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Radar System Engineering

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216 THE EMPLOYMENT OF RA DAR DATA [SEC.7.2<br />

of dead-reckoning computers, or odographs, have been developed. The<br />

control box of one such computer is shown in Fig. 72. This device,<br />

developed in the Division 17 program of the NDRC, receives information<br />

from a true-airspeed meter and a repeater compass. These data are<br />

resolved into cartesian velocity components along the north-south and<br />

east-west directions, and these velocity values are integrated to provide<br />

continuous readings of air position with reference to any chosen point of<br />

departure.<br />

A mechanism isalsoprovided to indicate ground position by taking<br />

account of the effect of wind. The direction and speed of the wind (as<br />

determined from double drift readings, meteorological information, comparison<br />

of earlier wind settings with the actual course made good, radar<br />

fixes, or otherwise) can be set into the device by means of knobs shown<br />

in Fig. 7.2. Wind velocity is resolved<br />

into components along the<br />

north-south and east-west directions,<br />

integrated, and. the result<br />

added to the air position to give<br />

the ground position with respecb<br />

to the point of departure.<br />

Air position and actual ground<br />

position both appear on the<br />

counter dials shown at the lower<br />

left. The output signals of the<br />

unit can also be used to actuate<br />

a plotting arm which moves over<br />

1. ..; a map table not shown in Fig.<br />

FIG. 7.2.—Control box of aircraft odograph<br />

or dead-reckoningcomputer.<br />

7.2. With this addition, the device<br />

draws on a map the actual<br />

ground track made good by the aircraft carrying the instrument. Various<br />

map scales can be selected for the plotting table by means of a knob<br />

on the control box. The control box can also be provided with a gear<br />

train that actuates a mechanism showing latitude and longitude directly,<br />

in addition to showing the departure from the last fix. In a carefully<br />

made installation, the cumulative error of this instrument amounts to<br />

only ~ per cent of the total distance traveled from the point of departure.<br />

Ground-position Indicator, GPI.—Although the device just described<br />

aids in performing dead reckoning, and to this extent assists in radar<br />

navigation, it is convenient to present the results of the dead reckoning<br />

directly on the radar scope. This has been done in a device called the<br />

“ Ground-position Indicator,” or GPI.<br />

The GPI provides an electronic index for the PPI tube of the radar<br />

in the form of the intersection of a circle of constant range and an azimuth

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