500 宇宙航空研究開発機構特別資料 JAXA-SP TURANDOT ORDEM 3.0 Introduce an analysis feature using ORDEM 3.0 to the Tactical Utilities for Rapid ANalysis of Deb
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1 第 7 回 スペースデブリワークショップ 講演資料集 499 H2 デブリ衝突損傷リスク解析ツールへの ORDEM 3.0 導入 Introduce an analysis feature using ORDEM 3.0 to the Tactical Utilities for Rapid ANalysis of Debris on Orbit Terrestrial 中渡瀬竜二, 上田裕子, 八田真児 (MUSCAT スペース エンジニアリング ( 株 )), 東出真澄, 平井隆之, 河本聡美 (JAXA/RDD) Ryuji Nakawatase, Hiroko O. Ueda, Shinji Hatta (MUSCAT Space Engineering Co., Ltd.), Masumi Higashide, Takayuki Hirai, Satomi Kawamoto (JAXA/RDD) デブリ衝突損傷リスク解析ツール (Turandot) は, 宇宙機設計支援ソフトウェアである. 本ツールは宇宙機表面を詳細な格子に分割し, デブリに対する宇宙機自身の遮蔽を考慮した上で, 各部位のデブリ衝突頻度を解析する. さらに, 任意の宇宙機部位について, 宇宙機表面材料と弾道方程式を設定することで, 損傷リスクも評価可能である. 弾道方程式については, 標準的と考えられているモデルをデフォルトとして与えるほか, ユーザが任意のモデルを生成して解析に利用することが可能である. また, これまで軌道上デブリフラックスのデータベースとして MASTER-2009 と ORDEM 2.0(ORDEM2000) を利用してきたが,ORDEM 3.0 によるフラックスも利用できるように機能を拡張した.ORDEM 3.0 で与えられるフラックスは, 天球を Igloo と呼ばれる 614 に分割した領域で与えられるが, 天球を約 1 平方度毎に分割した 41,258 の領域に Igloo との立体角比に従ってフラックスを再分配して解析に利用している. この講演では, 本ツールの概要と機能拡張について紹介する. The Tactical Utilities for Rapid ANalysis of Debris on Orbit Terrestrial(Turandot) supports design of spacecraft. This software is capable of prediction of spacecraft damage probability by collisional debris including shielding effect of the spacecraft itself. Turandot was expanded in order to use ORDEM 3.0 as well as MASTER-2009 and ORDEM2000 as database of debris flux. This presentation introduces overview and feature expansion of the Turandot.
2 500 宇宙航空研究開発機構特別資料 JAXA-SP TURANDOT ORDEM 3.0 Introduce an analysis feature using ORDEM 3.0 to the Tactical Utilities for Rapid ANalysis of Debris on Orbit Terrestrial Ryuji Nakawatase, Hiroko O. Ueda, Shinji Hatta (MUSCAT Space Engineering Co., Ltd.) Masumi Higashide, Takayuki Hirai, Satomi Kawamoto (JAXA/Research and Development Directorate) 7 th Space Debris 2016/10/18~2016/10/ _Debris_WS_MUSE 1 Contents Introduction What is TURANDOT Validation New function(ordem 3.0) Demonstration _Debris_WS_MUSE 2
3 第 7 回 スペースデブリワークショップ 講演資料集 501 Introduction M/OD risk assessment tools BUMPER II NASA ESABASE2 / DEBRIS ESA COLLO, BUFFER TSNIIMASH MDPANTO DLR SHIELD QinetiQ MODAOST CAST TURANDOT JAXA IADC Protection Manual(Version 7.0), IADC Update of the ESA Space Debris Mitigation Handbook, ESA Contract 14471/00/D/HK _Debris_WS_MUSE 3 About Turandot Turandot supports design of spacecraft. This software is capable of prediction of spacecraft damage probability by collisional debris including shielding effect of the spacecraft itself. April, 2007~ Collision Probability Analysis Tool Collisional Damage Probability Analysis Tool Including MASTER-2009 Detail Modifications & Validations _Debris_WS_MUSE 4
4 502 宇宙航空研究開発機構特別資料 JAXA-SP Functions I GUI Integrated Analysis Environment Satellite modeling Grid generation Acknowledgement for Kurihara, M _Debris_WS_MUSE 5 GUI Functions I Computation condition setting Requirement from Databases (MASTER & ORDEM) _Debris_WS_MUSE 6
