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Spaceflight Mechanics and Exploration Systems Laboratory

Publications.


Here you can find the full list of our laboratory's publications. You can filter by main collaborator, year, and type of publication by selecting or deselecting the appropriate buttons.

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Article Year
Journal Articles
Takao, Y., Mori, O., Matsushita, M., Sugihara, A. K., "Solar electric propulsion by a solar power sail for small spacecraft missions to the outer solar system," Acta Astronautica, Vol. 181, pp. 362-376, 2021, doi: 10.1016/j.actaastro.2021.01.020. 2021
Takao, Y., Mori, O., and Kawaguchi, J., "Analysis and Design of a Spacecraft Docking System Using a Deployable Boom," Acta Astronautica, Vol. 179, pp. 172-185, 2021. https://doi.org/10.1016/j.actaastro.2020.10.031 2021
Takao, Y., Mori, O., and Kawaguchi, J., "Self-Excited Oscillation of Spinning Solar Sails Utilizing Solar Radiation Pressure," Astrodynamics, Vol. 4, No. 3, pp. 177 - 192, 2020, doi:10.1007/s42064-018-0047-4. 2020
Takao, Y., Mimasu, Y., and Tsuda, Y., “Simultaneous Estimation of Spacecraft Position and Asteroid Diameter During Final Approach of Hayabusa2 to Ryugu,” Astrodynamics, Vol. 4, No. 2, 2020, pp. 163–175, doi:10.1007/s42064-020-0078-5. 2020
Takao, Y., Mori, O., and Kawaguchi, J., “Optimal Interplanetary Trajectories for Spinning Solar Sails Under Sail-Shape Control,” Journal of Guidance, Control, and Dynamics, Vol. 42, No. 11, 2019, pp. 2541–2549, doi:10.2514/1.G003776. 2019
Takao, Y., Tsuda, Y., Saiki, T., and Ogawa, N., “Model-Based Optical Navigation for Autonomous Landing on Asteroids,” Advances in the Astronautical Sciences, Vol. 168, No. 4, 2019, pp. 4279–4292. 2019
Takao, Y., Kikuchi, S., Mori, O., and Kawaguchi, J., “Attitude Control of Spinning Solar Sails Based on Modal Analysis,” Advances in the Astronautical Sciences, Vol. 167, No. 3, 2019, pp. 2825–2834. 2019
Takao, Y., Chujo, T., Mori, O., and Kawaguchi, J., “Active Shape Control of Spinning Membrane Space Structures and Its Application to Solar Sailing,” Transactions of the Japan Society for Aeronautical and Space Sciences, Vol. 61, No. 3, 2018, pp. 119–131, doi:10.2322/tjsass.61.119. 2018
松本, 純 and 岡本, 千里 and 青木, 順 and 大木, 優介 and 中村, 拓磨 and 柏岡, 秀哉, "Concept of Integrated Excavation/Sampling Device and Its Verification Experiment Results", Transactions of the Japan Society for Aeronautical and Space Sciences, 61, 60-68, 2018. 2018
Tsuda, Y., Ono, G., Saiki, T., Mimasu, Y., Ogawa, N., Terui, F., “Solar Radiation Pressure-Assisted Fuel-Free Sun Tracking and Its Application to Hayabusa2” Journal of Spacecraft and Rockets 2017 54:6, 1284-1293, doi.org/10.2514/1.A33799 2017
高尾 勇輝, 森 治, “連成振動を伴うスピン型ソーラーセイルの姿勢運動,” 航空宇宙技術, Vol. 16, 2017, pp. 81–89, doi:10.2322/astj.JSASS-D-17-00004. 2017
Tsuda, Y., Nakazawa, S., Kushiki, K., Yoshikawa, M., Kuninaka, H., Watanabe, S., Flight Status of Robotic Asteroid Sample Return Mission Hayabusa2, ActaAstronautica, Vol.127, pp.702-709, doi:10.1016/j.actaastro.2016.01.027, Accepted on Jan 15, 2016. 2016
水野貴秀,加瀬貞二,野田寛大,國森裕生,千秋博紀,尾川順子,竹内央,山口智宏,佐伯孝尚,並木則行,津田雄一,はやぶさ2LIDARの開発と光リンク機能を使った初期動作チェック,信学技法,電子情報通信学会,SANE2016-02, pp.7-12, 2016 2016
Ono, G., Tsuda, Y., Akatsuka, K., Saiki, T., Mimasu, Y., Ogawa, N., Terui, F., Generalized Attitude Model for Momentum-Biased Solar Sail Spacecraft, Journal of Guidance, Control and Dynamics, Vol. 39, No. 7, pp.1491-1500, doi: 10.2514/1.G001750, 2016, accepted on Jan.1, 2016. 2016
津田雄一,小惑星探査機「はやぶさ2」ミッションの概要と現況,特集「JAXAにおける宇宙開発と宇宙材料,日本材料科学会誌,Vol.53, No.6, December, 2016. 2016
Naoya Takeishi, Akira Tanimoto, Takehisa Yairi, Yuichi Tsuda, Fuyuto Terui, Naoko Ogawa and Yuya Mimasu, Evaluation of Interest-region Detectors and Descriptors for Automatic Landmark Tracking on Asteroids, Transactions of the Japan Society for Aeronautical and Space Sciences, Vol.58, No.1, 2015. 2015
Jozef van der Ha, Yuya Mimasu, Yuichi Tsuda, Osamu Mori, Solar and Thermal Radiation Models and Flight Evaluation for IKAROS Solar Sail,AIAA Journal of Spacecraft and Rocket, Vol.50, No.3, 2015, accepted on 2015/2/19. DOI: 10.2514/1.A33158 2015
Chujo, T., Tsuda, Y., Shimizu, Y., Yoshikawa2, M., Yano, H., Mars impact probability analysis for the Hayabusa-2 NEO sample return mission, Advances in Space Research, Vol.57, pp.1991-2002, 2016, accepted on 2015/7/30. doi:10.1016/j.asr.2015.07.042 2015
大島武,津田雄一,小惑星探査機「はやぶさ2」―深宇宙のための自律化技術―(小特集 宇宙開発への情報技術の貢献),情報処理(情報処理学会),Vol.56, No.7, 2015年7月. 2015
Chujo, T., Tsuda, Y., and Kawaguchi, J.: Analysis of Sail Deformation Based on Attitude Motion of Spinning Solar Sail, The 29 ISTS Special Issue of Transaction of JSASS, pp.Pd_53 - Pd_59 , 2014, Accepted on January 24th, 2014. 2014
