A note on the third stage control of the M-V launch vehicle

Material type: 文書・図像類

Author: Matko, Dragoほか

Publisher: 宇宙航空研究開発機構

Publication date: 2004-03

Material Format: Digital

Capacity, size, etc.: -

NDC: -

View All

Notes on use

Note (General)：: This paper presents an effective method for redesign of the M-V third stage attitude control algorithm. The fundamental aspect of the redesign is feat...

Search by Bookstore

Holdings of Libraries in Japan

This page shows libraries in Japan other than the National Diet Library that hold the material.

List of Cooperating Institutions and Databases

Please contact your local library for information on how to use materials or whether it is possible to request materials from the holding libraries.

other

JAXA Repository
Digital
You can check the holdings of institutions and databases with which 学術機関リポジトリデータベース（IRDB）（機関リポジトリ） is linked at the site of 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）.
JAXA Repository

Search by Bookstore

Bibliographic Record

You can check the details of this material, its authority (keywords that refer to materials on the same subject, author's name, etc.), etc.

Digital

Material Type: 文書・図像類
Title: A note on the third stage control of the M-V launch vehicle
Author/Editor: Matko, Drago
雛田, 元紀
Hinada, Motoki
Author Heading: Matko, Drago
雛田, 元紀
Hinada, Motoki
Publication, Distribution, etc.: 宇宙航空研究開発機構
Publication Date: 2004-03
Publication Date (W3CDTF): 2004-03
Alternative Title: M-V打上げ機の第3ステージ制御についての説明
Periodical title: 宇宙航空研究開発機構研究開発報告 = JAXA Research and Development Report
No. or year of volume/issue: JAXA-RR-03-004E
Volume: JAXA-RR-03-004E
ISSN (Periodical Title): ISSN : 1349-1113
Text Language Code: eng
Subject Heading: 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
attitude control
algorithm
launch vehicle
angular velocity
steady state
center of gravity
cascade control
model
Target Audience: 一般
Note (General): This 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.
資料番号: AA0046783000
レポート番号: JAXA-RR-03-004E
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=2416&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=2416&item_no=1&attribute_id=31&file_no=1
Access Restrictions: 限定公開
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