Accession Number : ADA306336

Title :   High Speed Antimissile Command Inertial Precision Guidance Systems,

Corporate Author : NATIONAL AIR INTELLIGENCE CENTER WRIGHT-PATTERSON AFB OH

Personal Author(s) : Zhihong, Zhang

PDF Url : ADA306336

Report Date : 12 FEB 1996

Pagination or Media Count : 10

Abstract : This article is a written translation of a voice recording of a lecture made by the author at the Moscow International Ballistic Missile Defense Symposium on 24 November 1993. It primarily discusses guidance and control methods associated with close and medium range high speed antimissile missiles to intercept in the atmosphere ballistic type missile warheads. Exposition is primarily of command inertial guidance methods opted for to use in high speed missiles within dense atmosphere as well as control methods associated with predetermined impact points. It gives the structures currently associated with this type of guidance method control system. The author of the lecture is a member of the Russian 'Trail Blazer' (Honarop Design Bureau, specializing in the development of high sped antimissile missiles. As far as the lack of illustrations in the original article is concerned, the appended Fig.'s in the article were added as supplements by the translator on the basis of the contents of the recorded lecture and the principles it concentrated on. They are only provided for reference.

Descriptors :   *ANTIMISSILE DEFENSE SYSTEMS, *INERTIAL GUIDANCE, GUIDED MISSILES, USSR, CONTROL, CONTROL SYSTEMS, RUSSIAN LANGUAGE, GRAPHICS, RECORDING SYSTEMS, TRANSLATIONS, GUIDANCE, ATMOSPHERES, VOICE COMMUNICATIONS, IMPACT POINT, COMMAND GUIDANCE, LECTURES, DENSE GASES.

Subject Categories : Antimissile Defense Systems
      Navigation and Guidance

Distribution Statement : APPROVED FOR PUBLIC RELEASE