Kuroda, D., Ishiguro, M., Takato, N., Hasegawa, S., Abe, M., Tsuda, Y., Sugita, S.,Usui, F., Hattori, T., Iwata, I., Imanishi, M., Terada, H., Choi, Y., Watanabe, S., and Yoshikawa, M., Visible wavelength spectroscopy of sub-km-sized Near-Earth Asteroids with low delta-v, accepted, Publications of the Astronomical Society of Japan(PASJ), Vol.66, issue 3, 2014, accepted on Feb.14, 2014. 2014
照井冬人,津田雄一,尾川順子,三桝裕也,小惑星探査機「はやぶさ2」の航法誘導制御における自動・自律機能 (特集 宇宙に挑む人工知能技術),人工知能,Vol.29, No.4, 2014, pp.327-334. 2014
Giancotti, M., Campagnola, S., Tsuda, Y., Kawaguchi, J. , Families of periodic orbits in Hill’s problem with solar radiation pressure: application to Hayabusa 2, Celestial Mechanics and Dynamical Astronomy, Vol.120, Issue 3, pp.269-286, 2014, doi: 10.1007/s10569-014-9564-5. 2014
津田雄一,白澤洋次,佐伯孝尚,三桝裕也,船瀬龍,河内宏道,卯尾匡史,谷口正,石橋史朗,IKAROSの姿勢系システム (< 特集 > 小型ソーラー電力セイル実証機「IKAROS(イカロス)」第6回),日本航空宇宙学会,Vol.61, No.4., 2013, pp.136-142. 2013
Tsuda, Y., Saiki, T., Funase, R., Mimasu, Y., Generalized Attitude Model for Spinning Solar Sail Spacecraft, AIAA Journal of Guidance, Control and Dynamics, , Vol. 36, No. 4, 2013, pp. 967-974. doi:10.2514/1.59516. 2013
Yamaguchi, T., Mimasu, Y., Tsuda, Y., and Yoshikawa, M., Hybrid Estimation of the Solar Radiation Pressure for a Spinning Solar Sail Spacecraft, Engineering note, Journal of Spacecraft and Rockets, doi:10.2514/1.A32387, 2013, Accepted on April 2013. 2013
Tsuda, Y., Yoshikawa, M., Abe, M., Minamino, H., Nakazawa, S., System Design of The Hayabusa 2 – Asteroid Sample Return Mission To 1999 JU3,Acta Astronautica, Vol.90, pp.356-362, 10.1016/j.actaastro.2013.06.028, 2013. 2013
Tsuda, Y., Terui, F., Saiki, T., Ground-Based Guidance and Navigation for Kinetic Impact to Asteroid 1999JU3, Transactions of JSASS, Aerospace Technology Japan, Accepted on Oct. 30, 2013. 2013
Tsuda, Y., Mori, O., Funase, R., Sawada, H., Yamamoto, T., Saiki T., Endo, T., Yonekura, K., Hoshino, H., Kawaguchi, J., Achievement of IKAROS –Japanese Deep Space Solar Sail Demonstration Mission, Acta Astronautica,Volume 82, Issue 2, February 2013, pp.183–188. doi:10.1016/j.actaastro.2012.03.032. 2012
Tsuda, Y., Saiki, T., Mimasu, Y., Yamaguchi, T., Ikeda, H., Nakamiya, M., Takeuchi, H. and IKAROS Demonstration Team, Modetdng of Solar Radiation Pressure Effect for Trajectory Guidance of Spinner Solar Sailer IKAROS, Transaction of JSASS, Aerospace Technology Japan, Vol. 10, No. ists28, pp. Po_4_7-Po_4_12, 2012. 2012
Soma, E., Endo, T., , Tanaka, K., Miyauchi, M., Yokota, R., Tsuda, Y., Mori, O. and IKAROS Demonstration Team,Flexible Solar Array of Small Solar Power Sail Demonstrator “IKAROS”,Trans. JSASS Aerospace Tech. Japan Vol. 10, No. ists28, pp. Po_4_27-Po_4_31, 2012. 2012
Mori, O, Tsuda, Y., Sawada, H., Funase, R., Saiki, T., Yamamoto, T., Yonekura, K., Hoshino, H., Minamino, H., Endo, T., Kawaguchi, J. and IKAROS Demonstration Team,IKAROS and Extended Solar Power Sail Missions for Outer Planetary Exploration, Trans. JSASS Aerospace Tech. Japan, Vol. 10, No. ists28, pp. Po_4_13-Po_4_20, 2012. 2012
Mori, O, Shirasawa, Y., Sawada, H., Tsuda, Y., Funase, R., Saiki, T., Yamamoto, T., Motooka, N., Jifuku, R., Attitude Dynamics of Spinning Solar Sail "IKAROS" Considering Thruster Plume, Transactions of JSASS, Aerospace Technology Japan, Vol.10, pp.27-32, 2012. 2012
森治,津田雄一,ソーラー電力セイル実証機IKAROS,日本物理学会誌, Vol.67, No.6, 2012, pp378-384. 2012
津田雄一,森治,白澤洋次,三桝裕也,澤田弘崇,船瀬龍,遠藤達也,山本高行,田中孝冶,横田力男,川口淳一郎,JAXAにおけるソーラーセイル展開展張技術の開発経緯(特集 小型ソーラー電力セイル実証機「IKAROS(イカロス)」第2回),日本航空宇宙学会,Vol.60, No.10, 2012, pp.357-363. 2012
Tanaka, K., Tsuda, Y., Saiki, T., Shirasawa, Y., Jifuku, R., The Development of Spherical Gas Bearings for the 3DRW Operated by a Small Air Supptder, Transactions of JSASS, Aerospace Technology Japan, Vol. 10 (2012) No. ists28. 2012
森治,津田雄一,澤田弘崇,佐伯孝尚,船瀬龍,イカロスの技術(ソーラーセイル),人工知能学会誌,Vol.26, No.2, pp.164-175, 2011, (招待論文,特集「宇宙探索と人工知能」) 2011
Tsuda, Y., Mori, O., Funase, R., Sawada, H., Yamamoto, T., Saiki, T., Endo, T., Kawaguchi, J., Flight Status of IKAROS Deep Space Solar Sail Demonstrator, Acta Astronautica Vol.69, 2011, pp.833-840. 2011
Funase, R., Shirasawa, Y., Mimasu, Y., Mori, O., Tsuda, Y., Saiki, T., Kawaguchi, J., On-orbit Verification of Fuel-free Attitude Control System for Spinning Solar Sail Utitdzing Solar Radiation Pressure, Advances in Space Research, Volume 48, Issue 11, 1 December 2011, Pages 1740-1746. 2011
津田雄一,大面積柔軟膜面を有する軸対称スピン物体の姿勢安定条件,日本航空宇宙学会誌, Vol.58, No.678, pp187-194, 2010. 2010
Mimasu, Y., Kitajima A., Yamaguchi, T., Funase, R., Morimoto, M. Y., Sawada, H., Takeuchi, H., Mori, O., Tsuda, Y. and Kawaguchi, J., Photon Acceleration Model of Flexible Spinning Solar Sail, Transactions of JSASS, Aerospace Technology Japan, Vol. 8 (2010) No. ists27 pp.Pk_1-Pk_6. 2010