5 第 7 回 スペースデブリワークショップ 講演資料集 503 Functions II MASTER-2009(MASTER-2005) & ORDEM 2.0(ORDEM2000) fordem fmaster K if 1 K fordem fmaster if K 1 FORDEM K f d f 4 : flux MASTER _Debris_WS_MUSE 7 Damage Probability Users Definition Fortran 95 like Functions III _Debris_WS_MUSE 8
6 504 宇宙航空研究開発機構特別資料 JAXA-SP _Debris_WS_MUSE 9 Comparison with MASTER-2009 Flux computing function of MASTER Fluxes for 6 Faces of a cube _Debris_WS_MUSE 10
7 第 7 回 スペースデブリワークショップ 講演資料集 505 Result Condition TURANDOT MASTER Error a) 0.1mm<d b) 1cm<d Debris % Meteoroid % Debris % Meteoroid % Good agreement TURANDOT is reasonable _Debris_WS_MUSE 11 MASTER-2005 BLE Validation(1) Earth oriented attitude 2002/01/01~2002/12/ m<d<0.1m 85 debris flux data from expl.cpe as No.1001, 2001,, debris flux from every 1000 debris flux _Debris_WS_MUSE 12
8 506 宇宙航空研究開発機構特別資料 JAXA-SP BLE Validation(2) Cube, (1m) 3 Damaged@1cm<d z : outward radial Trailing y Trailing 1m 1m Top Right 1m Leading q : Elevation f : Azimuth x : projected orbital velocity direction _Debris_WS_MUSE 13 BLE Validation(3) Direction vector of debris flux v debri cos cos cos sin sin Normal vectors of the cube surfaces Name Nomal Vector Leading (1,0,0) Trailing (-1,0,0) Left (0,1,0) Right (0,-1,0) Top (0,0,1) Bottom (0,0,-1) _Debris_WS_MUSE 14
9 第 7 回 スペースデブリワークショップ 講演資料集 507 BLE Validation(4) Collision Probability for unit time P collision damage V Vn flux 0 V debri Vn 0 Vdebri Vn if contidion true debri For Damage Probabillity, including condition, P V Vn flux debri _Debris_WS_MUSE 15 Result BLE Validation(5) MASTER2009 +MS-Excel TURANDOT Leading 9.95E E-09 Trailing 1.21E E-12 Left 1.24E E-09 Right 5.62E E-09 Top 5.49E E-12 Bottom 3.04E E-11 Good agreement _Debris_WS_MUSE 16
10 508 宇宙航空研究開発機構特別資料 JAXA-SP Validation IADC Inter-Agency Space Debris Coordination Committee Benchmark _Debris_WS_MUSE 17 IADC Benchmark 1) Cube 2) Sphere 3) Station 3m 1m 1m 2m 1m Cross section 1m _Debris_WS_MUSE 18
11 第 7 回 スペースデブリワークショップ 講演資料集 509 ORDEM 3.0 NASA Orbital Debris Engineering Model ORDEM User s Guide, NASA/TP , p _Debris_WS_MUSE 19 Celestial Grid and Igloo Celestial Grid about 1 deg 2 (0.3 msr) 41,258 cells Igloo 10 deg (in azimuth) x 10 deg (in elevation) 614 cells Flux is redistributed from Igloo to Celestial Grid according to ratio of solid angle _Debris_WS_MUSE 20
12 510 宇宙航空研究開発機構特別資料 JAXA-SP Redistributed flux Igloo to Celestial Grid ORDEM 3.0 "2-D Directional Flux" (DIRFLUX_SC.OUT) ORDEM 3.0"SIZEFLUX_SC.OUT and Cumulative Flux based on Celestial Grid(Calaf) Flux distribution based on Celestial Grid Year:2014 Perigee Altitude / km = 400.0, Apogee Altitude / km = 400.0, Inclination / deg = 51.60, RAAN/AoP : random _Debris_WS_MUSE 21 GUI for ORDEM 3.0- JX-PSPC A_16_01_29_MUSE 22
13 第 7 回 スペースデブリワークショップ 講演資料集 511 Conclusion General information about Turandot. Turandot was expanded in order to use ORDEM _Debris_WS_MUSE 23
第 5 回 スペースデブリワークショップ 講演資料集 291 TURANDOT Expansion of Tactical Utility for Rapid ANalysis of Debris on Orbit Terrestrial J. Kim (MUSCAT Space Engineeri
290 宇宙航空研究開発機構特別資料 JAXA-SP-13-018 E4 デブリ衝突損傷リスク解析ツール (TURANDOT) の機能拡張 Expansion of Tactical Utilities for Rapid ANalysis of Debris on Orbit Terrestrial 金正浩, 八田真児 (MUSCAT スペース エンジニアリング株式会社 ), 東出真澄, 河本聡美
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