105| USER MANUAL
Motor Energy 1-6 Watt-hours
Integrated ESC power consumption
- can be used to compare motor
efficiencies or thrust skew
Motor Accel 1-6 a.u.
High pass filtered RMS vibration level
measured at ESC - can be used to
compare motor / propeller imbalance
Motor Temp 1-6 °C
ESC temperature measured
from last telemetry update
Motor Status 1-6 bit-field ESC fault condition monitor
GPS Sats Satellites
Number of satellites used for
position calculation by GPS
GPS Hacc meters
Horizontal position accuracy
reported by GPS
GPS Sacc meters / second
Horizontal speed accuracy
reported by GPS
Voltage Volts
Main battery voltage measured
by the flight controller
Current Amps
Total battery current inferred
from ESC measurements
Power Watts Total battery power
Energy Watt-hours
Integrated battery power - to be used
in conjunction with battery recharge
measurements - ascertaining battery
health and expected flight times
Temperature °C Flight controller PCB temperature
Barometric
Altitude
meters
Height above take-off location
derived by pressure measurement
Status a.u.
Flight controller status - indicating
things like auto-land
Fail bitfield
Machine alarm register indicating
particular system failures
GPS Loss
of Signal
binary
Declared if GPS signal is not
adequate for safe position hold
Radio A Drops number Accumulated signal drops from radio A
Radio B Drops number Accumulated signal drops from radio B
Magnetometer
Bad
binary
Alarm indicating compass
magnitude is corrupted
Position Lock binary
Status indicating position
estimation filter has locked
Heading Lock binary Status indicating heading lock is active
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