATT_FS_VOLTSRC,1  # Let the firmware handle the nasty business of variable and battery dependent internal resistance
 BATT_I2C_BUS,0  # Selected in component editor window
 BATT_LOW_MAH,600  # When only 600mAh out of the total 3000mAh remain, trigger low failsafe
-BATT_LOW_VOLT,21.6  # (Low voltage + 0.0) x no. of cells
+BATT_LOW_VOLT,21.6  # Low failsafe voltage x nr. of cells
 BATT_MONITOR,4  # Selected in component editor window
 BATT_VOLT_MULT,11  # Use a power source with a voltage close to BATT_LOW_VOLT measure with a calibrated voltimeter and adapt this parameter so that the telemetry voltage reading matches it
 MOT_BAT_VOLT_MAX,25.2  # Scale the PIDs up when battery voltage is below this threshold
diff --git a/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/Demo32Motor_PeterHall/08_batt1.param b/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/Demo32Motor_PeterHall/08_batt1.param
@@ -1,12 +1,12 @@
 BATT_ARM_VOLT,14.7  # Only arm above this voltage, to avoid taking off with insufficient battery capacity
 BATT_CAPACITY,3300  # Total battery capacity specified in the component editor
 BATT_CRT_MAH,0
-BATT_CRT_VOLT,13.2  # (Critical voltage + 0.0) x no. of cells
+BATT_CRT_VOLT,13.2  # Critical failsafe voltage x nr. of cells
 BATT_FS_CRT_ACT,1  # Land ASAP
 BATT_FS_LOW_ACT,2  # Return and land at home or rally point
 BATT_FS_VOLTSRC,0
 BATT_LOW_MAH,0
-BATT_LOW_VOLT,14  # (Low voltage + 0.0) x no. of cells
+BATT_LOW_VOLT,14  # Low failsafe voltage x nr. of cells
 BATT_MONITOR,10  # Selected in component editor window
 BATT_SUM_MASK,60
 BATT2_CAPACITY,1800
diff --git a/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/FETtec-5/08_batt1.param b/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/FETtec-5/08_batt1.param
@@ -1,13 +1,13 @@
 BATT_ARM_VOLT,21.4998  # Only arm above this voltage, to avoid taking off with insufficient battery capacity
 BATT_CAPACITY,5000  # Total battery capacity specified in the component editor
 BATT_CRT_MAH,200  # trigger critical failsafe at 25% remaining
-BATT_CRT_VOLT,19.2  # (Critical voltage + 0.0) x no. of cells
+BATT_CRT_VOLT,19.2  # Critical failsafe voltage x nr. of cells
 BATT_FS_CRT_ACT,1  # Land ASAP
 BATT_FS_LOW_ACT,2  # Return and land at home or rally point
 BATT_FS_VOLTSRC,0
 BATT_I2C_BUS,0  # Selected in component editor window
 BATT_LOW_MAH,900  # trigger low failsafe just below 33% remaining
-BATT_LOW_VOLT,21  # (Low voltage + 0.0) x no. of cells
+BATT_LOW_VOLT,21  # Low failsafe voltage x nr. of cells
 BATT_MONITOR,9  # Selected in component editor window
 MOT_BAT_VOLT_MAX,25.2  # Scale the PIDs up when battery voltage is below this threshold
 MOT_BAT_VOLT_MIN,19.2  # Scale the PIDs up when battery voltage is above this threshold
diff --git a/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/GazeboIrisWithTargetFollow/08_batt1.param b/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/GazeboIrisWithTargetFollow/08_batt1.param
@@ -2,13 +2,13 @@ BATT_AMP_PERVLT,17  # new calibrated value for Mamba F45_128k 4in1 ESC
 BATT_ARM_VOLT,15.7  # Only arm above this voltage, to avoid taking off with insufficient battery capacity
 BATT_CAPACITY,1800  # Total battery capacity specified in the component editor
 BATT_CRT_MAH,0  # When only 450mAh out of the total 1800mAh remain, trigger critical failsafe
-BATT_CRT_VOLT,14.2  # (Critical voltage + 0.0) x no. of cells
