Accession Number : ADA309746

Title :   Control Law of Terminal-Guidance Segment of Space Interceptors,

Corporate Author : NATIONAL AIR INTELLIGENCE CENTER WRIGHT-PATTERSON AFB OH

Personal Author(s) : Yingbo, Yang ; Huizhong, Zhou

PDF Url : ADA309746

Report Date : 27 MAR 1996

Pagination or Media Count : 18

Abstract : The article discusses the control law of space single axis spin stabilized interceptors, relying on multiple solid fuel thruster engines for orbital control. By analyzing the motion law of the terminal guidance segment with mathematical simulation, an effective divergence control method with proportional guidance is derived. Moreover, the authors go on to discuss the principle of selecting various control parameters, and measures for reducing the off target amount, which have reference value in studying and developing similar types of space interceptors in China.

Descriptors :   *ATTITUDE CONTROL SYSTEMS, *INTERCEPT TRAJECTORIES, *INTERCEPTOR SPACECRAFT, PARAMETERS, TRANSLATIONS, CONTROL THEORY, PROPORTIONAL NAVIGATION, TERMINAL GUIDANCE, CHINA, CHINESE LANGUAGE.

Subject Categories : Spacecraft Trajectories and Reentry

Distribution Statement : APPROVED FOR PUBLIC RELEASE