发明名称 MISSILE GUIDANCE SYSTEM AND ACQUISITION METHOD OF TARGET ANGLE INFORMATION
摘要 PROBLEM TO BE SOLVED: To provide a missile guidance system capable acquiring target angle information sufficiently from a distance, even for a target having a reduced RCS.SOLUTION: A missile guidance system includes: calculating position information of a missile 3 itself; calculating an angle formed on the basis of position information of a target, position information of a radar 1, and position information of the missile 3; guiding the missile itself from a direction of the formed angle to the target 2 on the basis of the formed angle; receiving a reflected wave of a radio wave transmitted to the target 2; and acquiring target angle information using the reflected wave from the target 2.
申请公布号 JP2013181737(A) 申请公布日期 2013.09.12
申请号 JP20120048129 申请日期 2012.03.05
申请人 TOSHIBA CORP 发明人 KINOSHITA TOMOYA
分类号 F41G7/22;G01S13/87;G01S13/88 主分类号 F41G7/22
代理机构 代理人
主权项
地址