Open AccessThe method of exact solution of the problem of short-range guidance with two turns
Author(s) -
А. Е. Феликсон
Publication year - 2018
Publication title -
vestnik koncerna vko «almaz - antej»
Language(s) - English
Resource type - Journals
ISSN - 2542-0542
DOI - 10.38013/2542-0542-2018-4-91-99
Subject(s) - range (aeronautics) , trajectory , task (project management) , exact solutions in general relativity , process (computing) , software , computer science , iterative method , control theory (sociology) , mathematical optimization , mathematics , algorithm , mathematical analysis , engineering , aerospace engineering , artificial intelligence , physics , control (management) , systems engineering , astronomy , programming language , operating system
The task of determining the guidance parameters by the “two-turn maneuver” method is related to numerical solution of an equation defining the trajectory of the fighter-interceptor. We propose an easy-to-implement in software approach which is based on the exact solution of the problem at each step of the iterative process constructed by one of the parameters