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Programming examples - Delta and ying wing
»Wing mixers« (beginning page 172)
… menu, is set appropriately in the "HR WK" line to
"Aileron, camber flaps" or, if applicable, "Camber flap 2":
FL.pos
Diff.
Ail-tr.
AI
Normal AILE
+100%
WK2
FLAP
0%
0% 0%
+100%
0%
+100%
0%
+100%
0%
0%
0%0%
+100% 0% 0%
0%
FL
EL FL
+100%
+100%
+100%
+100%
0%0%
0%
0%
0%0% 0%
0%
Note:
Contrary to the separately set aileron
trimming, see below, the trimming is
transferred proportionally to the set mixer
value with the mixer "EL FL".
The following settings are model-
specific and may not be adopted
without checking that they are cor-
rect!
In the top line of this "Multi-flap menu", analogous to
"normal" four, six or eight flap wings, the effect of the
aileron stick will be set to aileron, camber flap and, if
applicable to FL2. One line below, in the line "Ail-tr."
line, will set the influence of aileron trimming on ailer-
ons and camber changing flaps.
The setting of a differentiation is rather tricker due to
the model type and should only take place based on
a feel for the flight behavior of the model.
The line "FL" should then be set to the stand-
ard default of +100 % in the "FLAP" (or "FL2") col-
umn – as shown – to 0 %, just to be safe:
Aileron differential
Brake settings
0%
Aileron 0%
WING MIXERS
Elevator aileron 0%0%
–––
–––
rudder
2
3
4
5
Normal
Due to the specific idiosyncrasies of this model type,
additional settings lead to moments which cannot be
compensated.
Delta/ying wing of the type: "2 / 4 AIL 1 / 2 / 4 FL"
Tail type
Motor on C1 none
Aileron/camber flaps
M O D E L T Y P E
Brake Offset Input 1+100%
SEL
Delt/fl.wing
2 AIL 2 FL
With delta/flying wing constructions with more than
two flaps, more moments can be compensated for.
For example, the "lifting" moment caused by the
raising of the ailerons (= elevator effect) can be com-
pensated with camber changing flaps lowered corre-
spondingly wide ( = hydroplane effect).
If you decide in favor of this model type and have
assigned the receiver outputs in accordance with the
connection plan shown above, the aileron function of
the two (exterior) aileron servos will function correctly
immediately, but not the elevator function of the two
aileron servos and, if applicable, the (interior) camber
changing flaps.
This is only then achieved for "2/4 AIL 1/2/4 FL"
when, in the "Multi-aps menu" of the …
FL.pos
Diff.
Ail-tr.
AI
Normal AILE
+100%
WK2
FLAP
0%
0% 0%
+100%
0%
+100%
0%
+100%
0%
0%
0%0%
+100% 0% 0%
0%
FL
EL FL
+100%0%
0%
0%0%
0%
0%
0%0% 0%
0%
Even though all inputs are set to "free" by default
in the »Control adjust« menu, should a control be
assigned sometime by mistake … then it will at least
have no effect.
The last line, "EL FL", was explained at the begin-
ning of this section.
In principle, the author of this manual had pro-
grammed a delta model years ago operated with the
mc-20 and a crow system as landing assistance
… entirely without tilting moments through corre-
spondingly attuned wing mixers "Brake Aileron"
and "Brake Camber ap", whereby "Aileron" refers
to the exterior rudder pair and "Camber ap" refers to
the interior rudder pair.
To achieve this now with the mc-32 Hott also,
switch to "Brake settings" in the …
»Wing mixers« (beginning page 172)
… menu, and enter the values for the ailerons to be
raised and the "flaps" to be lowered in the "Crow" line
so that the occurring moments compensate one an-
other and the altitude of the model remains stable. In
the process, however, you should leave the flaps with
enough "play" for the elevator function!!! Therefore, do
not utilize the entire servo travel for the crow alone;
for example:
321


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