Ogawa, N., Morimoto, M. Y., Tsuda, Y., Yamada, T., Fujita, K., Yamaguchi, T., Kawakatsu, Y., Kubota, T. and Kawaguchi, J., Pretdminary Mission Analysis and Orbit Design for Next Mars Exploration, Transactions of JSASS Aerospace Technology Japan, Vol. 8 (2010) No. ists27 pp.Tk_7-Tk_12. 2010
Yanaguchi, T., Mimasu, Y., Tsuda, Y., Funase, R., Sawada, H., Mori, O., Morimoto, M. Y., Takeuchi H. and Yoshikawa, M., Trajectory Analysis of Small Solar Sail Demonstration Spacecraft IKAROS Considering the Uncertainty of Solar Radiation Pressure, Transactions of JSASS, Aerospace Technology Japan, Vol. 8 (2010) No. ists27 pp.Pd_37-Pd_43. 2010
Mori, O., Sawada, H., Funase, R., Morimoto, M. Y., Endo T., Yamamoto T., Tsuda, Y., Kawakatsu Y., Kawaguchi J., Miyazaki Y., Shirasawa, Y., IKAROS Demonstration Team and Solar Sail Working Group, First Solar Power Sail Demonstration by IKAROS, Transactions of JSASS, Aerospace Technology Japan, Vol. 8 (2010) No. ists27 pp.To_4_25-To_4_31. 2010
Sasaki, S., Fujimoto, M., Takashima T., Yano, H., Kasaba, Y., Takahashi Y., Kimura, J., Okada, T., Kawakatsu, Y., Tsuda, Y., Kawaguchi, J., Funase, R., Mori, O., Morimoto M., Ikoma, M., Naganuma T, Yamaji, A., Hussmann, H., Kurita, K. and Jupiter Working Group, Exploration of the Jovian System by EJSM (Europa Jupiter System Mission): Origin of Jupiter and Evolution of Sateltdtes, Transactions of JSASS, Aerospace Technology Japan, Vol. 8 (2010) No. ists27 pp.Tk_35-Tk_38. 2010
Tsuda, Y., Scheeres, D.J., Numerical Method of Symplectic State Transition Matrix and Application to Fully Perturbed Earth Orbit, Transactions of the Japan Society for Aeronautical and Space Sciences, Vol.53, No.180, pp.105-113, Aug., 2010. 2010
Tsuda, Y., State Transition Matrix Approximation with Geometry Preservation for General Perturbed Orbits, Acta Astronautica, 2010.09., SSN 0094-5765, DOI: 10.1016/j.actaastro.2010.09.016. 2010
Tsuda, Y., Scheeres, D.J.,, Series Expansion Form of an Approximate State Transition Matrix for Fully Perturbed Orbits, Transaction of JSASS, Aerospace Technology Japan, Vol. 8, 2010, pp.Pd_53-Pd_60. 2010
Shirasawa, Y., and Tsuda, Y., System Performance Analysis of Three Dimensional Reaction Wheel for the Attitude Control of Microsateltdtes, Trans. JSASS Space Tech. Japan, Vol. 7 (2009), pp.Pd_105-Pd_110. 2009
Toda, T., Saito, Y., and Tsuda, Y., Design and Experimental Vatddation of Inter-Sateltdte tdnk System for Formation Flight SCOPE Mission, Trans. JSASS Space Tech. Japan, Vol. 7 (2009), No. ists26, pp.Pj_1-Pj_6. 2009
[査読15] Tsuda, Y., Scheeres, D. J., Computation and Applications of an Orbital Dynamics Symplectic State Transition Matrix, Journal of Guidance, Control, and Dynamics, Vol. 32, No. 4, pp.1111-1123, 2009. 2009
Saiki, T., Nakaya, K., Yamamoto, T., Tsuda, Y., Mori, O., Kawaguchi, J., Development of a Small-spin-axis Controller and Its Application to a Solar Sail Subpayload Sateltdte, Transaction of the Japan Society for Aeronautical and Spae Sciences, Space Technology Japan, Vol. 7, pp.25-32, 2009. 2009
Funase, R., Hanaoka, F., Mori, O., Tsuda, Y. and Kawaguchi, J., Development of Oscillation-Free Attitude Maneuvering System for Spinning Solar Sail, Transactions of JSASS, Space Technology Japan, Vol. 7 (2009) No. ists26 pp.Pd_49-Pd_55. 2009
Tsuda, Y., Scheeres, D.J., State Transition Matrix Approximation Using a Generalized Averaging Method, Journal of Guidance, Control, and Dynamics, Vol. 32, No. 6, pp.1781-1794, 2009, doi: 10.2514/1.44142. 2009
齋藤宏文, 水野貴秀, 川原康介, 佐伯孝尚, 津田雄一, 福島洋介, 浜田裕介, 佐々木博幸, 勝本幸子, 黒木聖司, 梶川泰広, 車載用技術を利用した超小型宇宙用GPS受信機の開発と軌道上実証, 日本航空宇宙学会論文集,Vol. 56, No. 650, 2008. 2008
Funase, R., Nakasuka, S., Sako, N., Fujiwara T., Tsuda, Y., Ukawa, S., Kimura, S., Hashimoto, H., Yoshihara, K. and Yamamoto, T., On-Orbit Experiment of Vision-Based Motion Estimation and Tracking of Tumbtdng Object in Space, Transactions of the Japan Society for Aeronautical and Space Sciences, Vol.50, No.168, pp.97-104,2007. 2007
津田雄一, 中須賀真一, 制御量制約を考慮した高速タンブリング物体の実時間姿勢制御法 第三報 —保存性状態量を利用したフィードバック制御則—, 日本航空宇宙学会誌, Vol. 54, No. 627, pp.151-159, 2006. 2006
Tsuda, Y., Mori, O., Takeuchi, S., Kawaguchi, J., Flight Result and Analysis of Solar Sail Deployment Experiment Using S-310 Sounding Rocket, Space Technology, Vol.26, No.1-2, pp.33-39, 2006. 2006
津田雄一, 中須賀真一, 続報:制御量制約を考慮した高速タンブリング物体の実時間姿勢制御法 —保存性状態量による剛体ダイナミクスの定式化—, 日本航空宇宙学会誌, Vol.53, No.616, pp200-208, 2005. 2005
中須賀真一, 酒匂信匡, 津田雄一, 永島隆, 船瀬龍, 中村友哉, 永井将貴,CubeSat-XIの軌道上実証成果と超小型衛星による低コスト化・短期開発化の試み, 電子情報通信学会論文誌 VOL.J88-B, No.1, 2005. 2005
