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METHOD OF ADJUSTING RADAR STATIONS OF AUTOMATIC CONTROL SYSTEM

机译：自动控制系统的雷达站调整方法

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摘要

FIELD: physics; control.;SUBSTANCE: invention can be used in automated air traffic control systems. The result is achieved due to that the disclosed method includes measuring coordinates of a reflecting object, followed by determining adjustment systematic errors; satellite navigators determining Cartesian coordinates of proper points of location of radar stations (X_n, Y_n); the radar station to be adjusted measuring Cartesian coordinates of an aerial object (X_On, Y_On); automatic control systems receiving, through an automatic dependent surveillance radio receiver, coordinates of the current location of the aerial object (X_AZNn, Y_AZNn); interpolating all received Cartesian coordinates to a single moment in time; mathematically averaging the obtained Cartesian coordinates of the aerial object interpolated to a single moment in time

<mrow><msub><mi>X</mi><mrow><mi>m</mi><mi>c</mi></mrow></msub><mo>=</mo><mfrac><mrow><msub><mi>X</mi><mrow><mi>O</mi><mn>1</mn></mrow></msub><mo>+</mo><msub><mi>X</mi><mrow><mi>O</mi><mn>2</mn></mrow></msub><mo>+</mo><mo>⋯</mo><mo>+</mo><msub><mi>X</mi><mrow><mi>O</mi><mi>N</mi></mrow></msub><mo>+</mo><msub><mi>X</mi><mrow><mi>A</mi><mi>Z</mi><mi>N</mi></mrow></msub></mrow><mrow><mi>n</mi><mo>+</mo><mn>1</mn></mrow></mfrac><mo>;</mo></mrow>

<mrow><msub><mi>Y</mi><mrow><mi>m</mi><mi>c</mi></mrow></msub><mo>=</mo><mfrac><mrow><msub><mi>Y</mi><mrow><mi>O</mi><mn>1</mn></mrow></msub><mo>+</mo><msub><mi>Y</mi><mrow><mi>O</mi><mn>2</mn></mrow></msub><mo>+</mo><mo>⋯</mo><mo>+</mo><msub><mi>Y</mi><mrow><mi>O</mi><mi>N</mi></mrow></msub><mo>+</mo><msub><mi>Y</mi><mrow><mi>A</mi><mi>Z</mi><mi>N</mi></mrow></msub></mrow><mrow><mi>n</mi><mo>+</mo><mn>1</mn></mrow></mfrac></mrow>

calculating the adjustment for each of the radar stations to be adjusted

<mrow><mi>Δ</mi><msub><mi>β</mi><mi>n</mi></msub><mo>=</mo><mi>a</mi><mi>r</mi><mi>c</mi><mi>t</mi><mi>g</mi><mrow><mo>(</mo><mrow><mfrac><mrow><msub><mi>Y</mi><mrow><mi>o</mi><mi>n</mi></mrow></msub><mo>−</mo><msub><mi>Y</mi><mi>n</mi></msub></mrow><mrow><msub><mi>X</mi><mrow><mi>o</mi><mi>n</mi></mrow></msub><mo>−</mo><msub><mi>X</mi><mi>n</mi></msub></mrow></mfrac></mrow><mo>)</mo></mrow><mo>−</mo><mi>a</mi><mi>r</mi><mi>c</mi><mi>t</mi><mi>g</mi><mrow><mo>(</mo><mrow><mfrac><mrow><msub><mi>Y</mi><mrow><mi>m</mi><mi>c</mi></mrow></msub><mo>−</mo><msub><mi>Y</mi><mi>n</mi></msub></mrow><mrow><msub><mi>X</mi><mrow><mi>m</mi><mi>c</mi></mrow></msub><mo>−</mo><msub><mi>X</mi><mi>n</mi></msub></mrow></mfrac></mrow><mo>)</mo></mrow><mo>=</mo><mi>a</mi><mi>r</mi><mi>c</mi><mi>t</mi><mi>g</mi><mrow><mo>(</mo><mrow><mfrac><mrow><mfrac><mrow><msub><mi>Y</mi><mrow><mi>o</mi><mi>n</mi></mrow></msub><mo>−</mo><msub><mi>Y</mi><mi>n</mi></msub></mrow><mrow><msub><mi>X</mi><mrow><mi>o</mi><mi>n</mi></mrow></msub><mo>−</mo><msub><mi>X</mi><mi>n</mi></msub></mrow></mfrac><mo>−</mo><mfrac><mrow><msub><mi>Y</mi><mrow><mi>m</mi><mi>c</mi></mrow></msub><mo>−</mo><msub><mi>Y</mi><mi>n</mi></msub></mrow><mrow><msub><mi>X</mi><mrow><mi>m</mi><mi>c</mi></mrow></msub><mo>−</mo><msub><mi>Y</mi><mi>n</mi></msub></mrow></mfrac></mrow><mrow><mn>1</mn><mo>+</mo><mfrac><mrow><msub><mi>Y</mi><mrow><mi>o</mi><mi>n</mi></mrow></msub><mo>−</mo><msub><mi>Y</mi><mi>n</mi></msub></mrow><mrow><msub><mi>X</mi><mrow><mi>o</mi><mi>n</mi></mrow></msub><mo>−</mo><msub><mi>X</mi><mi>n</mi></msub></mrow></mfrac><mo>⋅</mo><mfrac><mrow><msub><mi>Y</mi><mrow><mi>m</mi><mi>c</mi></mrow></msub><mo>−</mo><msub><mi>Y</mi><mi>n</mi></msub></mrow><mrow><msub><mi>X</mi><mrow><mi>m</mi><mi>c</mi></mrow></msub><mo>−</mo><msub><mi>X</mi><mi>n</mi></msub></mrow></mfrac></mrow></mfrac></mrow><mo>)</mo></mrow></mrow>

