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 |
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代理人 |
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主权项 |
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地址 |
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