河原吉伸, 津田雄一, 中須賀真一, 多数機フォーメーションフライトの為の連続推力推進による燃料最小誘導則, 日本航空宇宙学会誌, Vol.52, No.601, pp72-79, 2004. 2004
Tsuda, Y., Nakasuka, S., New Attitude Motion Following Control Algorithm for Capturing Tumbtdng Object in Space, Acta Astronautica Vol. 53, No.11, pp.847-861, 2003. 2003
津田雄一, 中須賀真一, `制御量制約を考慮した高速タンブリング物体の実時間姿勢制御法, 日本航空宇宙学会誌, Vol.50, No.584, pp1-8, 2002. 2002
Nakasuka, S., Aoki, T., Ikeda, I., Tsuda, Y. and Kawakatsu, Y., “Furoshiki Sateltdte" -A Large Membrane Structure as a Novel Space System, Acta Astronautica, Vol.48, No.5-12, pp.461-468, 2001. 2001
Sako, N., Ota, S., Tsuda, Y., Yamamoto, T., Ikeda, I., Ii, H., Yamamoto, H., Tanaka, H., Eishima, T., Tanaka, A., Nakasuka, S., “CanSat” Suborbital Launch Experiment –University Educational Space Program Using Can Sized Pico-Sateltdte, Acta Astronautica, Vol. 48, No.5-12, pp.767-776, 2001. 2001
藤原健, 中村大賀, 津田雄一, 中須賀真一, 軌道上の浮遊物体に対する運動状態の認識とその捕獲(第1報) --全体像と運動推定問題--, 日本航空宇宙学会誌, Vol.47, No.547, pp1-7, 1999. 1999
Conference Proceedings (International)
Gutierrez-Ramon, R., Liang, Y., Tsuda, Y., “Design of a Deep Space Orbit Transfer Vehicle (DS-OTV) Architecture”, AIAA/AAS, Astrodynamics Specialist Conference, AAS 20-532, 2020. 2020
Takao, Y. and Tsuda, Y., “Landmark-Free Optical Navigation Around Small Bodies: Application to the Hayabusa2 Touchdown on Ryugu,” 70th International Astronautical Congress, Washington, D.C., 2019. 2019
Kashioka, S.; Ohira, G.; Takao, Y.; Kadokura, M.; Iota, T. & Tsuda, Y., "Position Estimation Method Using Asteroid Shape Model and Vector Code Correlation for On-board Optical Navigation", 32nd International Symposium on Space Technology and Science, Transactions of Japan Society for Aeronautical and Space Sciences, 2019 2019
Kashioka, S. & Tsuda, Y., "Analysis of bidirectional reflection distribution function on a solar cell with a microstructure", Proceedings of the International Astronautical Congress, IAC, 2018 2018
Takao, Y., Mori, O., and Kawaguchi, J., “Interplanetary Mission Design for Spinning Solar Sails Uti- lizing Active Shape Control of Sail Membranes,” 2018 Space Flight Mechanics Meeting, Kissimmee, FL, 2018, doi:10.2514/6.2018-0212. 2018
Takao, Y., “Attitude and Orbit Control of a Spinning Solar Sail by the Vibrational Input on the Sail Membrane,” 31st International Symposium on Space Technology and Science, Ehime, Japan, 2017. 2017
Takao, Y., Chujo, T., Mori, O., and Kawaguchi, J., “Attitude Control of a Spinning Solar Sail by the Active Control of the Sail Deformation,” 4th International Symposium on Solar Sailing, Kyoto, Japan, 2017. 2017
Tsuda, Y., Ono, G., Generalized Attitude Dynamics Model for Angular Momentum Stabilized Sail, 4th International Solar Sail Symposium, No.17078, Kyoto, 2017.1.29. 2017
Tsuda, Y., Yoshikawa, M., Flight Status of Hayabusa2: Asteroid Sample Return Mission to C-type Asteroid Ryugu, 14th SBAG(Small Body Assessment Group) meeting, 2016.1.28. 2016
Takao, Y., Tsuda, Y., Saiki, T., Ogawa, N., Terui, F., and Kawaguchi, J., “Optical Navigation for Asteroid Explorer by use of Virtual Feature Points,” AIAA/AAS Astrodynamics Specialist Conference, Long Beach, CA, 2016, doi:10.2514/6.2016-5213. 2016
Tsuda, Y., Ono, G., Saiki, T., Mimasu, Y., Ogawa, N., Terui, F., SRP-Assisted Fuel-Free Sun Tracking and Its Application to Hayabusa2, AIAA/AAS, Astrodynamics Specialist Conference, AIAA-2016-5379, 2016. 2016
Takao, Y., Kawasaki, S., Yamada, K., Chujo, T., Kikuchi, S., Ikemoto, K., Kitao, S., Kato, H., and Mori, O., “Lander System for the Trojan Asteroid Explorer and its Sample Return Scenario,” Jupiter Trojan 2016 , Sagamihara, Japan, 2016. 2016
Tsuda, Y., Yoshikawa, M., Flight Status of Hayabusa2: Asteroid Sample Return Mission to C-type Asteroid Ryugu, 15th SBAG(Small Body Assessment Group) meeting, 2016.6.28. 2016
Tsuda, Y., Watanabe, S., Saiki, T., Yoshikawa, M., Nakazawa, S., Cruise Status of Hayabusa2 : Round Trip Mission to Asteroid 162173 Ryugu, 67th International Astronautical Congress, IAC-16.A3.4.5, Guadalajara, Mexico, 2016. 2016
Tsuda, Y., Nakazawa, S., Kushiki, K.,, Yoshikawa, M., Watanabe, S., Kuninaka, H., Flight Status of Robotics Asteroid Sample Return Mission Hayabusa 2, 9th IAA Symposium on the Future of Space Exploration: Towards New Global Programmes, IAA-FSE-15-11-01, Torino, Italy, 2015.7.9. 2015
Tsuda, Y., Electric-Delta V Earth Gravity Assist Phase Operation of Hayabusa2, 2015 ISAS Workshop on Astrodynamics and Flight Mechanics, B-17, Sagamihara, 2015.7.28. 2015
Tsuda. Y., Ono, G., Akatsuka, K., Saiki, T., Mimasu, Y., Ogawa, N., Terui, F., Generalized Attitude Model for Momentum-Biased Solar Sail Spacecraft, AAS Astrodynamics Specialist Conference, AAS15-656, Vail, CO, 2015.8.12. 2015
