51
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Model Basic Setting Procedure
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match take off and landing and vertical climb at
a constant speed.
*For this curve, use the initial setting [Linear] curve
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[Separate] mode.
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fuselage is facing straight ahead when heading
into the wind.
*For this curve, [Linear] curve type can be used
and the entire curve can be lowered with the
[Offset] button.
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This function is set so that the fuselage is facing
straight ahead during straight line auto rotation.
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*For this curve, [Linear] curve type can be used
and the entire curve can be lowered with the
[Offset] button.
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The mixing rise characteristic of pitch operation
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which temporarily increases and decreases the
mixing amount, can be set.
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pitch interaction
The swash mix function is used to correct the swash plate
in the aileron (roll) direction and elevator (cyclic pitch)
corresponding to each operation of each condition.
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RPM loss caused by swash operation of aileron or elevator
can be corrected with the Throttle Mix function in the Model
Menu. The effects of clockwise and counterclockwise torque
applied when pirouetting can also be corrected.
10. Gyro sensitivity and mode switching
The gyro sensitivity and mode switching function is
dedicated to gyro mixing for each model used, and can be set for
each condition.
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maximum
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minimum
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this function may not have any affect at high gyro
sensitivity.
11. Throttle cut setting
Throttle cut provides an easy way to stop the engine, by
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functional at high throttle to avoid accidental dead sticks. The
switch’s location and direction must be chosen, as it defaults to
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*With throttle stick at idle, adjust the cut position until the
engine consistently shuts off, but throttle linkage is not
binding. When finished, touch the “Throttle Cut” button to
exit.
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This mixing is used with engines with a construction
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The needle servo rise characteristics at throttle
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which use a fuel mixture control carburetor.
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This mixing is dedicated governor mixing when a
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switched for each condition.
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Summary of Contents for T32MZ
Page 1: ...1M23Z06801 INSTRUCTION MANUAL ...
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