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Navigational Fix
Alexander Burton, CFI
Pacific Rim Aviation Academy Inc.
Pitt Meadows Regional Airport
393-11465 Baynes Road
Pitt Meadows, BC V3Y 2B4
“Though pleas'd to see the dolphins play,
I mind my compass and my way.”
- Matthew Green –
Last month, we discussed the Line of Position: how to
establish one either electronically
or visually and how to use one to facilitate locating
ourselves in this complex, sometimes
confusing world.
Learning to establish a Line of Position is an excellent
practice and can be very helpful in
pinpointing our position while enroute. Whether we do this
visually or with reference of a
navigational aid the same principles apply. We want to
determine where we are in
relation to a known, fixed point.
The basic principle of developing a Line of Position is to
establish a bearing FROM a
known point using either a visual or electronic reference
and extend that line outward
from the reference point. Your position lies along that Line
of Position. If we are
comfortable in establishing one Line of Position,
establishing two or more should not
present any significant difficulties.
With a Line of Position and a geographic reference or Lines
of Position from two or more
reference points or two or more Lines of Position from the
same reference point we can
locate our position over the ground, establishing a “fix” or
exact position quite easily.
There are a number of techniques we can use to establish a
fix, so let’s take a look at
some common ones.
A Line of Position from one reference point, a VOR, NDB or
visual reference can be
used in conjunction with any geographic reference, for
example a road, railroad track,
power line, coastline, river or lake to establish a fix. We
establish the Line of Position,
draw it on our chart and observe where it crosses a
geographic reference within our sight
radius to locate ourselves. What could be simpler?
If two NDBs, two VORs, or an NDB and a VOR are available,
they can be used together
to develop two Lines of Position, or more if we really want
to be precise, which will
locate or “fix” our position fairly precisely. Typically,
when using three or more Lines of
Position, we will end up with a small triangle rather than a
single point of intersection.
We are located within that triangle (1).
If we have two receivers in the aircraft, a VOR and an ADF,
two VORs or two ADFs, we
can establish the two Lines of Position at about the same
moment. With only one
receiver, there will be a necessary time lag between each
reading, building in an
inevitable error. Normally, this will not be a significant
problem at the speeds we fly with
small aircraft. SR-71 pilots, however, should take note.
To generate a fix using more than one navigation aid,
develop a Line of Position from
each reference, draw them on your chart, and observe where
the lines cross. This is your
position. When flying VFR, if we can locate ourselves within
even a two to three mile
radius, visual references should do the rest of the job
nicely.
If only one navigation aid is available to us, we can still
fix our position accurately. One
method is to use a variation on the 1 in 60 rule: a one
degree difference in track over 60
NM results in a difference of 1 NM in position. This basic
rule allows us to generate
several, useful relationships (2).
With reference to a single VOR station, for example, we can
develop a Line of Position
by determining the radial over which we are flying, turn 80
degrees right or left from the
inbound heading, the reciprocal of the radial, set the OBS
to the nearest 10 degree
increment opposite the direction of the turn and note the
elapsed time when the CDI
centres (3). The 10 degree bearing change is arbitrary; it
just keeps our math problem
simpler.
If we are using an NDB for reference, we establish an
initial Line of Position by using the
tail of the needle to indicate the outbound track over which
we are flying. Turn to and
maintain a heading 80 degrees right or left of the inbound
heading, the reciprocal of our
Line of Position, and note the time it takes us to fly
through 10 degrees of heading change
in relation to the station.
We can now calculate distance to the station using the 1 in
60 rule.
We use the formula: distance to the station is equal to our
speed times minutes flown
divided by number of degrees between bearings. If we want to
be a bit more precise, we
can use seconds flown divided by 60 to obtain our number for
minutes. If we are flying at
100 Kts., for example, and it has taken us five minutes, 300
seconds, to cover 10 degrees
of bearing change relative to our reference point, we are 50
NM out from the reference
along our second Line of Position (100 x 5/10 = 50) (4).
To locate ourselves, to “fix our position”, we measure 50 NM
out from the station along
our second Line of Position and there we are. The key is to
be familiar and comfortable
with the method through practice on the ground before
attempting it in the air.
Another method we can use requiring only one point of
reference, VOR, NDB, or visual
reference point, is to establish a Line of Position from our
reference point, draw the line
on our chart and fly at something close to right angles to
that Line of Position for 6
minutes, or some increment of 6. Make certain you maintain
constant heading during this
procedure. Then, establish a second Line of Position from
the same reference point or
navigation aid. I suggest six minutes for a reason; I want
to keep this simple.
We now have two Lines of Position plotted on our chart. We
also have our heading and
distance flown, not counting wind. The 6 minutes now comes
in very handy to keep the
math in check. At 90 Kts, discounting wind effects, we will
fly 9 NM in 6 minutes; at 130
Kts, we will fly 13 NM in 6 minutes (5).
