Product And Function Description; Functional Description - Multiplex WINGSTABI-7 Mode D'emploi

2. Product and function description

Freely programmable triple-axis gyro system for all RC fixed-wing model air-
craft. Having complete control over your model at all times is the dream of any
pilot. The WINGSTABI makes this dream achievable, and ticks every possible
box for beginners and pro-standard flyers alike in terms of handling, adjustment
and functionality.
· The WINGSTABI makes any simple radio control set into a fully
programmable RC system
· Gain (sensitivity) on all three axes can be varied separately or
jointly from the transmitter
· Variation factor can be set separately for each axis
· 7, 9 channels, or 12, 16 channels Pro versions with integrated battery backer
· The gyro function is freely assignable for each servo,
i.e. the unit caters for every model application
· Delta mixer, V-tail mixer and flap support
· Flaps can be set to amplify aileron response
· Real-time sensor diagram in the PC software
Four flight phases:
1. On/Off
2. Stabilisation for flying in windy conditions
3. Aerobatics and 3D flying
4. Torque-rolling (rock'n'roll at the flying site)
The WINGSTABI is also compatible with all current RC systems:
Graupner, Futaba, M-LINK, Jeti, HiTEC, Weatronic and others.
It supports the following types of signals:
PPM, Futaba S.Bus*, MULTIPLEX SRXL, Graupner SUMD and SUMO, Jeti UDI, JR
XBUX Mode B and S-BUS signal many other systems, such as HiTEC and FrSky.
The latest generation of ultra-precise triple-axis MEMS sensors ensures that the
sensation of flying remains realistic even at extremely high rates of stabilisation,
and the pilot never has the impression of flying a robot. The sleek case, made
of anodised aircraft aluminium, can be installed in any orientation of the model.
The WINGSTABI is straightforward and swift to program using a PC or an APP
with any smartphone or tablet.

Functional description

Heading Hold (HH) is a mode of operation for one or several axes which is
stabilised by means of the gyro, during which signals from the gyro sensors are
evaluated in order to maintain the current flight attitude. The model maintains
the last commanded flight attitude and must be actively commanded into the
next one.
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