JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
46783000.pdf1.11 MB
titleA note on the third stage control of the M-V launch vehicle
Other TitleM-V打上げ機の第3ステージ制御についての説明
Author(jpn)Matko, Drago; 雛田 元紀
Author(eng)Matko, Drago; Hinada, Motoki
Author Affiliation(jpn)宇宙航空研究開発機構 宇宙科学研究本部; 宇宙航空研究開発機構 宇宙科学研究本部
Author Affiliation(eng)Japan Aerospace Exploration Agency Institute of Space and Astronautical Science; Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
Issue Date2004-03
PublisherJapan Aerospace Exploration Agency (JAXA)
Publication date2004-03
AbstractThis paper presents an effective method for redesign of the M-V third stage attitude control algorithm. The fundamental aspect of the redesign is featured by introduction of an integral term into the controller in order to reduce steady state error caused by offset of the center of gravity of the vehicle and thrust axis misalignment. The proposed method is based on the idea to utilize the existing controller as the inner loop (attitude angular velocity) controller of the cascade control. Adding the velocity-position integrator into the controller leads to the desired integral characteristics. The dynamic character of the entire closed system and its robustness in the gain and phase margins are investigated for five representative controllers, which are switched at the specified time marks, and corresponding nominal and deviated dynamic models.
DescriptionJAXA Research and Development Report
Keywordsattitude control; algorithm; launch vehicle; angular velocity; steady state; center of gravity; cascade control; model; 姿勢制御; アルゴリズム; 打上げ機; 角速度; 定常状態; 重心; カスケード制御; モデル
Document TypeTechnical Report
JAXA Category研究開発報告
Report NoJAXA-RR-03-004E

Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.