液体燃料ロケットを用いた衛星打上げ用飛しょう体の初段に関する制御系構成

Material type: 文書・図像類

Author: 森, 英彦ほか

Publisher: 航空宇宙技術研究所

Publication date: 1972-01

Material Format: Digital

Capacity, size, etc.: -

NDC: -

View All

Notes on use

Note (General)：: A system study has been performed to construct a model launch vehicle for a geostationary satellite by Space Technology Research Group of NAL.As a par...

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: 液体燃料ロケットを用いた衛星打上げ用飛しょう体の初段に関する制御系構成
Author/Editor: 森, 英彦
輿石, 肇
MORI, Hidehiko
KOSHIISHI, Hajime
Author Heading: 森, 英彦
輿石, 肇
MORI, Hidehiko
KOSHIISHI, Hajime
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1972-01
Publication Date (W3CDTF): 1972-01
Alternative Title: Flight Control System Design for Launch Vehicles with Liquid Propellant
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-264
No. or year of volume/issue: 264
Volume: 264
Pages: 40-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: jpn
Target Audience: 一般
Note (General): A system study has been performed to construct a model launch vehicle for a geostationary satellite by Space Technology Research Group of NAL.As a part of the study, this research was executed to provide the synthetic procedure and techniques of designing the flight control system for the boost stage of this class of vehicles, and also to present the characteristics of the prototype of the model vehicle, SS-3. This report covers(1) the derivation of relating equations, (2) the system characterization with the aids of trajectory simulations, (3) the computing methods for flexible vehicle stabilization, and (4) the discussion about calculating methods of loads on the vehicle by the effects of the wind. The computer programs for drawing Nyquist plot, Bode plot and root locus of a high order system with multiple feedback loops were worked out and used for the third problem. They will have general applications in the stability analysis of multivariable control systems.
資料番号: NALTR0264000
レポート番号: NAL TR-264
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44507&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44507&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