发明名称 DEVICE AND METHOD FOR CONTROLLING FLIGHT OF PASSIVE TYPE MISSILE
摘要 <p><P>PROBLEM TO BE SOLVED: To improve positioning accuracy in a passive type missile observing TDOA and FDOA and passively positioning a target position. <P>SOLUTION: This passive type missile flight control device observes the TDOA and FDOA by receiving both scattered waves irradiated from a known transmission source, made to hit a target and scattered and direct waves directly coming from the known transmission source, and includes a flight control part (14) positioning the target without irradiating electric waves and controlling its own flight route toward the target. The passive type missile flight control device further includes a GDOP calculating part (18) calculating GDOP based on the geometric arrangement of the missile, the transmission source and the target, estimating the orthogonal degree of ISO-TDOA and ISO-FDOA and generating a quantitative determination index of current measurement errors by the missile. <P>COPYRIGHT: (C)2011,JPO&INPIT</p>
申请公布号 JP2011133165(A) 申请公布日期 2011.07.07
申请号 JP20090292500 申请日期 2009.12.24
申请人 MITSUBISHI ELECTRIC CORP 发明人 MORITA SHINICHI;MANIWA HISAKAZU;TAKAHASHI RYUHEI;OKAMURA ATSUSHI
分类号 F41G7/22;F42B10/60;F42B15/01;G01S13/46;G01S13/88;G01S13/94 主分类号 F41G7/22
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