Tsuda, Y, Kato, T., Shiraishi, M., Matsuoka, M., Trajectory Guidance and Navigation Operation Toward Earth Swing-by of Asteroid Sample Return Mission “Hayabusa2” , 25th International Symposium on Space Flight Dynamics, Munich, Germany, 2015.10.19. 2015
Van Der Ha, J.C., Mimasu, Y., Tsuda, Y., Mori, O., Solar and Thermal Radiation Pressure Models and Flight Evaluation for IKAROS Solar Sail, AAS Space Flight Mechanics Meeting, AAS14-244, Santa Fe, NM, 2014.1.26-30. 2014
Tsuda, Y., Systematic Interpretation of Spacecraft Dynamics Under the Effect of Solar Radiation Pressure, 24th Workshop on Astrodynamics and Flight Mechanics, C-13, Sagamihara, 2014.7.28. 2014
Tsuda, Y., Chujo, T., Shimizu, Y., Yano, Y., Mars Impact Probabitdty Analysis For The Hayabusa-2 NEO Sample Return Mission, PPP.2-3-14, 40th COSPAR Scientific Assembly, Moscow, 2014.8.2-10. 2014
Tsuda, Y., Terui, F., Saiki, T., Ground-Based Guidance and Navigation for Kinetic Impact to Asteroid 1999 JU3, 29th International Symposium on Space Technology and Science, Nagoya, 2013. 2013
Van Der Ha, J.C., Mimasu, Y., Tsuda, Y., Mori, O., Solar and Thermal Radiation Pressure Models and In-Flight Evaluation for IKAROS Solar Sail, 29th International Symposium on Space Technology and Science, Nagoya, 2013. 2013
Brémond, L., Tsuda, Y., Funase, R., Kawaguchi, J., A Trajectory Optimization for a Multiple Rendezvous Mission with Trojan Asteroids, AAS Space Flight Mechanics Meeting, AAS 13-497, Kauai, 2013.2. 2013
Ikeda, H., Tsuda, Y., Mimasu, Y., Yoshikawa, M., A Simulation Study of Gravity and Ephemeris Estimation of Asteroid 1999JU3 Using Spacecraft Radiometric Tracking, Optical and Altimeter Measurements, AAS Space Flight Mechanics Meeting, AAS13-417, Kauai, 2013.2. 2013
Mimasu, Y., Taniguchi, S., Takeuchi, H., Shirasawa, Y., Yonekura, K., Mori, O., Funase, R., Saiki, T., Tsuda, Y., Long-Term Attitude and Orbit Prediction of Solar Sailing IKAROS While Being Lost in Space, AAS Space Flight Mechanics Meeting, AAS13-406, Kauai, 2013.2. 2013
Tsuda, Y. and IKAROS Demonstration Team, How IKAROS Shape is Designed -Attitude Stabitdty of Spinning Solar Sail, The 3rd International Symposium on Solar Sailing, Glasgow, UK, June 11-13, 2013 2013
Tsuda, Y., Saiki, T. and Mimasu, Y., Realization of Minimal Attitude Determination System for Small Spinner Spacecraft IKAROS, Small Sateltdte Conference, SSC13-IV-4, Logan, Utah, 2013.8.13. 2013
Tsuda, Y., Okano, Y., Mimasu Y., Funase, R., On-Orbit Sail Quatdty Evaluation Utitdzing Attitude Dynamics of Spinner Solar Sailer IKAROS, AAS/AIAA Space Flight Mechanics Meeting, AAS12-211, 2012.2.1, Charleston; Also Advances in the Astronautical Sciences, Vol.143, pp.1609-1626, 2012. 2012
Tsuda, Y., Mimasu, Y., Funase, R., Okano, Y., Design Criteria of Spinning Solar Sail Surface Based on Attitude Dynamics, AIAA/AAS Astrodynamics Specialist Conference, AIAA2012-4662, Minneapotds, 2012.8.14. 2012
Tsuda, Y., Yoshikawa, M., Minamino, N., Nakazawa, S., System Design of Hayabusa2 –Asteroid Sample Return Mission to 1999JU3, 63rd International Astronautical Congress, IAC-12-A.3.4.5, Naples, 2012.10.4. 2012
Tsuda, Y., Saiki, T., Ogawa, N., Morimoto, M., Trajectory Design for Japanese New Asteroid Sample Return Mission Hayabusa-2, 23rd International Symposium on Space Flight Dynamics, IMD-1-1, Pasadena, 2012.10.29. 2012
Tsuda, Y., Saiki, T., Mimasu, Y. and Funase, R., Modetdng of Attitude Dynamics for IKAROS Solar Sail Demonstrator, AAS/AIAA Space Flight Mechanics Meeting, AAS11-112, 2011.2.14, New Orleans. 2011
Tsuda, Y., Saiki, T., Funase, R., Shirasawa, Y., Mimasu, Y., Shape Parameters Estimation of IKAROS Solar Sail Using In-Flight Attitude Determination Data, 12th AIAA Gossamer Systems Forum, 53-GSF-5-2, Apr.11,2011, Denver. 2011
Tsuda, Y., Saiki, T., Mimasu, Y., Yamaguchi, T., Ikeda, H., Nakamiya, M., Takeuchi, H. and IKAROS Demonstration Team, Modetdng of Solar Radiation Pressure Effect for Trajectory Guidance of Spinner Solar Sailer IKAROS, 28th International Symposium on Space Technology and Science, ISTS ISTS-o-4-10v, Okinawa, Japan, 2011.6.11. 2011
Tsuda, Y., Saiki, T., Mimasu, Y. and Funase, R., Sun-Earth Based Spin Axis Determination for Interplanetary Missions and Its Application to IKAROS, 2011 AIAA/AAS Astrodynamics Specialist Conference, AAS11-448, Girdwood, Alaska, 2011.8.2. 2011
Tsuda, Y., Reduction of Truncation Error in Computing Symplectic State Transition Matrix, 2010 AIAA/AAS Astrodynamics Specialist Conference, AIAA-2010-7660, Aug.2, 2010, Toronto. 2010
Tsuda, Y., Unscented Batch Sequential Filter and Its Application to Relative Orbit Determination for Formation Flight, 8th IFAC Symposium on Automatic Control in Aerospace, Sep. 6.2010, Nara. 2010
