GAUI X5 Lite Bedienungsanleitung Seite 40

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Verification of the control directions:
Upper figure:
The figure shows the height control of the model helicopter, with the respective lever motions in remove control systems for
mode I and mode II displayed.
If the angle of attack of the rotor blades is to be increased for lifting, the swash plate must be pushed upwards on the main
rotor shaft by the servos. Observe that the swash plate always remains horizontal and never tilts to the side during its
vertical movements.
Centre figure:
The figure shows the directional control of the model helicopter. The swash plate always has to tilt in the direction into which
the steering command is given. Observe that the swash plate has the same inclination angles to the right and left. The
inclination angles to the front and rear also need to match.
Lower figure:
The figure shows the tail control of the model helicopter. If the remote control steers to the right, the sliding sleeve of the
tail rotor linkage must be pushed towards the gear casing on the tail rotor shaft. If this is not the case, change the running
direction of the tail servo at the transmitter.
Also check the effective direction of the gyro in this context. If the fuselage tip of the helicopter is turned to counter-
clockwise to the left when viewed from above, the sliding sleeve must also be moved towards the gear casing by the gyro.
If this is not the case, change the running direction of the tail servo at the gyro. Then adjust the maximum deflection of the
tail servo at the gyro.
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Upper figure:
The figure shows a throttle and a pitch curve schematic for normal flight and freestyle/aggressive flight.
Please consider these values merely reference points for your personal settings that you need to determine in practical
flight.
Lower figure:
Before measuring the angles of attack for the blades with a pitch scales, check that the swash plate, the pitch compensation
levers and the blade holder linkage levers are aligned parallel with each other. The angle of attach of the rotor blades must
be 0°.
If you move the control lever for the pitch function (in normal flight) all the way down, you should be able to measure an
angle of attach of -2 to -3 ° at the rotor blades. If the control lever is moved all the way to the top, the rotor blades should
achieve an angle of attack of 13°. The maximum negative pitch angle (for freestyle flight) is -13°.
The collective pitch angle is max. +/- 13° and the cyclic pitch angle 10°.
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