首页> 外国专利> USE OF ITERATION TO IMPROVE THE CORRECTION OF AGC DEPENDENT CHANNEL-TO-CHANNEL GAIN IMBALANCE

USE OF ITERATION TO IMPROVE THE CORRECTION OF AGC DEPENDENT CHANNEL-TO-CHANNEL GAIN IMBALANCE

机译:使用迭代来改善AGC相关通道间增益失衡的校正

摘要

A mood and apparatus that uses iteration to achieve a better prediction of t he values of the commands needed to balance the gains of .SIGMA. + .DELTA. and .SIGMA. - .DELTA. channels of a radar guidance system, when an imbalance occurs due to a change caused by th e AGC circuitry. An improved method of measuring channel-to-channel gain imbalance versus AGC measurements is provided, which produces modified input values that are used as commands that correct the mismatch during missile flight so that residual error is minimized and more accurate guidance is achieved. The present method is implemented by measuring the gain imbalance at predetermined AGC points during system calibration, and iterating these measurements to produce a relatively small channel-to- channel gain imbalance at the .DELTA.AGC amplifiers. The measured imbalance is then converted to .DELTA.AGC commands and applied roc the .DELTA.AGC amplifiers. The resulting gain imbalance is measured and this value is added to the originally measured value. This iterated value is again converted to .DELTA.AGC commands and applied to the .DELTA.AGC amplifiers, and again the imbalance is measured, and is added to the first measurement. This procedure is repeated until a satisfactory level of error is measured which the proper correction factorthat balances the channel-to-channel gains for each valve o f AGC. These correction factors are stored in a lookup table and are subsequently applied to the missile during flight. The improved apparatus of the present invention comprises a .DELTA.AGC controller containing a lookup table that contains the correction factors determined using the above method and an amplifier control circuit that responds to the correction factors to apply modified gain factors to the .DELTA.AGC amplifiers. These correction factors are applied to the .DELTA.AGC amplifiers during operation of the guidance system to achieve more accurate missile guidance.
机译:一种情绪和设备,它使用迭代来更好地预测平衡.SIGMA增益所需的命令值。 +。和.SIGMA。 -.DELTA。当由于AGC电路引起的变化而引起不平衡时,雷达制导系统的各个通道。提供了一种改进的测量通道间增益不平衡与AGC测量的方法,该方法可产生修改后的输入值,这些输入值可用作在导弹飞行过程中校正失配的命令,从而使残留误差最小化并获得更精确的制导。通过在系统校准期间测量预定的AGC点处的增益不平衡,并重复这些测量以在ΔAGC放大器处产生相对较小的通道间增益不平衡,来实现本方法。然后将测得的不平衡量转换为ΔAGC命令,并应用于ΔAGC放大器。测量所得的增益不平衡,并将该值添加到原始测量值。将该迭代值再次转换为ΔAGC命令,并将其应用于ΔAGC放大器,再次测量不平衡,并将其添加到第一次测量中。重复该过程,直到测量到令人满意的误差水平为止,该误差水平是适当的校正因子,该校正因子平衡了AGC的每个阀的通道间增益。这些校正因子存储在查找表中,随后在飞行过程中应用于导弹。本发明的改进的装置包括:一个ΔAGC控制器,该控制器包含一个查找表,该查找表包含用上述方法确定的校正因子;一个放大器控制电路,该放大器控制电路响应该校正因子,以将修改后的增益因子应用于该ΔAGC。放大器。在制导系统运行期间,将这些校正因子应用于ΔAGC放大器,以实现更精确的导弹制导。

著录项

  • 公开/公告号CA2071557A1

    专利类型

  • 公开/公告日2004-05-12

    原文格式PDF

  • 申请/专利权人 HUGHES AIRCRAFT COMPANY;

    申请/专利号CA19922071557

  • 发明设计人 PRINGLE RICHARD C.;

    申请日1992-06-18

  • 分类号G01S7/40;G01S7/34;H03G3/20;

  • 国家 CA

  • 入库时间 2022-08-21 23:05:15

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