Tsuda, Y., Mori, O., Funase, R., Sawada, H., Yamamoto, T., Saiki, T., Endo, T. and Kawaguchi, J., Flight Status of IKAROS Deep Space Solar Sail Demonstrator, 61th International Astronautical Congress, IAC-10-A3.6.8, 2010.10.1, Prague. 2010
Tsuda, Y., Scheeres, D. J., Computation and Applications of an Orbital Dynamics Symplectic State Transition Matrix, 19th AAS/AIAA Space Flight Mechanics Meeting, AAS-09-158, Feb 8-12, 2009, Savannah, Georgia. 2009
Shirasawa, Y., Tsuda, Y., Development of Control and Measurement System for the Three-Dimensional Reaction Wheel, 19th AAS/AIAA Space Flight Mechanics Meeting,AAS-09-170, Feb 8-12, 2009, Savannah, Georgia. 2009
Fujimoto, M., Tsuda, Y., Saito, Y., Shinohara, I., Takashima, T., Matsuoka, A., Kojima, H., and Kasaba, Y., The SCOPE Mission, American Institute of Physics, Conf. Proc. Volume 1144, pp. 29-35 (s2009). 2009
Tsuda, Y., Series Expansion Form of an Approximate State Transition Matrix for Fully Perturbed Orbits, 27th International Symposium on Space Technology and Science, ISTS 2009-d-27, Tsukuba, Japan, 2009.7.8. 2009
Tsuda, Y., Scheeres, D. J., State Transition Matrix Approximation Using a Generalized Averaging Method, AAS/AIAA Astrodynamics Specialist Conference, AAS-09-444, Pittsburgh, 2009.8.13. 2009
Tsuda, Y. and Saito, Y., Formation Keeping and Changing Strategy for SCOPE Formation Flight Mission, 21th International Symposium on Space Flight Dynamics, Toulouse, 2009.9.29. 2009
Tsuda, Y., State Transition Matrix Approximation with Geometry Preservation for General Perturbed Orbits, 60th International Aeronautical Congress, IAC-09.C1.2.3, Daejeon, Korea, 2009.10.13. 2009
Shirasawa, Y., Tsuda, Y., Experimental Study and Analysis on Three Dimensional Reaction Wheel for Microsateltdtes, 18th AAS/AIAA Space Flight Mechanics Meeting, AAS 08-132, Jan 28, 2008. 2008
Hanaoka, F., Mori, O., Tsuda, Y. and Kawaguchi, J., Attitude Control of Spinning Solar Sail with Huge Membrane, 18th AAS/AIAA Space Flight Mechanics Meeting, AAS 08-221, Jan 28, 2008. 2008
Tsuda, Y., Stabitdty Criteria for the Spinning Spacecraft with Large Flexible Membrane, AIAA Guidance, Navigation and Control Conference, AIAA-2008-6456, 2008.8.18-21, Honolulu. 2008
Funase, R., Tsuda, Y., Mori, O, Hanaoka, F. and Kawaguchi, J., Attitude Control of Spinning Solar Sail Considering the Deformation by Solar Radiation Pressure, 59th International Astronautical Congress, IAC-08.C1.7.8, Sep 29-Oct 3, 2008, Glasgow, Scotland. 2008
Kawaguchi, J., Tsuda, Y., Mori, O., Yamamoto, T., Funase, R., Sawada, H., Kawakatsu, Y. and Morimoto, M., World’s First Solar Power Sail Demonstration Flight in Interplanetary Cruise in 2010, 59th International Astronautical Congress, IAC-08.A3.6.15, Sep 29-Oct 3, 2008, Glasgow, Scotland. 2008
Tsuda, Y., An Attitude Control Strategy for Spinning Solar Sail, 17th IFAC Symposium on Automatic Control in Aerospace, WE-P02, 2007.6.25-29 Toulouse. 2007
Tsuda, Y., Optimal Formation Design Strategy for Formation-Flying Mission in High-Eltdptic Orbit,11th International Space Conference of Pacific-basin Societies,2007.5.16-18, Beijin. 2007
Tsuda, Y., Formation Design Strategy For Scope High Eltdptic Formation Flying Mission, 20th International Symposium on Space Flight Dynamics, 3-13, September 23-28, 2007, Annapotds. 2007
Shibasaki, Y., Tsuda, Y. and Kawaguchi, J., Optimization of Return Trajectories for Orbital Transfer Vehicle Between Earth and Moon, 20th International Symposium on Space Flight Dynamics, 19-2, September 23-28, 2007, Annapotds. 2007
Tsuda, Y., Saito, Y. and Toda, T., Ontdne Relative Range Determination and Clock Synchronization Algorithm for Formation Flying Spacecrafts, AAS/AIAA Space Flight Mechanics Conference, AAS06-205, Tampa,USA, 2006.1. 2006
Tsuda, Y., Nakaya, K. and Yamamoto, T., Microsateltdte-Class Solarsail Demonstrator –Mission Design and Development Status–, 25th International Symposium on Space Technology and Science, ISTS 2006-k-37, Kanazawa, Japan, 2006.6. 2006
Tsuda, Y., Mori, O., Takeuchi, S. and Kawaguchi, J., Flight Result and Analysis of Solar Sail Deployment Experiment Using S-310 Sounding Rocket, 56th International Astronautical Congress, IAC-05-C1.4.05, Fukuoka, Japan, 2005.10. 2005
Tsuda, Y., Maezawa, K., Shinohara, I., Saito, Y., Higuchi, L, Toda, T., Takashima, T., Kojima, H. and Fujimoto, M., Mission Design of SCOPE –Small Sateltdtes Formation Flying Mission for Magnetospheric Tail Observation–, 6th AIAA International Conference on Low Cost Planetary Missions, Kyoto, Japan, 2005.10. 2005
Tsuda, Y., Mori, M., Nishimura, Y., Kawaguchi, J., Deployment Experiment of Thin Flexible Membrane Using Sounding Rocket for Future Solar Sail Mission, 24th International Symposium on Space Technology and Science, ISTS2004-c-11, Miyazaki, Japan ,2004.5. 2004