+BATT_CRT_VOLT,14.2  # Critical failsafe voltage x nr. of cells
 BATT_FS_CRT_ACT,1  # Land ASAP
 BATT_FS_LOW_ACT,2  # Return and land at home or rally point
 BATT_FS_VOLTSRC,0  # Let the firmware handle the nasty business of variable and battery dependent internal resistance
 BATT_I2C_BUS,0  # Selected in component editor window
 BATT_LOW_MAH,0  # When only 450mAh out of the total 1800mAh remain, trigger low failsafe
-BATT_LOW_VOLT,14.4  # (Low voltage + 0.0) x no. of cells
+BATT_LOW_VOLT,14.4  # Low failsafe voltage x nr. of cells
 BATT_MONITOR,4  # Selected in component editor window
 BATT_VOLT_MULT,10.1  # Use a power source with a voltage close to BATT_LOW_VOLT measure with a calibrated voltimeter and adapt this parameter so that the telemetry voltage reading matches it
 MOT_BAT_VOLT_MAX,16.8  # Scale the PIDs up when battery voltage is below this threshold
diff --git a/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/Holybro_X500/08_batt1.param b/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/Holybro_X500/08_batt1.param
@@ -2,13 +2,13 @@ BATT_AMP_PERVLT,36.363998  # Provided by the manufacturer
 BATT_ARM_VOLT,14.7  # Only arm above this voltage, to avoid taking off with insufficient battery capacity
 BATT_CAPACITY,5000  # Total battery capacity specified in the component editor
 BATT_CRT_MAH,0  # No capacity based failsafes, too unreliable
-BATT_CRT_VOLT,13.2  # (Critical voltage + 0.0) x no. of cells
+BATT_CRT_VOLT,13.2  # Critical failsafe voltage x nr. of cells
 BATT_CURR_PIN,3
 BATT_FS_CRT_ACT,1  # Land ASAP
 BATT_FS_LOW_ACT,2  # Return and land at home or rally point
 BATT_FS_VOLTSRC,1
 BATT_LOW_MAH,0  # No capacity based failsafes, too unreliable
-BATT_LOW_VOLT,13.6  # (Low voltage + 0.0) x no. of cells
+BATT_LOW_VOLT,13.6  # Low failsafe voltage x nr. of cells
 BATT_MONITOR,4  # Selected in component editor window
 BATT_VOLT_MULT,18.181999  # Provided by the manufacturer
 BATT_VOLT_PIN,2
diff --git a/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/Holybro_X500_V2/08_batt1.param b/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/Holybro_X500_V2/08_batt1.param
@@ -2,13 +2,13 @@ BATT_AMP_PERVLT,36.363998
 BATT_ARM_VOLT,14.7  # Only arm above this voltage, to avoid taking off with insufficient battery capacity
 BATT_CAPACITY,5000  # Total battery capacity specified in the component editor
 BATT_CRT_MAH,0  # No capacity based failsafes, too unreliable
-BATT_CRT_VOLT,13.2  # (Critical voltage + 0.0) x no. of cells
+BATT_CRT_VOLT,13.2  # Critical failsafe voltage x nr. of cells
 BATT_FS_CRT_ACT,1  # Land ASAP
 BATT_FS_LOW_ACT,2  # Return and land at home or rally point
 BATT_FS_VOLTSRC,0
 BATT_I2C_BUS,0  # Selected in component editor window
 BATT_LOW_MAH,1000  # Fail-safe needs to be responsive at 1000 mAh, no risk taking
-BATT_LOW_VOLT,13.6  # (Low voltage + 0.0) x no. of cells
+BATT_LOW_VOLT,13.6  # Low failsafe voltage x nr. of cells
 BATT_MONITOR,4  # Selected in component editor window
 BATT_VOLT_MULT,18.181999
 MOT_BAT_VOLT_MAX,16.8  # Scale the PIDs up when battery voltage is below this threshold
diff --git a/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/Holybro_X650_LTE/08_batt1.param b/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/Holybro_X650_LTE/08_batt1.param
@@ -2,14 +2,14 @@ BATT_AMP_PERVLT,36.363998  # from https://ardupilot.org/copter/docs/common-holyb
