AUTOMATIC COLL. PITCH
The automatic c.pitch action of the rescue features (2b) and (3b) overrides the pilot‘s c.pitch commands more and more with increasing gain setting at the Hor.-Channel. A
signal of -100% (according to [Diagnose] menu) completely overrides the x.pitch stick commands, which is the highly recommended setup. Furthermore, the rescue mode
should be triggered only by a spring loaded momentum switch, so that the pilot re-gains full control by releasing the switch.
NOTE ABOUT THE RESCUE OPTIONS (EXTENDED 3D LEVELING MODES)
The described rescue options provide an extremely high reliability, even during extreme 3D and acro maneuvers, acted in accordance with our rules for setup and hand-
ling. The sensors‘ immunity against vibrations, particularly of the Horizon-stabilisation, is unmatched.
We see this feature as a highly effi cient rescue option, as well as a training chance for un-familiar acro maneuvers.
However we warn to not go for any risks, particularly not to pull the rescue button for testing without fl ying in suffi cient safety altitude, unless being in a real trouble situati-
on. Likewise, nobody would use an emergency-only parachute for regular skydiving. As with any complex system, even in model fl ight, unpredictable infl uences have to
be accounted for at any moment. Also note that the leveling can naturally not perform a halt from high speed, and the heli may climb sideward.
The manufacturer confi rms an extremely high reliability of proper operation, but excludes any liability for damages caused by lack of function (no or wrong or delayed
reaction etc.).
TANDEM MIXER
LINKAGE
The linkage of the two swashplates requires the use of 4 servos, 2 pieces per swashplate. Since elevator is controlled via c.pitch on a tandem, it must be ensured that the
two swash plates can tend only on aileron. The conventional elevator function must be mechanically disabled (blocked). To achieve this, you need a H4 swashplate with
a V-rod, which is led by servo at 2 ball links per side. As the rods are in V-shape, the elevator function on the swashplate is eliminated. This must be given on both sides
of each swashplate. Please take care that the swashplates are 90 ° aligned to the main rotor shaft. Make sure that the rotation of the swashplates is prevented by swash
drivers. Also note that each linkage is smooth-running, only thus ensures that the swashplate working properly and no mechanical load occurs.
Now please carry out the setup by running the software’s setup wizard as usual.
EXTRAS
In the selection menu for the swashplate type, select „Tandem“. The wizard then skips the sections „Tail gyro“ and „Rigid“ because for the fi rst fl ight there is nothing to
adjust here.
Plug in the servos according to the connection diagram, column “Tandem“. Since the tail servo is omitted, this port can be optionally used for power supply.
The neutral trimming is done as usual on the Trim page. When in this page, set the servo arm to 90 ° and mechanically trim both swashplates horizontally. They should
be centered in between dome plate and center part. Only this way the control via elevator and c.pitch can work optimally.
For hover c.pitch set approx. 2-3° angle of attack on the blades of both rotors.
COLLECTIVE TRAVEL
a) In the Mixer page, see the parameter „Tandem: elevator front portion“ (see also tooltip in PC software). With this parameter you can differentiate the c.pitch
travel of the two swashplates for the elevator function, so that you get more or less collective travel at the tail in relation to the front for the elevator function.
In tandem helicopters generally, the front requires less collective portion. If both travels on front and rear are the same, the helicopter behaves dolphin-like
on elevator commands and the front rotor starts „diving“.
For perfect setup, set both rotors to 0° using the collective stick. Now go elevator full travel forward and measure the angle of attack on the rear rotor’s
lades. Now the front attack angle should be ideally half of the rear’s angle. Example: rear 6°, then set the front to 3°. To reduce the front path, move the
parameter to the left in the negative range, to increase it to the right in the positive range. By experience, a value of -30 is mostly suiting best, but can vary
depending on the heli model.
b) Set negative collective to not more than -3°. Inverse fl ight attitude is impossible anyway, due to missing or incorrect tail gyro effect.
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