Tsuda, Y., Global Optimization of Maneuver Schedule for Multiple Spacecrafts Flying in Formaon, 55th International Astronautical Congress, IAC-04-A.2.01, Vancouver, 2004.10. 2004
Tsuda, Y., Sako, N., Eishima, T., Ito, T., Arikawa, Y., Miyamura, N., Kanairo, K., Ukawa, S., Ogasawara, S., Ishikawa, S. and Nakasuka, S., University of Tokyo's CubeSat "XI" as a Student-Built Educational Pico-Sateltdte -Final Design and Operation Plan-, The 23rd International Symposium of Space Technology and Science, 2002-f-13, Matsue, Japan, 2002.5.30. 2002
Tsuda, Y. and Nakasuka, S., Impulsive Optimal Guidance Algorithm for Formation Flying Spacecraft, The 23rd International Symposium of Space Technology and Science, 2002-d-51, 松江, 2002.5.31. 2002
Tsuda, Y. and Nakasuka, S., Optimum Guidance Law and Information Management for a Large Number of Formation Flying Spacecrafts, 53rd International Astronautical Congress, IAC-02-A.P.09, Houston, 2002.10.15. 2002
Tsuda, Y., Sako, S., Eishima, T., Ito, T., Arikawa, Y., Miyamura, N., Kanairo, K., Ukawa, S., Ogasawara, S., Ishikawa, S. and Nakasuka, S., Educational Pico-Sateltdte Project CubeSat –University of Tokyo’s CubeSat ‘’XI’’ and its operation Plan, 53rd International Astronautical Congress, IAC-02-P.1.02, Houston, 2002.10.14. 2002
Tsuda, Y. and Nakasuka, S., New Attitude Motion Following Control Algorithm for Capturing Tumbtdng Object in Space, The 51st International Astronautical Congress, IAF-00-A.2.05, Rio de Janeiro, 2000.10. 2001
Tsuda, Y., Sako, N., Eishima, T., Ito, T., Arikawa, Y., Miyamura, N., Tanaka, A. and Nakasuka S., University of Tokyo’s CubeSat Project – Its Educational and Technological Significance –, The 15th Annual AIAA/USU Conference on Small Sateltdtes, SSC01-VIIIb-7, Logan, Utah, 2001.8. 2001
Tsuda, Y. and Nakasuka, S., Real-Time Attitude Motion Synchronization Control with Torque Constraint for Capturing Tumbtdng Objects in Space, The 22nd International Symposium on Space Technology and Science, 2000-s-14, Morioka, Japan, 2000.5. 2000
Conference Proceedings (Japan)
Yuto Takei, Takanao Saiki, Yuya Mimasu, Naoko Ogawa, Roger Gutierrez-Ramon, Yuki Kubo, Maiko Yamakawa, Yuki Takao, Yusuke Maru, Satoshi Nonaka, Yuichi Tsuda, “The Deep Space Orbital Transfer Vehicle Concept Driven by Hayabusa2 Technology”, ISAS Planetary Exploration Workshop 2020, Sagamihara, Japan, 2020. 2020
Yuto Takei, Takanao Saiki, Yuya Mimasu, Naoko Ogawa, Yuichi Tsuda, “Deep Space Rendezvous-Docking Driven by Hayabusa2 Technology”, 30th Workshop on JAXA Astrodynamics and Flight Mechanics, Sagamihara, Japan, 2020. 2020
Gutierrez-Ramon, R., Liang, Y., Tsuda, Y., “Design of a Deep Space Orbit Transfer Vehicle (DS-OTV) Architecture”, 30th Workshop on JAXA Astrodynamics and Flight Mechanics, Sagamihara, Japan, 2020. 2020
Takao, Y., Mori, O., Matsushita, M., Okuizumi, N., Sato, Y., and Kawaguchi, J., “Solar Sail Membrane Shape Control Based on Modal Excitation: Theory and Experiment,” 30th Workshop on JAXA Astrodynamics and Flight Mechanics, Sagamihara, Japan, 2020. 2020
Takao, Y., Mori, O., Matsushita, M., Sugihara, A. K., and Kawaguchi, J., “Low-Thrust Trajectories of Small Spacecraft for Deep Space Exploration Using Solar Power Sail,” 29th Workshop on JAXA Astrodynamics and Flight Mechanics, Sagamihara, Japan, 2019. 2019
Takao, Y., Matsushita, M., Okuizumi, N., Sato, Y., Mori, O., and Kawaguchi, J., “Active Shape Control of Spinning Solar Sails by Exciting StaticWaves: Experimental Study Under Vacuum Environment,” 29th Workshop on JAXA Astrodynamics and Flight Mechanics, Sagamihara, Japan, 2019. 2019
高尾 勇輝, 森 治, 中条 俊大, 菊地 翔太, 癸生川陽子, 伊藤 元雄, 山田 和彦, 澤田 弘崇, 川崎 茂男, 松本 純, 柏岡 秀哉, 倉川 正也, 渡邉 元樹, 大橋郁,, 大木 優介, “OKEANOS のサンプルリターンミッション,” 第 62 回宇宙科学技術連合講演会, 久留米, 2018. 2018
高尾 勇輝, 森 治,, 川口 淳一郎, “太陽光圧を用いた構造共振によるスピン型宇宙膜面構造物のアクティブ 形状制御,” 第 62 回宇宙科学技術連合講演会, 久留米, 2018. 2018
Kashioka, S.; Ohira, G.; Takao, Y.; Kadokura, M.; Iyota, T. & Tsuda, Y., "小惑星形状の点群データを用いた自律誘導航法に関する研究", 第62回宇宙科学技術連合講演会, 日本航空宇宙学会, 2018 2018
Ohira, G.; Kashioka, S.; Takao, Y.; Kadokura, M.; Iyoda, T. & Tsuda, Y., "On-board Processing of Vector Code Correlation Algorithm for Image-based Navigation System", The 28th Workshop on JAXA Astrodynamics and Flight Mechanics, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS), , 2018 2018
柏岡, 秀哉 and 大平, 元希 and 高尾, 勇気 and 津田, 雄一, "Study of Estimation of the Position of the Spacecraft by Point Cloud Data" [第28回アストロダイナミクスシンポジウム講演後刷り集], 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS), 2018 2018
