There are basically 3
tems in use at AFMTC for obtaining mi
>tory data. These
1i, and the Askania
are the Ballistic Camera, the
Cine-theodolite.
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instruments and are primarily used tc the tial po-
sition of the misslle along trajectory at | ticular instances
of time. From this position
velocity and acceleration in: the
a += 4 +13 la
avuivuae
Fixed Camera and the
data: the pitch, yaw, and roll, of the missile
ballistic camera syst
instrumentation system to be
-
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Systematic error less he random error) can also be 3
as a range calibration syste
tematic error from any other of r ation
This procedure is currently be: used with the Azusa System.
e a^ f^* dt EN AV de En À cng
grammetry. In essence, this
pendent orientation of each camera to be used in the triangu-
lation net; and second the determination of the most probable
Spatial position by the
each of the separate camera