An Evolutionary Reconfiguration for Attitude Controller after Thruster Trouble.

Accession number;00A0150789
Title;An Evolutionary Reconfiguration for Attitude Controller after Thruster Trouble.
Author;KUROTAKI MITSURU(Hokkaido Univ., Fac. of Eng.)   YOKOI HIROSHI(Hokkaido Univ., Fac. of Eng.)   KAKAZU YUKINORI(Hokkaido Univ., Fac. of Eng.)   KONO MITSURU(Fuji Heavy Ind. Ltd.)   ISHIDA SHINTARO(Fuji Heavy Ind. Ltd.)   YONEDA HIROSHI(Fuji Heavy Ind. Ltd.)   
Journal Title;Proceedings of the Space Sciences and Technology Conference
Journal Code:S0277A
ISSN:
VOL.43rd;NO.;PAGE.201-206(1999)
Figure&Table&Reference;FIG.7, REF.5
Pub. Country;Japan
Language;Japanese
Abstract;This paper describes a reconfiguration method using Genetic Algorithms for an attitude controller to a spacecraft. The proposed method is able to reconfigure the controller which stabilizes the spacecraft when the unforeknown failures are identified. The numerical simulation shows the proposed method reconfigured the feedback gain which uses inertia-coupling, and stabilized the spacecraft when the thrusters troubled. (author abst.)