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対外発表/2009


_ 対外発表 2009年(平成21年)

_ 論文

低速および高速衝突実験に基づく新しい衛星破砕モデルの構築
New Satellite Fragmentation Model Based upon Low-Velocity and Hypervelocity Impacts
Performance of Spin-Axis Attitude Estimation Algorithms With Real Data
Attitude Control by Magnetic Torquer
Benefits and Risks of Using Electrodynamic Tethers to De-Orbit Spacecraft
  • Carmen Pardini, Toshiya Hanada, Paula H. Krisko
  • Acta Astronautica, Vol. 64, Nos. 5-6, 2009, pp. 571-588.
QSAT: the Satellite for Polar Plasma Observation
  • Yoshihiro Tsuruda, Akiko Fujimoto, Naomi Kurahara, Toshiya Hanada, Kiyohumi Yumoto, Mengu Cho
  • International Journal of Earth, Moon and Planets, Vol. 104, Nos. 1-4, 2009, pp. 349-360.
QSAT: A Low-Cost Design for 50 kg Class Piggyback Satellite
  • Yoshihiro Tsuruda, Toshiya Hanada, Jozef C. van der Ha
  • Transactions of Japan Society for Aeronautical and Space Sciences, Space Technology Japan, Vol. 7, No. ists26 (ISTS Special Issue: Selected papers from the 26th International Symposium on Space Technology and Science), 2009, pp. Tf_7-Tf_12.
Outcome of Recent Satellite Impact Experiments
  • Toshiya Hanada, Jer-Chyi Liou, Takashi Nakajima, Eugene Stansbery
  • Advances in Space Research, Vol. 44, No. 5, 2009, pp. 558-567.
For Better Calculation of the Average Cross-Sectional Area of Breakup Fragments
  • Toshiya Hanada, Jer-Chyi Liou, Paula Krisko, and Takashi Nakajima
  • Transactions of Japan Society for Aeronautical and Space Sciences, Space Technology Japan, Vol. 7, No.ists26 (ISTS Special Issue: Selected papers from the 26th International Symposium on Space Technology and Science), 2009, pp. Pr_2_25-Pr_2_30.
Spin-Axis Attitude Determination from Earth Chord-Angle Variations for Geostationary Satellites
  • Jozef C. van der Ha and Frank L. Janssens
  • Journal of Guidance, Control, and Dynamics, Vol. 32, No. 5, Sepember-October 2009, pp. 1598-1608.
Orbital Debris Modeling at Kyushu University
A Test Flight Experiment of Electrodynamic Tether Using a Small Satellite: As the First Step for Debris Removal
  • Satomi Kawamoto, Yuki Kobayashi, Yasushi Ohkawa, Shoji Kitamura, Shin-Ichiro Nishida, Chiharu Kikkawa, Atsushi Yanagida, Susumu Toda, Yoshiki Yamagiwa, Mengu Cho, Toshiya Hanada
  • Journal of Space Technology and Science, Vol. 24, No. 2, 2009, pp. 36-44.

_ 解説記事

Two New Microsatellite Impact Tests in 2008
A Tutorial on Vectors and Attitude
  • Jozef C. van der Ha, Malcolm D. Shuster
  • IEEE Control Systems Magazine, Volume 29, Issue 2, pp. 94-107, April 2009.
人工衛星衝突で「宇宙のごみ」が大量発生
えあろすぺーすABC「スペースデブリ」
  • 花田俊也
  • 日本航空宇宙学会誌, 第57巻, 第665号, 187頁, 2009年6月.
Progress in Satellite Attitude Determination and Control
人工衛星の姿勢決定と制御における進歩

_ 特許

スペースデブリ除去方法
  • 花田俊也, 北澤幸人, 川辺有恒
  • 出願番号2009-276530, 2009年10月26日.

