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Method for simulating a mission of an unmanned armed aerial vehicle

机译:模拟无人机飞行任务的方法

摘要

The method involves exchanging an irreversibly operated valve (54) against a switchable valve or exchanging a cooling medium-storage tank (52) having the irreversibly operated valve against a cooling medium-storage tank having the switchable valve. A switching signal cable (33) for a signal is separated, and an output of a computer is connected with the switchable valve. An aircraft (2) and a missile (1) are controlled along a flight path provided by a mission plan, where a switching signal for activating a battery (6) is guided into a simulation configuration for the switchable valve. An independent claim is also included for a missile for simulating a mission.
机译:该方法包括将不可逆操作的阀(54)与可切换阀进行交换,或将具有不可逆操作的阀的冷却介质储存箱(52)与具有可切换阀的冷却介质存储箱进行交换。分离用于信号的切换信号电缆(33),并且计算机的输出与可切换阀连接。沿着任务计划所提供的飞行路径来控制飞机(2)和导弹(1),其中用于激活电池(6)的切换信号被引导到用于可切换阀的模拟配置中。还包括用于模拟任务的导弹的独立索赔。

著录项

  • 公开/公告号EP2381205B1

    专利类型

  • 公开/公告日2013-06-19

    原文格式PDF

  • 申请/专利权人 MBDA DEUTSCHLAND GMBH;

    申请/专利号EP20110002912

  • 发明设计人 WOHLGEMUTH WERNER;GRABMEIER MICHAEL;

    申请日2011-04-07

  • 分类号F41G7/00;F42B8/12;F42B15/10;G09B9/00;

  • 国家 EP

  • 入库时间 2022-08-21 16:33:15

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