发明名称 |
RADIO GUIDANCE METHOD, RADIO GUIDANCE DEVICE, GUIDANCE PROGRAM, AND MISSILE |
摘要 |
PROBLEM TO BE SOLVED: To provide a radio guidance method and a radio guidance device which can arbitrarily set guidance accuracy and a flight route of a missile.SOLUTION: A radio guidance device which identifies a target 200 by a radar wave emitted by a missile 100 so as to guide the missile 100 to the target 200 includes an index setting section and an analysis section. The index setting section changeably sets a design index of a reflection cross section of an irradiation object by the radar wave. The analysis section determines the maximum value of a grazing angle of the radar wave with respect to the target 200 on the basis of the design index.SELECTED DRAWING: Figure 1A |
申请公布号 |
JP2016180699(A) |
申请公布日期 |
2016.10.13 |
申请号 |
JP20150061291 |
申请日期 |
2015.03.24 |
申请人 |
MITSUBISHI HEAVY IND LTD |
发明人 |
HIROKANE MARIKO;UENO YOSHIHIKO |
分类号 |
G01S13/88;F41G7/22;F42B15/01 |
主分类号 |
G01S13/88 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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