Linear mil and north hook
RESTRICTED
Linear
Mil
North
Hook
Fig. 43
surface when the earth
has moved through the
arc
represented by the distance from B to
1. To the
observer it would appear that the spin axis had
changed its position.
Actually the rotation of
the earth has caused
the vertical to change rela-
tive to any point of reference, such as the verti-
cal spin axis of the gyro.
The observer does not
sense this, and so it appears to him
as though the
bottom of
the
gyro's spin axis actually moved to-
ward the east.
A linear mil is an
angle which from the ver-
tical subtends 1/1000th of
its altitude along its
base line. Determine the finear distance subtend-
ed and then any angle,
no matter how far from the
vertical it may be tormed, which subtends this
same linear distance in the same problem
is also
a mil. Actually,
farther the angle proceeds
away from the vertical, the smaller it must become
to subtend the same linear distance.
To reiterate: In computing the amount of re-
lative displacement of the gyro spin axis with the
reference vertical (to the earth's surface) there
are two units of measurement
that can
be consid-
They are degrees and mils.
A degree is l/360th of the circumference of
a circle.
for our purpose,
is an
angle
that will
subtend
A mil 1000th of its altitude along
its base line.
vertical (that is a mil, is the angle formed from
(cat and thich
is determined from
the
subtends 1/1000th of its
altitude), then
as earh
mil angle is formed
far-
ther from
the vertical it becomes progressively
smaller in order to subtend the fixed mil
dis-
be shown mathematically that
the angular increase between the gyro spin axis
and the vertical continues to increase at the same
the spin axis 10 min-
to precess the first 4°
from
the vertical, it
will take it 10
minutes to precess go
the vertical.
farther away the spin
axis deviates
vertical, the greater linear
mii distance
it precesses
for any given period
of time.
North hook is or can be caused by (1) flex-
ible lead
drag,
(2)
bearing drag,
and (3) pendul-
ousness of the
vertical gyro. Notice Fig. 43 for
position of the bearings.
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