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本文为作者在１９９３年１１月２４日在莫斯科国际弹道导弹防御系统研讨会上所作报告的录音记录的译文，它主要论述在大气层内拦截弹道式导弹头的中程及近程高速反导弹的制导方式及导引方法，主要论述了在稠密大气层内高速导弹采用的指令惯性制导方式及前置命中点的导引方法，给出了实现这种制导方式控制系统的结构。报告作者为俄罗斯专门研制高速反导弹的＂创新者＂（）设计局的人员。原文图缺，文中附图是译者根据录音报告的内容及其所注的原理加以补上，仅供参考。
This is a translation of the transcripts of the transcripts of the report made by the author at the Symposium on the Ballistic Missile Defense in Moscow on November 24, 1993. It mainly deals with the guidance of mid-range and short-range high-speed anti-missile missiles that intercept ballistic missiles in the atmosphere Methods and guidance methods, mainly discusses the instruction inertial guidance method and the guidance method of the front hit point adopted by the high-speed missile in the dense atmosphere, and presents the structure of the control system realizing this guidance method. The report was written by Russia’s “innovator” design agency specializing in high-speed anti-missile. The original picture is missing, the text in the drawings is the translator according to the contents of the recording report and the principle of its injection to be supplemented, for reference purposes only.