发明名称 |
Firing control system for a direct firing weapon mounted on a rotary-wing aircraft |
摘要 |
Firing control system for a direct firing weapon mounted on a rotary-wing aircraft, which is designed to be actuated by the pilot himself and comprises an electronic computer, the said weapon being mounted for rotating about two transverse axes Y-Y' and Z-Z', due to driving means controlled by the said computer. According to the invention, said firing control system is characterized in that it comprises a sighting system on which a target and an adjusting mark can appear simultaneously, which adjusting mark can be moved on the said sighting system by a control of the pilot, as well as means to determine the coordinates of the position of the said adjusting mark with respect to a system of axes tied to the aircraft and to transmit them to said electronic computer at least when the said adjusting mark is brought to a position on the said sight finder where it is superposed on the said target.
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申请公布号 |
US4528891(A) |
申请公布日期 |
1985.07.16 |
申请号 |
US19820425392 |
申请日期 |
1982.09.28 |
申请人 |
SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE |
发明人 |
BRUNELLO, ALAIN M.;CATANI, GUY G. |
分类号 |
F41G3/22;F41G5/18;(IPC1-7):F41G5/18 |
主分类号 |
F41G3/22 |
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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