Accession Number : ADA306504
Title : Design of Near-Optimal Guidance Law For Space Interception,
Corporate Author : NATIONAL AIR INTELLIGENCE CENTER WRIGHT-PATTERSON AFB OH
Personal Author(s) : Xiaoping, Shi
PDF Url : ADA306504
Report Date : 21 MAR 1996
Pagination or Media Count : 17
Abstract : The article applies an augmented linearization method for nonlinear systems to propose a near optimal control resolution method of secondary type index problems for nonlinear systems. This method is applied to design a near optimal terminal guidance law for space interception. As indicated in the simulation results, the near optimal guidance has good performance.
Descriptors : *INTERCEPT TRAJECTORIES, *SPACE NAVIGATION, OPTIMIZATION, AUGMENTATION, NONLINEAR SYSTEMS, TRANSLATIONS, GUIDANCE, TERMINAL GUIDANCE, CHINA, CHINESE LANGUAGE.
Subject Categories : Space Navigation and Guidance
Distribution Statement : APPROVED FOR PUBLIC RELEASE