发明名称 GUIDING METHOD OF MISSILE
摘要 PURPOSE:To improve a sensing accuracy for a target position and an accuracy of an on-target impart by a method wherein a reflecting sound of a sound wave reflected from a target object from an active soner is caught by a sono- buoy and a position of a target object is calculated in response to a transmitting signal and then a missile is guided. CONSTITUTION:Active soner 23 on a marine 1 disperses sono-buoys 13, transmits a sound wave 25 to a target object 20. Its reflecting sound 26 is caught by each of sono-buoys 13. Each of the sono-buoys 13 performs a predetermined calculation and transmits a time information S3 receiving a reflecting sound 26 and a position information S4 of each of the sono-buoys 13 itself. The signal is taken into a missile injecting control device 4 on the marine 1 and a predetermined calculation is carried out, a position of the target object 20 is calculated and outputted to a guiding control part for the missile 2 and then the missile 2 is injected. As the missile 2 approaches the target 20, a torpedo 8 is released below a sea water and for example it starts an activity for the torpedo 8 toward the target object 20 through a homing guide or the like and then if the target object 20 is within an effective range, the missile breaks the target 20.
申请公布号 JPH0415497(A) 申请公布日期 1992.01.20
申请号 JP19900119260 申请日期 1990.05.09
申请人 TECH RES & DEV INST OF JAPAN DEF AGENCY;NISSAN MOTOR CO LTD 发明人 MATSUMOTO SHINSUKE;NAKANO TORU
分类号 F41G7/20;F42B12/36;F42B15/01;F42B17/00;G01S15/66;G06F19/00 主分类号 F41G7/20
代理机构 代理人
主权项
地址
您可能感兴趣的专利