 BATT_ARM_VOLT,22.0998  # Only arm above this voltage, to avoid taking off with insufficient battery capacity
 BATT_CAPACITY,11000  # Total battery capacity specified in the component editor
 BATT_CRT_MAH,0  # No capacity based failsafes, no current monitor
-BATT_CRT_VOLT,19.8  # (Critical voltage + 0.0) x no. of cells
+BATT_CRT_VOLT,19.8  # Critical failsafe voltage x nr. of cells
 BATT_CURR_PIN,4  # from https://ardupilot.org/copter/docs/common-holybro-pixhawk6C.html#battery-monitoring
 BATT_FS_CRT_ACT,1  # Land ASAP
 BATT_FS_LOW_ACT,2  # Return and land at home or rally point
 BATT_FS_VOLTSRC,0  # no current monitor
 BATT_I2C_BUS,0  # Selected in component editor window
 BATT_LOW_MAH,0  # No capacity based failsafes, no current monitor
-BATT_LOW_VOLT,20.4  # (Low voltage + 0.0) x no. of cells
+BATT_LOW_VOLT,20.4  # Low failsafe voltage x nr. of cells
 BATT_MONITOR,3  # Selected in component editor window
 BATT_VOLT_MULT,18.181999  # from https://ardupilot.org/copter/docs/common-holybro-pixhawk6C.html#battery-monitoring
 BATT_VOLT_PIN,8  # from https://ardupilot.org/copter/docs/common-holybro-pixhawk6C.html#battery-monitoring
diff --git a/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/Hoverit_X11+/08_batt1.param b/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/Hoverit_X11+/08_batt1.param
@@ -2,13 +2,13 @@ BATT_AMP_PERVLT,0  # WE DO NOT HAVE A VOLTAGE OR AMP SENSOR , WE TAKE DATA FROM
 BATT_ARM_VOLT,55.2006  # Only arm above this voltage, to avoid taking off with insufficient battery capacity
 BATT_CAPACITY,80000  # Total battery capacity specified in the component editor
 BATT_CRT_MAH,0  # WE DONT HAVE MAH READING SENSOR
-BATT_CRT_VOLT,49.7  # (Critical voltage + 0.0) x no. of cells
+BATT_CRT_VOLT,49.7  # Critical failsafe voltage x nr. of cells
 BATT_FS_CRT_ACT,1  # Land ASAP
 BATT_FS_LOW_ACT,2  # Return and land at home or rally point
 BATT_FS_VOLTSRC,0  # AS EPR OUR PREVIOUS DRONE SETUP
 BATT_I2C_BUS,0  # Selected in component editor window
 BATT_LOW_MAH,0  # WE DONT HAVE A MAH SENSOR
-BATT_LOW_VOLT,50.4  # (Low voltage + 0.0) x no. of cells
+BATT_LOW_VOLT,50.4  # Low failsafe voltage x nr. of cells
 BATT_MONITOR,9  # Selected in component editor window
 BATT_VOLT_MULT,0  # WE DONT HAVE A VOLT METER
 MOT_BAT_VOLT_MAX,58.8  # Scale the PIDs up when battery voltage is below this threshold
diff --git a/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/Hoverit_X13/08_batt1.param b/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/Hoverit_X13/08_batt1.param
@@ -2,13 +2,13 @@ BATT_AMP_PERVLT,0  # WE TAKE DATA FROM ESC TELEMETRY, so this can stay at 0
 BATT_ARM_VOLT,55.2006  # Only arm above this voltage, to avoid taking off with insufficient battery capacity
 BATT_CAPACITY,160000  # Total battery capacity specified in the component editor
 BATT_CRT_MAH,0  # WE DONT HAVE MAH READING SENSOR
-BATT_CRT_VOLT,49.7  # (Critical voltage + 0.0) x no. of cells
+BATT_CRT_VOLT,49.7  # Critical failsafe voltage x nr. of cells
 BATT_FS_CRT_ACT,1  # Land ASAP
 BATT_FS_LOW_ACT,2  # Return and land at home or rally point
 BATT_FS_VOLTSRC,0  # AS PER OUR PREVIOUS DRONE SETUP
 BATT_I2C_BUS,0  # Selected in component editor window
 BATT_LOW_MAH,0  # WE DONT HAVE A MAH SENSOR
-BATT_LOW_VOLT,50.4  # (Low voltage + 0.0) x no. of cells