_ 講演

Performance of Spin Axis Attitude Estimation Algorithms with Real Data
  • J. C. van der Ha
  • 19th AAS Space Flight Mechanics Symposium, Savannah, GA, February 8-12, 2009.
Attitude Control using Magnetorquers
Can Thermal Radiation Serve as Explanation for the Flyby Anomaly?
  • Jozef C. van der Ha
  • Investigation of the Flyby Anomaly Workshop, International Space Science Institute, Bern, Switzerland, March 2-6, 2009.
小型衛星衝突破砕実験で生じた積層断熱材由来の破片について
小型衛星衝突破砕実験で生じた破片の形状分布について
Shape Distribution of Fragments From Microsatellite Impact Tests
  • T. Hanada, J.-C. Liou
  • Presented at the 5th European Conference on Space Debris, Darmstadt, Germany, March 30 – April 2, 2009
Micro-Satellite Impact Tests to Investigate Multi-Layer Insulation Fragments
  • Junko Murakami, Toshiya Hanada, Jer-Chyi Liou, Eugene Stansbery
  • Presented at the 5th European Conference on Space Debris, Darmstadt, Germany, March 30 – April 2, 2009
距離画像時系列データを用いたデブリ衝突痕の自律形状・位置同定
  • 藤田浩輝, 花田俊也
  • 日本機械学会ロボティクス・メカトロニクス講演会2009, 1A2-G05, 2009年5月25日.
Space Debris Impact Model for High Performance Simulator
Model for Determination of Spin-axis Attitude and its Covariances
Micro-satellite Impact Testing
GEODEEM 4.0: Updated Model for Better Understanding GEO Debris Environment
Impact of Fengyun-1C Accident on the LEO Debris Population
Benefits of Active Debris Removal on the LEO Debris Population
Survivability of Tether throughout Deorbiting
Structural Design of UNITEC-1
Photon Accerelation Model of Flexible Spinning Solar Sail
  • Yuya Mimasu, Akifumi Kitajima, Ryu Funase, Osamu Mori, Jun'ichiro Kawaguchi
  • 27th ISTS, 2009-k-44, July 9, 2009.
Development of a New Type Sensor for Micrometeoroid and Space Debris In-Situ Measurement at JAXA
  • Yukihito Kitazawa, A. Sakurai, T. Yasaka, K. Funakoshi, T. Hanada, H. Matsumoto
  • 27th ISTS, 2009-r-2-37p, July 9, 2009.
  • 2nd prize in poster session
System Design and Project Management for University Satellites
Trajectory Analysis of Small Solar Sail Demonstration Spacecraft Ikaros Considering the Uncertainty of Solar Radiation Pressure
  • Tomohiro Yamaguchi, Mutsuko Morimoto, Hiroshi Takeuchi, Makoto Yoshikawa, Yuya Mimasu, Yuichi Tsuda, Ryu Funase, Hirotaka Sawada, Osamu Mori
  • 27th ISTS, 2009-d-59, July 10, 2009.
Calibration Technique for Attitude Maneuvers of Spinning Satellites
Kalman Filter Unit-Vector Attitude Determination of Spin-Stabilized Satellites
ソーラーセイルにおける姿勢ダイナミクスを考慮した太陽輻射圧パラメータの推定
Estimation of Parameters of Solar Radiation Pressure by Analyzing Attitude Dynamics
CHOPIN: Methods and Results of the Fourth Global Trajectory Optimization Competition
Trajectory Estimation of the Hayabusa Sample Return Capsule Using Optical Sensors
小型ソーラーセイル実証機の軌道決定
Orbit Determination of Small Solar Sail Demonstration Spacecraft
Development of a New Type of Sensor for In-Situ Space Debris Measurement
  • Haruhisa Matsumoto, Yukihito Kitazawa, Akira Sakurai, Tetsuo Yasaka, Funakoshi Kunihiro, Toshiya Hanada, Sunao Hasegawa
  • The 10th Annual Advanced Maui Optical and Space Surveillance Technology (AMOS) Conference, Maui, Hawaii, US, September 1-4, 2009
九州大学における民生部品を利用した姿勢決定センサユニットの開発と評価
Development of COTS-based Sensor Unit for Attitude Determination
鹿児島衛星の打ち上げ準備状況
Progress Report of Kagoshima Satellite for Launch on 2010
  • 西尾正則, 宮原照昌, 佐藤哲郎, 東成生, 藤井亮, 林良太, 片野田洋, 中尾茂, 木下紀正, 時藤勉, 花田俊也, 氏原秀樹, 坂本祐二, 南竹力
  • 第53回宇宙科学技術連合講演会, 2F12, JSASS-2009-4293, pp. 1353-1355, 2009年9月10日.
小型ソーラーセイル実証機の太陽輻射圧加速度推定
