发明名称 CORRECTION METHOD OF FLIGHT TRAJECTORY OF CONTROLLED SHELL, AND SHELL FOR METHOD'S IMPLEMENTATION
摘要 FIELD: weapons and ammunition.SUBSTANCE: it is proposed to direct or rotate beam (12) of laser rays relative to centre (13) of the current specified heading of shell (1) so that shell (1) can determine by itself a data set and then perform automatic correction. For that purpose, the first laser ray (11) is supplied through certain area (15) relative to the specified heading of shell (1), which at the same time can cause the beginning of time reckoning. For example, at the same time, other rotating laser ray (12) with constant rotation frequency (Q) is located around area (15). By means of the second laser ray (12) the shell determines the data set relative to the specified heading and initiates correction based on the established data set. Size of the established data set is used to begin corrections. For that purpose, delays are implemented in shell (1).EFFECT: improving correction efficiency of flight trajectory.16 cl, 4 dwg
申请公布号 RU2509975(C1) 申请公布日期 2014.03.20
申请号 RU20120134788 申请日期 2010.12.07
申请人 REJNMETALL EHJR DIFENS AG 发明人 ZAJDENSTIKER JENS
分类号 F41G7/26 主分类号 F41G7/26
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