Accession Number : ADA306494
Title : Research On Dynamic Model of Space Interceptor In End-Guidance Phase,
Corporate Author : NATIONAL AIR INTELLIGENCE CENTER WRIGHT-PATTERSON AFB OH
Personal Author(s) : Huimin, Zheng
PDF Url : ADA306494
Report Date : 08 MAR 1996
Pagination or Media Count : 20
Abstract : This paper is intended to explain the realization of direct collision kill mode by space interceptor against a target. In accordance with the requirements of the interceptor guidance and control system program, an orbital control engine is proposed to make a modulation over interceptor centroid movement in the end guidance phase. Also, an attitude control engine is used to make an attitude adjustment. Furthermore, a six degree of freedom interceptor trajectory simulation model is constructed. The computational results of the model indicate that it is necessary and possible to achieve control over the interceptor by using attitude control and orbital control engines in the end guidance phase.
Descriptors : *INTERCEPT TRAJECTORIES, *TERMINAL GUIDANCE, ATTITUDE CONTROL SYSTEMS, COMPUTATIONS, KILL PROBABILITIES, TRANSLATIONS, INTERCEPTORS, CHINA, CHINESE LANGUAGE.
Subject Categories : Space Navigation and Guidance
Distribution Statement : APPROVED FOR PUBLIC RELEASE