The Digitrak is described as employing "gyroscopic rate sensors are
installed so as to sense motion about each of the major axes (roll,
yaw and pitch)."

I assume they mean there is a spinning gryo around which three sensors
are arranged, to sense motion in each axis, pitch, roll and yaw. The
sensors report how much the aircraft has moved around the gyro for
each axis.

From what I can see of the various default instruments in FlightGear,
the only source of roll angle from an instrument is the attitude
indicator or indirectly, the turn coordinator, which the Digitrak does
not use.

I conclude that to model the Digitrak fully, I would need to create C
code to represent this three axis gyro using the gyro.*** code that
the attitude indicator depends on. I have a little experience with C,
but not much. I nearly understand how the attitude indicator works
with the gyro model, but I still have to many questions to comprehend
all it is doing.

I also assume that using /orientation/roll-angle is the best
substitute currently available.

I would appreciate any help with this and please correct me if I am
wrong in any of this.

I think the Digitrak would make an interesting contribution to
FlightGear.

Thanks,

Steve



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