A single dislocation of logic was present
in the last posting on this topic.
Angle of attack is translated to aircraft
flight vectors with the relation of
force-sec to force for the matrix of hamilton.
Making the implied four state matrix the wing.
And the three dimensional velocity vector
now the aircraft.
Now, the reason for this transformation is
because it works. A cause to its correctness
in theory is rediculously given to parody.
So a short rhym was written:
A wings wind,
a blow and the bounce.
A rhym where the title is also the rhym.
And the word bounce imples the effect of
air inertia.
It will not predict the velocity given
significant stalling. So just write
a flight algorithm with limits to the
velocities. And if a control algorithm was
the intention, then use the airspeed to estimate
the ground speed and use a safety factor
for gusty winds.
Making the exact flight controler emperical
and in need of a special sensor such as an
angle of attack indicator to truely function
safely.
.
|
