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AIR-TO-AIR MISSILE LAUNCHING METHOD AND SMALL-SIZED UNMANNED PLATFORM MACHINE

机译:空空导弹发射方法和小型无人平台机

摘要

PROBLEM TO BE SOLVED: To improve a probability of remaining live of a mating team and also improve a probability of live by a method wherein an enemy airplane can be attacked in unmanned state during an air-born battle using a missile. ;SOLUTION: A small-sized unmanned platform air-plane 4 having a missile 3 installed therein is separated from a mother plane 1, thereafter it is automatically turned along a flying course programmed in advance. Then, during turning operation, an enemy plane is automatically caught by a target retrieving device 12 and then either active or passive hosing guidance type missile is automatically launched. The mother plane 1 performs an avoiding action after separating the small-sized unmanned platform plane 4. The small-sized unmanned platform plane 4 automatically returns to the ground under an automatic navigation control either after launching of the missile 3 or after a turning of a specified period of time.;COPYRIGHT: (C)1997,JPO
机译:要解决的问题:通过使用一种方法,可以在空降战斗中使用导弹对敌机进行无人攻击,从而提高配对队的剩余生存率,并提高生存率。解决方案:将装有导弹3的小型无人平台飞机4与母机1分开,然后沿预先设定的飞行路线自动转向。然后,在转弯操作期间,敌机被目标检索装置12自动捕获,然后主动或被动升空制导型导弹被自动发射。在分离小型无人平台4之后,母机1执行回避动作。小型无人平台4在导弹3发射之后或在飞行器转动之后在自动导航控制下自动返回地面。指定的期限。;版权:(C)1997,日本特许厅

著录项

  • 公开/公告号JPH09138098A

    专利类型

  • 公开/公告日1997-05-27

    原文格式PDF

  • 申请/专利权人 NEC CORP;

    申请/专利号JP19950321026

  • 发明设计人 OTSU SUGURU;

    申请日1995-11-15

  • 分类号F42B15/01;B64C13/18;B64C39/02;B64D5/00;B64D7/08;F42B15/10;

  • 国家 JP

  • 入库时间 2022-08-22 03:34:41

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