Accession Number : ADA300022
Title : Closed-Form Solution to Guidance Problems,
Corporate Author : NATIONAL AIR INTELLIGENCE CENTER WRIGHT-PATTERSON AFB OH
Personal Author(s) : Jiang, Yuxian
PDF Url : ADA300022
Report Date : 22 AUG 1995
Pagination or Media Count : 11
Abstract : The effect of inertia of the guidance systems on the closed-form solution to guidance problems is investigated and an analytical solution is obtained. It indicates that the solution without considering the inertia is only a special form for long Line-of-Sight, However, this solution is also available to short Line-of-Sight. The unstability of angular rate of the Line-of-Sight and the reason for miss-distances are also expressed by this solution. The results can be used to analyse the effect of the proportional-navigation coefficient and the inertia of guidance system on miss-distances.
Descriptors : *GUIDANCE, LINE OF SIGHT, INERTIA, RATES, SHORT RANGE(TIME), SOLUTIONS(GENERAL), TRANSLATIONS, PROPORTIONAL NAVIGATION, CHINA, ANGULAR MOTION, ANALYTIC FUNCTIONS, MISS DISTANCE, CHINESE LANGUAGE.
Subject Categories : Navigation and Guidance
Distribution Statement : APPROVED FOR PUBLIC RELEASE