D-SEND#2の誘導制御系の評価について

Material type: 規格・テクニカルリポート類

Author: 二宮, 哲次郎ほか

Publisher: 宇宙航空研究開発機構(JAXA)

Publication date: 2018-11-12

Material Format: Digital

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Note (General)：: 出版タイプ： NAD-SENDプロジェクトは, ソニックブームの低減を目的とした空力設計技術を飛行実証するための飛行実験である. D-SEND#2では, 有翼機体を高層気球を用いて高度約30kmから分離し, 地上に設置したソニックブーム計測システム（BMS）にてソニックブームを計測することを目的とし...

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Material Type: 規格・テクニカルリポート類
Title: D-SEND#2の誘導制御系の評価について
Author/Editor: 二宮, 哲次郎
鈴木, 広一
川口, 純一郎
Ninomiya, Tetsujiro
Suzuki, Hirokazu
Kawaguchi, Junichiro
Author Heading: Ninomiya, Tetsujiro
Suzuki, Hirokazu
Kawaguchi, Junichiro
Publication, Distribution, etc.: 宇宙航空研究開発機構(JAXA)
Publication Date: 2018-11-12
Publication Date (W3CDTF): 2018
Alternative Title: Performance evaluation of GNC system of D-SEND#2
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-18-004
Volume: JAXA-RR-18-004
Pages: 1-140
ISSN (Periodical Title): ISSN : 2433-2216
Subject Heading: Flight test
Guidance and Control
Dynamic Inversion
Target Audience: 一般
Note (General): 出版タイプ： NA
D-SENDプロジェクトは, ソニックブームの低減を目的とした空力設計技術を飛行実証するための飛行実験である. D-SEND#2では, 有翼機体を高層気球を用いて高度約30kmから分離し, 地上に設置したソニックブーム計測システム（BMS）にてソニックブームを計測することを目的としている. 本稿では, D-SEND#2の誘導制御系を対象に, 飛行実験に向けて実施した様々な観点からの評価について報告する.
This report is concerned with evaluation of GNC systems for D-SEND#2. D-SEND is a project to demonstrate a low sonic boom aerodynamic design concept, and the objective of D-SEND #2 flight test is to measure a sonic boom which is generated by a test vehicle at prescribed flight conditions. In this flight test, an unpowered test vehicle is lifted to an altitude of 30km by a balloon from which it then separates. After the separation, the vehicle's on-board flight control computer selects a target Boom Measurement System (BMS) according to the separation point. The vehicle then autonomously flies to the selected BMS and establishes prescribed sonic boom measurement flight conditions. Since it is required to achieve mission objectives at the very first flight in such a flight testing using a balloon, evaluation of mission success chance is mandatory adding to that of controller stability. It is also important to establish operational criteria for various anomaly cases. Some customized evaluation are also carried out to asses various risks in the flight test. This report describes a comprehensive evaluation method for GNC systems of D-SEND #2.
形態: カラー図版あり
Physical characteristics: Original contains color illustrations
資料番号: AA1830008000
レポート番号: JAXA-RR-18-004
DOI: 10.20637/JAXA-RR-18-004/0001
https://doi.org/10.20637/JAXA-RR-18-004/0001
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