发明名称 |
SYSTEM AND METHOD FOR GUIDING A CANNON SHELL IN FLIGHT |
摘要 |
An apparatus (14) and method for guiding a cannon shell (10) accurately are disclosed. The apparatus (14) includes two main parts (21,22) adapted to be installed on the leading end of the cannon shell (10). The front main part (21) of the apparatus (14) is equipped with at least one pair of fins (26,28) and is rotatable with respect to the rear main part (22). The pair of fins (26,28) is controlled to hold the front main part (21) substantially stable with respect to an external reference frame when the cannon shell (10) rotates as it flies towards its target. Control system is comprised within the apparatus that receives location signals and is adapted to provide guiding control commands to the cannon shell (10) via the fins (26,28) so as to guide the shell (10) accurately to its preprogrammed target. The control system is adapted to activate the detonation chain of the shell according to preprogrammed mode. |
申请公布号 |
EP2423637(A2) |
申请公布日期 |
2012.02.29 |
申请号 |
EP20110178692 |
申请日期 |
2011.08.24 |
申请人 |
BAE SYSTEMS ROKAR INTERNATIONAL LTD. |
发明人 |
MALUL, ASSAF;MOSHKOVITZ, ZIV |
分类号 |
F42B10/64;F42B10/14 |
主分类号 |
F42B10/64 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|