Eagle Tree Systems Vector User Manual page 95

2nd Rudder Rx In %
Aileron/M2 Output %
Elevator/M3 Output %
Throttle/M4 Output %
Rudder/M1 Output %
Aux1/M5 Output %
Aux2/M6 Output %
G-Force X Axis
G-Force Y Axis
G-Force Z Axis
Pitch
Roll
Yaw
Climbrate
Vario(TEC Climbrate)
GPS Satellite Count
Receiver RSSI
GPS Groundspeed
GPS Altitude
GPS Course
GPS HDOP
Spektrum Rx Holds
Spektrum Lost Frames
Spektrum Ant A Fades
Spektrum Ant B Fades
The measured pulsewidth at the Vector's 2
The pulsewidth being sent to the Vector's Aileron/M2 output (0% = 1 millisecond,
100% = 2 milliseconds)
The pulsewidth being sent to the Vector's Elevator/M3 output
The pulsewidth being sent to the Vector's Throttle/M4 output
The pulsewidth being sent to the Vector's Rudder/M1 output
The pulsewidth being sent to the Vector's Aux1/M5 output, if configured
The pulsewidth being sent to the Vector's Aux2/M6 output, if configured
The g-force measured in the X axis
The g-force measured in the Y axis
The g-force measured in the Z (vertical) axis
The amount of pitch from level, in degrees
The amount of roll from level, in degrees
The amount of yaw motion, in degrees (When the compass is enabled and
properly calibrated, this represents the heading relative to true North)
The model's present climbrate
The model's present climbrate, after Total Energy Compensation has been applied
The number of satellites in view, as reported by the GPS
The present RSSI %
The present ground speed of the model, as reported by the GPS
The zero referenced altitude, as reported by the GPS
The present true course heading, as reported by the GPS
The present HDOP, as reported by the GPS
Receiver health information from the Spektrum™ Flightlog™ data port. Find the
Spektrum™ Flightlog™ manual online for more information
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Rudder input, if used
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USER GUIDE
95