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Measured Range Accuracy of the Hermes A-3 Digital Computer as Affected By (a) Certain Guidance Systems Tolerances (b) Winds and Finite Ground Loop Response

机译：爱马仕a-3数字计算机的测量范围精度受（a）某些制导系统公差的影响（b）风和有限地面环路响应

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摘要

Deviations of the kermes A-3 flight path from the standard trajectory in elevation and azimuth require small correction to be made in the competed range of the missile. This study was made to determine if the corrections, corresponding to expected flight path devastations, were small enough to be neglected in the digital computer.

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P. G. Cushman; J. J. Weinstein;
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年度 1951
页码 1-18
总页数 18
原文格式 PDF
正文语种 eng
中图分类工业技术;
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5. Linear second-order system solution accuracies with digital, analog and hybrid computer methods. [D] . Camire, Guy A. 1983

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Measured Range Accuracy of the Hermes A-3 Digital Computer as Affected By (a) Certain Guidance Systems Tolerances (b) Winds and Finite Ground Loop Response

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