首页> 外国专利> METHOD OF AUTONOMOUS GUIDANCE OF A ROTATION-STABILIZED ARTILLERY PROJECTILE AND ARTILLERY PROJECT OF AUTONOMOUSLY GUIDED FOR THE IMPLEMENTATION OF THE PROCESS

METHOD OF AUTONOMOUS GUIDANCE OF A ROTATION-STABILIZED ARTILLERY PROJECTILE AND ARTILLERY PROJECT OF AUTONOMOUSLY GUIDED FOR THE IMPLEMENTATION OF THE PROCESS

机译:旋转稳定炮弹的自主制导方法以及实施该程序的自主制导炮弹项目

摘要

The invention relates to a method for autonomous guidance of an artillery projectile (2) stabilized by rotation, on a target (12). To obtain that an artillery projectile (2; 25) very precisely hits a target (12), even at distances greater than or equal to 35 km, the invention proposes that, before firing the projectile (2) , the target data, determined beforehand, are transmitted to the latter and that, after firing the projectile (2), these data are compared with the position data of the projectile, measured using a navigation system by satellite. The correction data resulting from this comparison is then used to direct the projectile (2). To this end, shortly before the guidance phase, we pass from a flight state stabilized by rotation to a flight state stabilized by ailerons, then an aerodynamic guidance of the projectile (2) is carried out by means of deployable fins (9). outside the projectile, arranged at the front thereof, the rotation brakes (7) acting as lift surfaces, once placed in a locked state.
机译:本发明涉及一种通过旋转稳定地在目标(12)上自主引导炮弹(2)的方法。为了获得大炮弹(2; 25)甚至在大于或等于35 km的距离时也非常精确地击中目标(12),本发明建议在发射弹丸(2)之前预先确定目标数据被发射到后者,并且在发射了射弹(2)之后,将这些数据与射弹的位置数据进行比较,该射弹的位置数据是使用卫星导航系统测量的。然后,由该比较得出的校正数据将用于引导弹丸(2)。为此,在制导阶段之前不久,我们从通过旋转稳定的飞行状态过渡到通过副翼稳定的飞行状态,然后借助可展开的鳍片(9)对弹丸(2)进行空气动力学引导。在弹丸的外部,布置在弹丸的前部,一旦处于锁定状态,则旋转制动器(7)充当举升表面。

著录项

  • 公开/公告号FR2768500A1

    专利类型

  • 公开/公告日1999-03-19

    原文格式PDF

  • 申请/专利权人 RHEINMETALL W & M GMBH;

    申请/专利号FR19980011537

  • 发明设计人 WOLFGANG SEIDEL;FRANK GUISCHARD;

    申请日1998-09-16

  • 分类号F41G7/34;F42B15/01;F42B10/54;F42B10/56;

  • 国家 FR

  • 入库时间 2022-08-22 02:10:24

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