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METHOD OF DETERMINING MODULUS OF VELOCITY OF BALLISTIC TARGET IN GROUND-BASED RADAR STATION

机译:确定地面雷达站弹道目标速度模量的方法

摘要

FIELD: radio engineering, communication.;SUBSTANCE: method comprises measuring range and altitude of a ballistic target through time intervals equal to the scanning period T0 of radar stations; determining an estimate of the altitude of the ballistic target in the middle of the observation interval <mrow><msub><mover accent="true"><mi>z</mi><mo>^</mo></mover><mrow><mi>m</mi><mi>d</mi></mrow></msub></mrow> through weighted summation of N digital altitude measurements; determining an estimate of a second increment of the square of the range <mrow><msub><mover accent="true"><mi>Δ</mi><mo>^</mo></mover><mn>2</mn></msub><msup><mi>r</mi><mn>2</mn></msup></mrow> for scanning through weighted summation of N digital signals of squares of range; determining the geocentric angle between the radar station and the ballistic target in the middle of the observation interval using the formula <mrow><msub><mi>γ</mi><mrow><mi>m</mi><mi>d</mi></mrow></msub><mo>=</mo><mi>t</mi><mi>a</mi><msup><mi>n</mi><mrow><mo>−</mo><mn>1</mn></mrow></msup><mfrac><mrow><msqrt><mrow><msubsup><mi>r</mi><mrow><mi>m</mi><mi>d</mi></mrow><mn>2</mn></msubsup><mo>−</mo><msubsup><mover accent="true"><mi>z</mi><mo>^</mo></mover><mrow><mi>m</mi><mi>d</mi></mrow><mn>2</mn></msubsup></mrow></msqrt></mrow><mrow><msub><mi>R</mi><mi>E</mi></msub><mo>+</mo><msub><mover accent="true"><mi>z</mi><mo>^</mo></mover><mrow><mi>m</mi><mi>d</mi></mrow></msub></mrow></mfrac><mo>,</mo></mrow> where rmd is the range to the ballistic target in the middle of the observation interval, RE is the radius of the Earth; determining gravitational acceleration in the middle of the observation interval using the formula <mrow><msub><mi>g</mi><mrow><mi>m</mi><mi>d</mi></mrow></msub><mo>=</mo><msub><mi>g</mi><mn>0</mn></msub><msup><mrow><mrow><mo>(</mo><mrow><mfrac><mrow><msub><mi>R</mi><mi>E</mi></msub><mi>c</mi><mi>o</mi><mi>s</mi><msub><mi>γ</mi><mrow><mi>m</mi><mi>d</mi></mrow></msub></mrow><mrow><msub><mi>R</mi><mi>E</mi></msub><mo>+</mo><msub><mover accent="true"><mi>z</mi><mo>^</mo></mover><mrow><mi>m</mi><mi>d</mi></mrow></msub></mrow></mfrac></mrow><mo>)</mo></mrow></mrow><mn>2</mn></msup><mo>,</mo></mrow> where g0 is the gravitational acceleration on the surface of the Earth; determining the modulus of the velocity of the ballistic target in the middle of the observation interval on an unperturbed passive area of the trajectory using the formula <mrow><msub><mi>V</mi><mrow><mi>m</mi><mi>d</mi></mrow></msub><mo>=</mo><msqrt><mrow><mfrac><mrow><msub><mover accent="true"><mi>Δ</mi><mo>^</mo></mover><mn>2</mn></msub><msup><mi>r</mi><mn>2</mn></msup></mrow><mrow><msub><mi>T</mi><mn>0</mn></msub><msup><mrow /><mn>2</mn></msup></mrow></mfrac><mo>+</mo><mfrac><mrow><msub><mi>g</mi><mrow><mi>m</mi><mi>d</mi></mrow></msub></mrow><mrow><mi>c</mi><mi>o</mi><mi>s</mi><msub><mi>γ</mi><mrow><mi>m</mi><mi>d</mi></mrow></msub></mrow></mfrac><mrow><mo>(</mo><mrow><msub><mover accent="true"><mi>z</mi><mo>^</mo></mover><mrow><mi>m</mi><mi>d</mi></mrow></msub><mo>+</mo><msub><mi>R</mi><mi>E</mi></msub><mi>s</mi><mi>i</mi><msup><mi>n</mi><mn>2</mn></msup><msub><mi>γ</mi><mrow><mi>m</mi><mi>d</mi></mrow></msub></mrow><mo>)</mo></mrow><mo>−</mo><mfrac><mrow><mn>3</mn><msup><mi>N</mi><mn>2</mn></msup><mo>−</mo><mn>1</mn><mn>3</mn></mrow><mrow><mn>5</mn><mn>6</mn></mrow></mfrac><msup><mrow><mrow><mo>(</mo><mrow><msub><mi>g</mi><mrow><mi>m</mi><mi>d</mi></mrow></msub><mi>c</mi><mi>o</mi><mi>s</mi><msub><mi>γ</mi><mrow><mi>m</mi><mi>d</mi></mrow></msub><msub><mi>T</mi><mn>0</mn></msub></mrow><mo>)</mo></mrow></mrow><mn>2</mn></msup></mrow></msqrt><mo>.</mo></mrow> ;EFFECT: high accuracy of determining the modulus of velocity of a ballistic target in ground-based radar stations with rough measurements of elevation and bearing angles.;4 dwg, 2 tbl
机译:领域:该方法包括通过等于雷达站的扫描周期T 0 的时间间隔来测量弹道目标的范围和高度;确定在观察间隔 <![CDATA [ z ^ m d ]]> 通过对N个数字高度测量值进行加权求和;确定范围 <![CDATA [ Δ ^的平方的第二增量的估计。 2 r 2 ]]> <图像文件=“ 00000056.GIF” he =“ 6” imgContent =“ undefined” imgFormat =“ GIF” wi =“ 8” /> 用于扫描N个范围平方的数字信号的加权求和;使用公式 <![CDATA [ γ 来确定观察间隔中间雷达站与弹道目标之间的地心角 m d = t a n 1 r m d 2 - z ^ m d 2 R E + z ^ m d ]]> <图片文件=“ 00000057.GIF” he =“ 15” imgContent =“ undefined” imgFormat =“ GIF” wi =“ 46” /> 其中r md 是在观察间隔中间到弹道目标的范围,R E 是地球的半径;使用公式 <![CDATA [ g m < mi> d = g 0 < mrow> R E c < / mi> o s γ m d < / mrow> R E + z ^ m d < / msub> 2 ]]> <图像文件=“ 00000058.GIF” he =“ 15” imgContent =“ undefined” imgFormat =“ GIF” wi =“ 46” /> 其中g 0 是地球表面的重力加速度;确定使用公式 <![CDATA [ V < / mi> m d = Δ ^ 2 r 2 T 0 < mrow /> 2 + g m d c o s γ m d mfrac> z ^ m d + R E s i n 2 γ m d 3 N 2 - 1 < mn> 3 5 6 g m d c o s γ m d T 0 2 ]]> <图像文件=“ 00000059.GIF”他=“ 16” imgContent =“ undefined” imgFormat =“ GIF” wi =“ 134” /> ;效果:通过粗略测量地面雷达站中弹道目标的速度模量的高精度仰角和方位角。; 4 dwg,2 tbl

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