Estimation of Solar Radiation Pressure Acceleration for Small Solar Sail Demonstration Spacecraft
  • 山口智宏, 三桝裕也, 津田雄一, 船瀬龍, 澤田弘崇, 森治, 森本睦子, 竹内央, 吉川真
  • 第53回宇宙科学技術連合講演会, 2F15, JSASS-2009-4296, pp. 1368-1373, 2009年9月10日.
高精度衛星運動シミュレータのためのスペースデブリ衝突擾乱モデル
Space Debris Impact Model for Satellite Dynamics Simulator
  • 平山寛
  • 第53回宇宙科学技術連合講演会, 3H09, JSASS-2009-4509, pp. 2368-2371, 2009年9月11日.
Development of a New Type Sensor for In-Situ Space Debris Measurement
  • Yukihito Kitazawa, Akira Sakurai, Tetsuo Yasaka, Kunihiro Funakoshi, Toshiya Hanada, Sunao Hasegawa, Haruhisa Matsumoto,
  • 60th International Astronautical Congress, IAC-09.A6.1.9, Daejeon, October 12, 2009.
Success Rate and Effect of using Electrodynamic Tether System for De-orbit LEO Spacecraft
Low-cost Small Satellite System for Electro-Dynamic Tether Demonstration Mission
Orbit Acquisition and Station-Keeping in Sun-Synchronous Orbit Using Solar Radiation Pressure
Low-cost Asteroid Mission Opportunities using Venus Gravity Assist
Solar Radiation Pressure Model for Attitude Motion of Hayabusa in Return Cruising
  • Yuya Mimasu, Jozef van der Ha, Ryu Funase, Osamu Mori, Junichiro Kawaguchi, Kenichi Shirakawa
  • 60th International Astronautical Congress, IAC-09.C1.9.9, Daejeon, October 14, 2009.
On the Stability of Spinning Satellites
  • Jozef van der Ha, Frank Janssens
  • 60th International Astronautical Congress, IAC-09.C1.6.2, Daejeon, October 15, 2009.
Trajectory Estimation of the Hayabusa Sample Return Capsule Using Optical Sensors
ΠΛΑΝΗΤΕΣ Could Be a True Story? Instability of the Current Debris Population in LEO
  • Toshiya Hanada
  • 第6回宇宙環境シンポジウム, JAXA-SP-09-006, AA0064542003, 2009年10月29日.
地球低軌道における能動的デブリ除去の効果について
  • 眞庭知成, 花田俊也, 河本聡美
  • 第6回宇宙環境シンポジウム, JAXA-SP-09-006, AA0064542032, 2009年10月30日.
静止軌道のスペースデブリの現況と将来予測
QSAT-DMC: A Constellation of In-situ Debris Measurement Satellites
  • K. Nagamine, K. Maniwa, S. Onishi, T. Hanada, A. Sakurai
  • Proceedings of the 2009 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2009), November 4-5, 2009, Gifu, Japan.
Small and Medium Orbital Debris Removal Using Special Density Material
  • T. Hanada, Y. Kitazawa, A. Kawabe, H. Matsumoto, S. Kawamoto
  • International Conference on Orbital Debris Removal, Chantilly Virginia, USA, December 8-10, 2009.
Strategies and Technologies for Cost Effective Removal of Large Sized Debris
  • S. Kawamoto, Y. Ohkawa, S. Nishida, S. Kitamura, S. Kibe, T. Hanada, M. Mine
  • International Conference on Orbital Debris Removal, Chantilly Virginia, USA, December 8-10, 2009.
「はやぶさ」再突入カプセル軌道決定の観測画像処理システム
Observation and Image Processing System for Trajectory Estimation of the Hayabusa Reentry Capsule
熱輻射圧が惑星間航行衛星に与える影響の研究
Effect of Thermal Radiation Pressure on Interplanetary Satellites
小型衛星のバッテリーユニット破裂実験
Lithium-ion Battery Explosion Test with Battery Unit
小型副衛星群を用いた微小デブリ観測網の構築に関する研究開発
QSAT-DMC: A Constellation of In-situ Debris Measurement Satellites
低密度物質による粒子捕獲の可能性について
Feasibility Study to Capture Particles with Low-density Materials
小型衛星群によるフェーズドアレーレーダを用いた軌道上デブリの実時間観測に関する研究
Study of Real-time Debris Observation Using Phased Array Radar with Small Satellites Constellation
Attitude Control for Low-Cost Asteroid Mission
慣性座標指向の小型人工衛星の磁気トルカを用いた姿勢制御
Attitude control for small satellite pointing inertial frame by magnetorquer
カイトプレーンとローバーのハイブリッド型CanSatの開発
Development of Hybrid CanSat with Kite Plane and Rover
静止軌道デブリ観測の高効率化の検討
Improving the efficiency of GEO debris observation

Last-modified: 2014-06-13 (Fri) 11:51:36 (1018d)