发明名称 JUDOHISHOTAI
摘要 <p>PURPOSE:To eliminate the occurrence of a malfunction at the time of low- attitude flight so as to accurately detect the existing direction of an object by determining the intruding quadrant of the object based on the action of a radio target detector and relative speed information from a target inducing device. CONSTITUTION:The existing quadrant of an object 50 is determined based on the detection of reflected waves from a target 50 intruding into a beam emitted from a radio target detector 11 and the firing action of the warhead is commanded by using information regarding the relative speed of the object 50 outputted from a target inducing device 20. In addition, information regarding the distance to the ground surface is prepared from control information based on reflected waves from the ground surface and information regarding the attitude angle of a missile outputted from the device and a steering device is controlled by using these information. Then, by generating information indicating the arriving quadrant direction of the object 50 based on information regarding the existing direction of the object 50 outputted from the device 20, the detector 11 is controlled so that only its quadrant system corresponding to the object existing direction can be operated.</p>
申请公布号 JP2650793(B2) 申请公布日期 1997.09.03
申请号 JP19910023034 申请日期 1991.02.18
申请人 MITSUBISHI PURESHIJON KK;MITSUBISHI DENKI KK 发明人 MAEJIMA TOKUYUKI;MIZUSAKI KATSUO
分类号 B64C13/18;F41G7/22;F42B15/01;F42C13/04;G01S7/34;G01S13/08;G01S13/88;G05D1/10;(IPC1-7):G01S13/88 主分类号 B64C13/18
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