GRAUPNER mx-20 Hott Programming Manual page 171

33124.mx-20 hott.1.en
Table of Contents

Advertisement

Tail rotor  throttle
Pitch
C1
Throttle
C1
Tail
Tail
Throttle
Roll
Throttle
Normal
While the tail rotor normally compensates for the effect
of main rotor torque on the fuselage, it is also used to
control the helicopter around the vertical axis. Increasing
tail rotor thrust requires a corresponding adjustment
to motor power, however, to avoid a fall-off in system
rotational speed.
This mixer sets the extent to which the throttle follows
the tail rotor. The throttle will follow on one side only,
to the side on which the tail rotor thrust is increased.
Values in the range 0% to +100% are therefore possible.
The direction depends on the main rotor's direction of
rotation (left or right), and this must fi rst be set correctly
on the "Helicopter type" menu. For left-hand rotation
systems, the throttle follows the tail rotor when the tail
rotor joystick is moved to the left, and vice versa for
right-hand rotation systems.
If you tap the  or  keys on the right touch
pad (CLEAR) at the same time, this will reset values
changed in the active (highlighted) fi eld back to 0%.
In the auto-rotation fl ight phase this mixer is
automatically switched off.
Set-up notes:
To set the mixer value accurately you should either fi rst
fl y several high-speed pirouettes against the direction of
main rotor rotation or, if a strong wind is blowing, hover
at right angles to the wind with a suffi ciently large tail
rotor defl ection. Set the mixer value so that there is no
fall-off in system rotational speed.
Roll  Throttle and Nick  Throttle
C1
0%
Tail
0%
Roll
SEL
Roll
Nick
Normal
Increasing collective pitch is not the only change that
requires the throttle to follow suit: major cyclic control
movements also require this, i. e. if the swashplate is
tilted in any direction. The mx-20 HoTT program lets
you adjust the degree of throttle follow separately for roll
and pitch-axis controls.
This offers particular advantages in aerobatic fl ying, e. g.
when fl ying a roll: here, with moderate collective pitch
values and the carburetor only about half-open, cyclic
control travels are nonetheless executed that require
much higher performance from the motor.
The mixer value can be varied within the range 0 to
+100%. The correct mixer direction is automatically
taken into account.
If you tap the  or  keys on the right touch
pad (CLEAR) at the same time, this will reset values
changed in the active (highlighted) fi eld back to 0%.
In the auto-rotation fl ight phase this mixer is
automatically switched off.
Tail
Throttle
0%
Throttle
0%
Tail
0%
Throttle
0%
SEL
Roll  Tail and Nick  Tail
Roll
Throttle
Roll
Tail
Nick
Throttle
Nick
Tail
Gyro suppress
Normal
Increasing pitch is not the only change that requires a
corresponding torque compensation via the tail rotor:
major cyclic control movements also require this, e.g.
if the swashplate is tilted in any direction. Here, too,
the mx-20 HoTT program lets you confi gure settings
for both types of tilt movement (roll and pitch-axis)
separately.
For advanced aerobatics in particular, which involve
very large control defl ections in the pitch-axis
controls, e. g. the "Bo-turn" (vertical pull-up followed
by tipping over around the pitch-axis) and tight loops,
the uncompensated torque present in these fl ights
causes the model to turn to a greater or lesser degree
around the yaw axis. This spoils the appearance of the
maneuver.
These two mixers permit static torque compensation to
be activated by the swashplate tilting in any direction.
The mixers work by always increasing tail rotor thrust,
starting from the center point of the roll and pitch-axis
sticks, i.e. they always generate a tail rotor defl ection
in the same direction regardless of the direction of the
command.
The mixer value can be varied within the range 0 to
+100%.
The mixer direction is determined automatically by your
defi nition of the direction of main rotor rotation on the
Detail program description - Control adjust
0%
0%
0%
0%
0%
SEL
171

Hide quick links:

Advertisement

Table of Contents
loading

Table of Contents