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Activation of new aaa units - Air Defense Artillery

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1948 DETERl\lINATION OF FIRING ERRORS FOR HEAVY AAA 33<br />

muth and elevation errors are <strong>of</strong> the same order <strong>of</strong> magnitude<br />

and independent <strong>of</strong> each other. Actually, the studies<br />

indicated that the ratio <strong>of</strong> these errors varied from unity to<br />

one and a half. A separate study was made on the degree <strong>of</strong><br />

independence, and a small degree <strong>of</strong> dependence was fOLlnd.<br />

.-\.nadditional study was made to determine the amount <strong>of</strong><br />

error which would be introduced by the assumptions used,<br />

and this study indicated that no significant error resulted.<br />

ihe study described above will, when completed, have<br />

obtained the standard deviations for a large number <strong>of</strong><br />

points in space. Interpolation, and to a lesser extent, extrapolation,<br />

can be used to obtain standard deviations for any<br />

point in space within range <strong>of</strong> the weapon studied. The<br />

distribution <strong>of</strong> firing errors having been determined, there<br />

remains only the problem <strong>of</strong> combining this distribution<br />

with the lethality <strong>of</strong> bursts to obtain an answer to the question,<br />

"What are the capabilities <strong>of</strong> antiaircraft weapons engaging<br />

targets at all altitude and ranges."<br />

The techniques described are applicable not only to the<br />

antiaircraft weapons on which the experimental data were<br />

taken, but to modifications and improvements <strong>of</strong> present<br />

weapons as well as to <strong>new</strong> equipment. Where the behavior<br />

<strong>of</strong> the <strong>new</strong> equipment can be forecast, theoretical explorations<br />

can be made. Where a combination <strong>of</strong> fact

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