发明名称 PRECISION GUIDANCE APPARATUS FOR MISSILE
摘要 <p>PURPOSE:To achieve a higher target hitting accuracy by arranging a portable small transponder and a missile having a radar triangulation type guided missile to make it fly to a target being guided with a simple device. CONSTITUTION:A plurality of portable type small transponders 3a and 3b are loaded on a carrier and carried to be set at a position determined somewhere before a target area (a). Missile 1 have a radar triangulation type guided device 2 and a setting positions of the transponders 3a and 3b are inputted into the device 2. Thereafter, when the missile 1 is fired to a target, with the transponders 3a and 3b preset as reference, the device 2 irradiates the transponders and receives a response wave thereof to calculate own position in a manner of triangulation survey so that the missile flies to the target correcting own flight course. Thus, the missile 1 flies over the earth being guided and hits the target.</p>
申请公布号 JPH04127081(A) 申请公布日期 1992.04.28
申请号 JP19900247247 申请日期 1990.09.19
申请人 MITSUBISHI HEAVY IND LTD 发明人 SAKAMOTO SHINICHIRO
分类号 F41G7/34;F42B15/01;G01C21/00;G01S13/46;G01S13/74;G01S13/88 主分类号 F41G7/34
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