+BATT_LOW_VOLT,50.4  # Low failsafe voltage x nr. of cells
 BATT_MONITOR,9  # Selected in component editor window
 BATT_VOLT_MULT,0  # WE TAKE DATA FROM ESC TELEMETRY, so this can stay at 0
 MOT_BAT_VOLT_MAX,58.8  # Scale the PIDs up when battery voltage is below this threshold
diff --git a/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/Marmotte5v2/08_batt1.param b/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/Marmotte5v2/08_batt1.param
@@ -2,13 +2,13 @@ BATT_AMP_PERVLT,64  # new calibrated value for Mamba F45_128k 4in1 ESC
 BATT_ARM_VOLT,23.5998  # Only arm above this voltage, to avoid taking off with insufficient battery capacity
 BATT_CAPACITY,1400  # Total battery capacity specified in the component editor
 BATT_CRT_MAH,100  # When only 100mAh out of the total 1400mAh remain, trigger critical failsafe
-BATT_CRT_VOLT,21.3  # (Critical voltage + 0.0) x no. of cells
+BATT_CRT_VOLT,21.3  # Critical failsafe voltage x nr. of cells
 BATT_FS_CRT_ACT,1  # Land ASAP
 BATT_FS_LOW_ACT,2  # Return and land at home or rally point
 BATT_FS_VOLTSRC,1  # Let the firmware handle the nasty business of variable and battery dependent internal resistance
 BATT_I2C_BUS,0  # Selected in component editor window
 BATT_LOW_MAH,300  # When only 300mAh out of the total 1400mAh remain, trigger low failsafe
-BATT_LOW_VOLT,21.6  # (Low voltage + 0.0) x no. of cells
+BATT_LOW_VOLT,21.6  # Low failsafe voltage x nr. of cells
 BATT_MONITOR,4  # Selected in component editor window
 BATT_VOLT_MULT,11.1  # Use a power source with a voltage close to BATT_LOW_VOLT measure with a calibrated voltimeter and adapt this parameter so that the telemetry voltage reading matches it
 MOT_BAT_VOLT_MAX,25.2  # Scale the PIDs up when battery voltage is below this threshold
diff --git a/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/ReadyToSkyZD550/08_batt1.param b/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/ReadyToSkyZD550/08_batt1.param
@@ -2,13 +2,13 @@ BATT_AMP_PERVLT,29.87824  # measured/calibrated
 BATT_ARM_VOLT,23.5998  # Only arm above this voltage, to avoid taking off with insufficient battery capacity
 BATT_CAPACITY,6500  # Total battery capacity specified in the component editor
 BATT_CRT_MAH,1625  # trigger critical failsafe at 25% remaining
-BATT_CRT_VOLT,21.3  # (Critical voltage + 0.0) x no. of cells
+BATT_CRT_VOLT,21.3  # Critical failsafe voltage x nr. of cells
 BATT_FS_CRT_ACT,1  # Land ASAP
 BATT_FS_LOW_ACT,2  # Return and land at home or rally point
 BATT_FS_VOLTSRC,1  # Let the firmware handle the nasty business of variable and battery dependent internal resistance
 BATT_I2C_BUS,0  # Selected in component editor window
 BATT_LOW_MAH,2000  # trigger low failsafe just below 33% remaining
-BATT_LOW_VOLT,21.6  # (Low voltage + 0.0) x no. of cells
+BATT_LOW_VOLT,21.6  # Low failsafe voltage x nr. of cells
 BATT_MONITOR,4  # Selected in component editor window
 BATT_VOLT_MULT,18.97948  # measured/calibrated
 MOT_BAT_VOLT_MAX,26.1  # Scale the PIDs up when battery voltage is below this threshold
diff --git a/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/TarotFY680Hexacopter/08_batt1.param b/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/TarotFY680Hexacopter/08_batt1.param
@@ -2,13 +2,13 @@ BATT_AMP_PERVLT,117.6  # 6 motors, but only 4 on the current sensing ESC, so 1.5
