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Radar System Engineering

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SEC. 7.2] AIDS TO INDIVIDUAL NAVIGATION 217<br />

marker. Once this index has been set on a radar echo by means of<br />

adjusting knobs provided on the device, the index will move across the<br />

face of the tube with the echo, provided that the wind setting has been<br />

made properly, regardless of maneuvers of the aircraft.<br />

A simplified schematic diagram of the GPI is shown in Fig. 7.3. To<br />

the left of the box marked “ Rectangular to polar coordinate resolv w,”<br />

the device is identical with the dead-reckoning computer just described.<br />

Since the basic coordinates of the PPI are range and azimuth, it is necessary<br />

to convert the cartesian position information to polar coordinates;<br />

this is done in the resolver shown. The azimuth resulting from this<br />

operation is compared with the instantaneous azimuth of the radar<br />

True<br />

air<br />

speed<br />

N.S fix knob<br />

Compass<br />

repeater — SpeedD<br />

4 ON-S rate knob Altitude knob<br />

1,<br />

&ound position<br />

integrators for<br />

N-S and E-W<br />

components<br />

wind constant.speed speed<br />

mechanism a E-Wrate knob<br />

.* Azimuth from<br />

radar scanner<br />

E-Wfix knob<br />

FIG. 7.3.—Simplifiedschematicdiagram of Ground Position Indicator.<br />

scanner. When the two are equal, an azimuth mark is put on the radar<br />

indicator electronically.<br />

The range information provided by the resolver is measured horizontally<br />

along the ground; it must be corrected for the altitude of the<br />

aircraft if, as is usual, slant range is displayed by. the radar indicator.<br />

This is done by means of the electrical triangle-solver labeled ‘‘ Slant range<br />

circuit, “ into which the value of aircraft altitude is set by the operator.<br />

The value of slant range computed by this device is used to put a range<br />

marker on the PPI at the appropriate distance from the origin of the<br />

sweep.<br />

Taking a fix with the GPI involves turning the Ii-S and E-W fix knobs<br />

until the intersection of the range and azimuth marks appears on top of<br />

an identified target signal. The “fix” dials will then read the ground<br />

range of the target from the aircraft, resolved into north-south and eastwest<br />

components. As the aircraft moves, these dials will continue to<br />

read the correct position of the target relative to the aircraft and the

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