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