 BATT_ARM_VOLT,22.9998  # Only arm above this voltage, to avoid taking off with insufficient battery capacity
 BATT_CAPACITY,5500  # Total battery capacity specified in the component editor
 BATT_CRT_MAH,0  # No capacity based failsafes, too unreliable
-BATT_CRT_VOLT,20.7  # (Critical voltage + 0.0) x no. of cells
+BATT_CRT_VOLT,20.7  # Critical failsafe voltage x nr. of cells
 BATT_FS_CRT_ACT,1  # Land ASAP
 BATT_FS_LOW_ACT,2  # Return and land at home or rally point
 BATT_FS_VOLTSRC,0
 BATT_I2C_BUS,0  # Selected in component editor window
 BATT_LOW_MAH,100  # Fail-safe needs to be responsive at 1000 mAh, no risk taking
-BATT_LOW_VOLT,21  # (Low voltage + 0.0) x no. of cells
+BATT_LOW_VOLT,21  # Low failsafe voltage x nr. of cells
 BATT_MONITOR,4  # Selected in component editor window
 BATT_VOLT_MULT,21.35235  # measured with multimeter
 MOT_BAT_VOLT_MAX,25.2  # Scale the PIDs up when battery voltage is below this threshold
diff --git a/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/Tarot_X4/08_batt1.param b/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/Tarot_X4/08_batt1.param
@@ -1,13 +1,13 @@
 BATT_ARM_VOLT,18.7998  # Only arm above this voltage, to avoid taking off with insufficient battery capacity
 BATT_CAPACITY,30000  # Total battery capacity specified in the component editor
 BATT_CRT_MAH,0  # Energy consumption not measured
-BATT_CRT_VOLT,16.5  # (Critical voltage + 0.0) x no. of cells
+BATT_CRT_VOLT,16.5  # Critical failsafe voltage x nr. of cells
 BATT_FS_CRT_ACT,1  # Land ASAP
 BATT_FS_LOW_ACT,2  # Return and land at home or rally point
 BATT_FS_VOLTSRC,0  # Using only RAW voltage
 BATT_I2C_BUS,2  # Selected in component editor window
 BATT_LOW_MAH,0  # Energy consumption not measured
-BATT_LOW_VOLT,18.6  # (Low voltage + 0.0) x no. of cells
+BATT_LOW_VOLT,18.6  # Low failsafe voltage x nr. of cells
 BATT_MONITOR,21  # Selected in component editor window
 MOT_BAT_VOLT_MAX,24.6  # Scale the PIDs up when battery voltage is below this threshold
 MOT_BAT_VOLT_MIN,16.5  # Scale the PIDs up when battery voltage is above this threshold
diff --git a/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/X11_plus/08_batt1.param b/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/X11_plus/08_batt1.param
@@ -2,13 +2,13 @@ BATT_AMP_PERVLT,17
 BATT_ARM_VOLT,23.5998  # Only arm above this voltage, to avoid taking off with insufficient battery capacity
 BATT_CAPACITY,30000  # Total battery capacity specified in the component editor
 BATT_CRT_MAH,0  # No capacity based failsafes, too unreliable
-BATT_CRT_VOLT,21.3  # (Critical voltage + 0.0) x no. of cells
+BATT_CRT_VOLT,21.3  # Critical failsafe voltage x nr. of cells
 BATT_FS_CRT_ACT,1  # Land ASAP
 BATT_FS_LOW_ACT,2  # Return and land at home or rally point
 BATT_FS_VOLTSRC,1  # Use sag-compensated voltage limits
 BATT_I2C_BUS,0  # Selected in component editor window
 BATT_LOW_MAH,0  # No capacity based failsafes, too unreliable
-BATT_LOW_VOLT,21.6  # (Low voltage + 0.0) x no. of cells
+BATT_LOW_VOLT,21.6  # Low failsafe voltage x nr. of cells
 BATT_MONITOR,4  # Selected in component editor window
 BATT_VOLT_MULT,12.1
 MOT_BAT_VOLT_MAX,25.2  # Scale the PIDs up when battery voltage is below this threshold
diff --git a/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/diatone_taycan_mxc/4.3.8-params/08_batt1.param b/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/diatone_taycan_mxc/4.3.8-params/08_batt1.param
