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Dynamic guidance for close-in maneuvering air combat

机译：近距离机动空战的动态制导

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摘要

A system, apparatus and method for optimizing the conduct of a close-in air combat are disclosed. A computing device is operative in the analysis of a close-in air combat situation. The computing device stores and utilizes one or more aerial aircraft-specific, weapon systems-specific and close-in air combat-situation-specific information. The computing device is operative in the analysis of the current air combat situation (12) and in the generation of a flight control recommendation (40). Consequently, the recommendation is converted into an indication having visual or audio format to be communicated to the operating crew of the aerial vehicle. The recommendation could further to be converted into specific flight control/energy commands and to be introduced directly to the control systems of the aircraft.

机译：公开了一种用于优化近距离空战的行为的系统，设备和方法。计算设备可用于分析近距离空战情况。该计算设备存储并利用一种或多种特定于飞机的，特定武器系统的和近距离空中作战的位置的信息。该计算设备可用于分析当前的空战情况（ 12 ）和生成飞行控制建议（ 40 ）。因此，推荐被转换为具有视觉或音频格式的指示，以传达给飞行器的操作人员。该建议可以进一步转换为特定的飞行控制/能量命令，并直接引入飞机的控制系统。 展开▼

著录项

公开/公告号US2006142903A1

专利类型

公开/公告日2006-06-29

原文格式PDF

申请/专利权人 NIR PADAN;
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申请/专利号US20050537475

发明设计人 NIR PADAN;
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申请日2003-06-11

分类号G01C23/00;

国家 US

入库时间 2022-08-21 21:46:07

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