<mrow><msub><mi>D</mi><mi>n</mi></msub><mo>=</mo><msqrt><mrow><msup><mrow><mrow><mo>(</mo><mrow><msub><mi>X</mi><mrow><mi>m</mi><mi>c</mi></mrow></msub><mo>−</mo><msub><mi>X</mi><mi>n</mi></msub></mrow><mo>)</mo></mrow></mrow><mn>2</mn></msup><mo>+</mo><msup><mrow><mrow><mo>(</mo><mrow><msub><mi>Y</mi><mrow><mi>m</mi><mi>c</mi></mrow></msub><mo>−</mo><msub><mi>Y</mi><mi>n</mi></msub></mrow><mo>)</mo></mrow></mrow><mn>2</mn></msup></mrow></msqrt><mo>−</mo><msqrt><mrow><msup><mrow><mrow><mo>(</mo><mrow><msub><mi>X</mi><mrow><mi>o</mi><mi>n</mi></mrow></msub><mo>−</mo><msub><mi>X</mi><mi>n</mi></msub></mrow><mo>)</mo></mrow></mrow><mn>2</mn></msup><mo>+</mo><msup><mrow><mrow><mo>(</mo><mrow><msub><mi>Y</mi><mrow><mi>o</mi><mi>n</mi></mrow></msub><mo>−</mo><msub><mi>Y</mi><mi>n</mi></msub></mrow><mo>)</mo></mrow></mrow><mn>2</mn></msup></mrow></msqrt><mo>;</mo></mrow>

comparing the calculated adjustments Δβ_n, ΔD_n with the resolution of each of the radar stations to be adjusted and, if the adjustment is greater than the resolution of one of the radar stations to be adjusted, said radar station is re-tuned, and measurements and calculations are repeated until the adjustment value is less than the resolution of all radar stations to be adjusted.;EFFECT: high accuracy of adjustment.;1 dwg

机译：领域：物理学;发明内容：本发明可以用于自动空中交通管制系统中。由于所公开的方法包括测量反射物体的坐标，然后确定调整系统误差，因此获得了结果。卫星导航员确定雷达站的适当位置的直角坐标（X _{n ，Y _{n ）;待调整的雷达台测量空中物体的直角坐标（X _{On ，Y _{On ）;自动控制系统通过依赖于监视的自动无线电接收机接收空中物体当前位置的坐标（X _{AZNn ，Y _{AZNn ）;将所有收到的笛卡尔坐标插值到单个时刻;对获得的插值到单个时刻的空中物体的笛卡尔坐标进行数学平均处理 $<！[CDATA [Xm < / mi>c=XO1+XO2+\dots+XON+XAZNn+1;]]><图像文件=“ 00000018.GIF” he =“ 10” imgContent =“ undefined” imgFormat =“ GIF” wi =“ 62” /><！[CDATA [Ymc=$}}}}}}

著录项

公开/公告号RU2529875C2

专利类型
公开/公告日2014-10-10

原文格式PDF
申请/专利权人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO GOLOVNOE SISTEMNOE KONSTRUKTORSKOE BJURO KONTSERNA PVO ALMAZ-ANTEJ IMENI AKADEMIKA A.A. RASPLETINA (OAO GSKB ALMAZ-ANTEJ);
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申请/专利号RU20120148572
发明设计人 SUKHOV VJACHESLAV VITALEVICH;SAVVATEEV VLADIMIR SERGEEVICH;
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申请日2012-11-15
分类号G01S7/40;
国家 RU
入库时间 2022-08-21 15:38:19

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