@@ -2,13 +2,13 @@ BATT_AMP_PERVLT,158.4  # new calibrated value for Mamba F45_128k 4in1 ESC
 BATT_ARM_VOLT,15.7  # Only arm above this voltage, to avoid taking off with insufficient battery capacity
 BATT_CAPACITY,1800  # Total battery capacity specified in the component editor
 BATT_CRT_MAH,450  # When only 450mAh out of the total 1800mAh remain, trigger critical failsafe
-BATT_CRT_VOLT,14.2  # (Critical voltage + 0.0) x no. of cells
+BATT_CRT_VOLT,14.2  # Critical failsafe voltage x nr. of cells
 BATT_FS_CRT_ACT,1  # Land ASAP
 BATT_FS_LOW_ACT,2  # Return and land at home or rally point
 BATT_FS_VOLTSRC,1  # Let the firmware handle the nasty business of variable and battery dependent internal resistance
 BATT_I2C_BUS,0  # Selected in component editor window
 BATT_LOW_MAH,600  # When only 450mAh out of the total 1800mAh remain, trigger low failsafe
-BATT_LOW_VOLT,14.4  # (Low voltage + 0.0) x no. of cells
+BATT_LOW_VOLT,14.4  # Low failsafe voltage x nr. of cells
 BATT_MONITOR,4  # Selected in component editor window
 BATT_VOLT_MULT,10.985  # Use a power source with a voltage close to BATT_LOW_VOLT measure with a calibrated voltimeter and adapt this parameter so that the telemetry voltage reading matches it
 MOT_BAT_VOLT_MAX,16.8  # Scale the PIDs up when battery voltage is below this threshold
diff --git a/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/diatone_taycan_mxc/4.4.4-params/08_batt1.param b/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/diatone_taycan_mxc/4.4.4-params/08_batt1.param
@@ -2,13 +2,13 @@ BATT_AMP_PERVLT,158.4  # new calibrated value for Mamba F45_128k 4in1 ESC
 BATT_ARM_VOLT,15.7  # Only arm above this voltage, to avoid taking off with insufficient battery capacity
 BATT_CAPACITY,1800  # Total battery capacity specified in the component editor
 BATT_CRT_MAH,450  # When only 450mAh out of the total 1800mAh remain, trigger critical failsafe
-BATT_CRT_VOLT,14.2  # (Critical voltage + 0.0) x no. of cells
+BATT_CRT_VOLT,14.2  # Critical failsafe voltage x nr. of cells
 BATT_FS_CRT_ACT,1  # Land ASAP
 BATT_FS_LOW_ACT,2  # Return and land at home or rally point
 BATT_FS_VOLTSRC,1  # Let the firmware handle the nasty business of variable and battery dependent internal resistance
 BATT_I2C_BUS,0  # Selected in component editor window
 BATT_LOW_MAH,600  # When only 450mAh out of the total 1800mAh remain, trigger low failsafe
-BATT_LOW_VOLT,14.4  # (Low voltage + 0.0) x no. of cells
+BATT_LOW_VOLT,14.4  # Low failsafe voltage x nr. of cells
 BATT_MONITOR,4  # Selected in component editor window
 BATT_VOLT_MULT,10.985  # Use a power source with a voltage close to BATT_LOW_VOLT measure with a calibrated voltimeter and adapt this parameter so that the telemetry voltage reading matches it
 MOT_BAT_VOLT_MAX,16.8  # Scale the PIDs up when battery voltage is below this threshold
diff --git a/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/diatone_taycan_mxc/4.5.x-params/08_batt1.param b/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/diatone_taycan_mxc/4.5.x-params/08_batt1.param
diff --git a/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/diatone_taycan_mxc/4.6.x-params/08_batt1.param b/ardupilot_methodic_configurator/vehicle_templates/ArduCopter/diatone_taycan_mxc/4.6.x-params/08_batt1.param
