发明名称 |
Method and arrangement for guiding a missile to intercept a moving target |
摘要 |
The present invention relates to a method for guiding a missile (1) to intercept a moving target. The method comprises providing information regarding a position, velocity vector and future velocity characteristic of the missile and information on a target position and a target velocity vector of the target to a processor in the missile. The processor then predicts an intercept point of the missile and the target, said prediction includes calculating a future trajectory of the target based on an assumption of the future manoeuvres of the target and predicting the intercept point from the calculated future trajectory and the information provided and the information received. The missile is homed in to the predicted intercept point. <IMAGE>
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申请公布号 |
EP1439369(A2) |
申请公布日期 |
2004.07.21 |
申请号 |
EP20040007906 |
申请日期 |
1999.01.20 |
申请人 |
SAAB AB |
发明人 |
HAGELIN, HANS-OVE;SKARMAN, ERIK |
分类号 |
F41G7/20;F41G7/22;F42B15/01;G05D1/00;G05D1/10;G05D1/12;(IPC1-7):F41G7/20 |
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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