We can now transfer the distance and heading we have flown
to our chart starting at our
first Line of Position, perhaps using a pencil or our
fingers to represent the distance. That
distance at a particular heading will fit at only one place
between the two, diverging
Lines of Position. Our current position is the point where
our line of travel touches the
second Line of Position. Try it a couple of times at the
comfort of your desk and you will
see how simple it is.
With VOR, ADF or a visual reference we can also use a couple
of simple geometric
relationship to determine our distance from a given point: a
45 degree right triangle has
equal sides; the sides of a 30, 60 degree right triangle
have a special relationship for
lengths: 1,
√3, 2. One represents the base leg and
2 the hypotenuse. We could, of course,
use other right triangle relationships, or even trig
functions, but let’s not get too crazy
here.
The NDB or visual reference problem is a littler simpler
(less math), so I’ll focus on that.
With reference to the 45 degree triangle relationship, turn
the aircraft until the relative
bearing on the ADF or the relative bearing to the visual
reference is either 45 or 315
degrees; note your heading and take the time (T 1).
Maintain that heading until achieving a
relative bearing of 90 or 270 degrees, a change in bearing
of 45 degrees; take the time
(T 2).
The time interval you have recorded will be equal to the
time required to fly to the
reference point from your position at T 2.
Distance to the station, necessary to determine
your position, is speed times time in minutes divided by 60;
for example, 12 minutes at
100 Kts is 20 NM (100 x 12/60 = 20) (6). In this example,
your position is 20 NM from
the reference point along your second Line of Position.
To make use of the special length relationships of the 30
degree right triangle, establish a
relative bearing of 60 degrees or 300 degrees; note your
heading and take the time (T 1).
Maintain that heading until achieving a relative bearing of
90 or 270 degrees, a change in
bearing of 30 degrees, and take the time (T 2).
The time to fly to the station from your
position at T 2
will be 1.7 (√3)
times the time interval you have recorded between T1
and
T 2.
Perhaps a bit simpler method using ADF is to establish a
relative bearing of either 90 or
270 degrees, note heading and time (T 1),
maintain heading until your relative bearing is
either 120 or 240 degrees and take the time (T 2).
From your position at T2,
time to the
station will be twice the time from T 1
to T2.
You can do the distance calculation as you would for the 45
degree triangle.
Playing with and practicing navigational techniques both
visually and electronically in a
safe and known environment will enable you to make use of
these techniques when
venturing into unfamiliar areas. Having a few extra tricks
up your sleeve is all to the good
and, of course, it’s pretty cool to learn something new.
Enjoy.
Notes:
1. Ideally, the angle of interception between Lines of
Position extending from reference points and your
position will equal 90 degrees. If the reference points are
too close together or too far apart, the angle of
interception formed by the Lines of Position will be too
steep (acute) or too shallow (oblique) to
determine an accurate “fix” or position. You can easily draw
some triangles and see the problem. As the
reference points get closer or farther apart in relation to
your position the inevitable error in the bearing
of your Lines of Position is magnified.
2. Distance between bearings/Distance to station = Degrees
between bearings/60; Distance between
bearings = speed x minutes flown/60; Distance to station =
TAS x minutes flown/Degrees between
bearings; Time to station = 60 x minutes flown between
bearings/Degrees between bearings.
3. Using an 80 degree turn averages out the difference in
heading between the two radials we will be using.
A 90 degree heading from our first radial tends to emphasize
the difference in radial headings and
increases the error factor in the angles. If you draw the
problem out you will see what this compromise is
attempting to achieve. However, no need to get overly
excited about the differences.
4. Although the formula calls for TAS, at the speeds and
altitudes we fly in small VFR aircraft, I wouldn’t
worry too much about the conversions required to obtain TAS.
Use your IAS and things will normally
work out within limits you can easily live with.
5. 100 Kts = 100 NM/60 minutes or 10 NM/6 minutes. This
works for any speed. Using a larger increment
of 6, for example 12, simply doubles the distance flown: 100
Kts = 200 NM/120 minutes or 20 NM in 12
minutes. For small aircraft flying at around 100 Kts, 6
minutes will normally be a sufficient amount of
time to produce usable results. This method does not, of
course, factor in ground speed resulting from the
effects of wind. However, over a reasonably short distance,
unless the wind is very strong, we should still
be able to produce quite usable results. Unless we are on a
precision bombing mission, we only need to
locate ourselves within a reasonable radius and then revert
to visual reference.
6. Distance = 100NM/1 hour x 1 hour/60 minutes x 12 minutes
= 20 NM. Or, more simply, use your handydandy
E6B to compute that 12 minutes of flying at 100 Kts = 20 NM.
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