Control Surfaces
Elevator
0°
ROLL AXIS · L/R
Aileron
0°
PITCH AXIS · U/D
RUDDER
0°
YAW AXIS · L/R
THROTTLE
0%
ENGINE POWER
Camera Views
Flight Notes
• AILERONS deflect oppositely to roll the aircraft.
• ELEVATOR controls nose pitch up/down.
• RUDDER yaws left/right around vertical axis.
• THROTTLE drives airspeed simulation.
FREE VIEW
PITCH
ROLL
YAW
Instruments
ATTITUDE INDICATOR
Airspeed
0kts
Altitude
3500ft
Vertical Speed
0 ft/min
EULER ANGLES
PITCH
0°
ROLL
0°
YAW
0°
G-Force
1.0 G