Takao, Y. and Mori, O., “Active Shape Control of Spinning Solar Sails Based on Self-Excited Oscillation,” 28th Workshop on JAXA Astrodynamics and Flight Mechanics, Sagamihara, Japan, 2018. 2018
Toshihiro, C.; Mori, O.; Matsumoto, J.; Saiki, T.; Kato, H.; Tsuda, Y.; Ogawa, N.; Mimasu, Y.; Kawaguchi, J.; Okuizumi, N.; Tanaka, K.; Terui, F.; Kawasaki, S.; Nishiyama, K.; Hosoda, S.; Yamada, K.; Okada, T.; Iwata, T.; Ralf, B.; Kikuchi, S.; Oki, Y.; Takao, Y. & Kashioka, S., "ソーラー電力セイルによる木星トロヤ群小惑星探査ミッションおよび探査機システム", Proceedings of the 18th Space Science Symposium, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS), 2018 2018
Takao, Y., Mimasu, Y., and Tsuda, Y., “Optical Navigation for Hayabusa2 Approaching Phase,” 28th Workshop on JAXA Astrodynamics and Flight Mechanics, Sagamihara, Japan, 2018. 2018
津田雄一,渡邊誠一郎,はやぶさ2プロジェクトチーム,小惑星探査機はやぶさ2: 運用状況及び小惑星近傍フェーズに向けた準備状況,第17回宇宙科学シンポジウム,S4-001,2017.1.6. 2017
Kashioka, S. & Tsuda, Y., "Precise SRP Torque Evaluation for Deep Space Navigation and Attitude Control Based on Non-Conventional Optical Reflectance Model" 第60回自動制御連合講演会, 2017 2017
高尾 勇輝, 森 治,, 川口 淳一郎, “柔軟性伸展ブームを用いた自律ドッキングのダイナミクスとその設計指 標,” 第 61 回宇宙科学技術連合講演会, 新潟, 2017. 2017
Matsumoto, J.; Okada, T.; Aoki, J.; Kawai, Y.; Okamoto, C.; Kebukawa, Y.; Ohtsuki, M.; Oki, Y.; Nakamura, T.; Kashioka, S.; Ito, M.; Yano, H. & Mori, O., "Solar Power Sail mission: Sampling and in-situ analysis", Proceedings of the 17th Space Science Symposium, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS), 2017. 2017
Nobukatsu, O.; Jun, M.; Osamu, M.; Hideki, K.; Koji, T.; Hiroyuki, T.; Satoshi, H.; Ken, G.; Yuichi, I.; Rikio, Y.; Shiro, K.; Michihiro, N.; Hiroshi, F.; Hiraku, S.; Saburo, M.; Miyazaki, Y.; Kazuya, S.; Ayako, K.; Kyoichi, N.; Toshihiro, C.; Yuki, T.; Shuya, K.; Takuma, N.; Motoki, W. & Masaya, K., "Current Status of the Development of Thin Film Solar Array Membrane Structure for Solar Power Sail Explorer", Proceedings of the 17th Space Science Symposium, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS), 2017. 2017
Takao, Y., Mori, O., and Kawaguchi, J., “Analysis of Spinning Solar Sail Missions Utilizing Active Shape Control,” 27th Workshop on JAXA Astrodynamics and Flight Mechanics, Sagamihara, Japan, 2017. 2017
柏岡, 秀哉 and 津田, 雄一, "光物理に忠実な太陽光圧モデル作成と姿勢制御に与える影響", [第27回アストロダイナミクスシンポジウム講演後刷り集], 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS), 2017 2017
Takao, Y., Mori, O., and Kawaguchi, J., “Autonomous Docking Dynamics with Flexible Extendible Booms,” 27th Workshop on JAXA Astrodynamics and Flight Mechanics, Sagamihara, Japan, 2017. 2017
高尾 勇輝, 川崎 繁男, 坂東 信尚, 中条 俊大, 菊地翔太, 池本 和晃, 北尾 啓, 加藤 秀樹,, 森 治, “木星トロ ヤ群探査機とそのサンプル採取機の自律ランデブードッキング及びサンプル受け渡し技術に関する検討,” 第 60 回宇宙科学技術連合講演会, 函館, 2016. 2016
Takao, Y., Chujo, T., and Kawaguchi, J., “Analytical Study of Vibration Mode and Forced Response of Spinning Large Membrane Space Structures,” 26th Workshop on JAXA Astrodynamics and Flight Mechanics, Sagamihara, Japan, 2016. 2016
Gutierrez-Ramon, R., Boden, R., Mori, O., and Kawaguchi, J., “Model for Touchdown Dynamics of a Lander on the Solar Power Sail Mission”, 26th Workshop on JAXA Astrodynamics and Flight Mechanics, Sagamihara, Japan, 2016. 2016
Takao, Y., Kawasaki, S., Chujo, T., Kikuchi, S., Ikemoto, K., Kitao, S., Kato, H., and Mori, O., “Analysis of Autonomous Rendezvous Docking and Sample Transfer Technology for a Space Probe in the Jupiter Trojan Region,” 26th Workshop on JAXA Astrodynamics and Flight Mechanics, Sagamihara, Japan, 2016. 2016
高尾 勇輝, 佐伯孝尚, 尾川順子, 照井冬人,, 津田雄一, “仮想的特徴点を用いた画像処理による小惑星探査 機の自己位置推定,” 第 47 期日本航空宇宙学会年会講演会, 東京, 2016. 2016
津田雄一,渡邊誠一郎,はやぶさ2プロジェクトチーム,小惑星探査機「はやぶさ2」の運用状況:巡航開始から地球スイングバイまで,第16回宇宙科学シンポジウム,S4-002,2016.1.6. 2016
Tsuda, Y., Robust Trajectory Design for Mars System Sample Return Mission(ロバスト性を考慮した火星圏サンプルリターンのための軌道設計),2016 ISAS Workshop on Astrodynamics and Flight Mechanics, B-2, Sagamihara, 2016.7.25. 2016
津田雄一,中澤暁,佐伯孝尚,渡邊誠一郎,小惑星探査機はやぶさ2のミッションと巡航運用状況, 第60回宇宙科学技術連合講演会, 1G06, 函館,2016.9.6. 2016
津田雄一,はやぶさからはやぶさ2へ:太陽系探査技術の進化,石油学会装置研究討論会,2016.12.8. 2016
Takao, Y., Saiki, T., Ogawa, N., Terui, F., and Tsuda, Y., “Estimation of the spacecraft position by applying Phase-Only Correlation to the images of the asteroid s surface,” 25th Workshop on JAXA Astrodynamics and Flight Mechanics, Sagamihara, Japan, 2015. 2015
津田雄一,重力天体探査の技術展望,第15回宇宙科学シンポジウム, S2-009,相模原,2015.1.6. 2015
谷本啓,武石直也,矢入健久,津田雄一,照井冬人,尾川順子,三桝裕也,観測画像列からの小惑星形状と相対運動の同時推定(英題:Simultaneous Estimation of Asteroid Shape and Motion),The 27th Annual Conference of Japanese Society for Artificial Inteltdgence, 1G4-2, 2013. 2013
Tsuda, Y., Kikuchi, S., Marco, G., A Study on Quasi-Periodic Orbits around Small Body for Hayabusa-2 Mission, 23rd Workshop on Astrodynamics and Flight Mechanics, B-16, Sagamihara, 2013.7.30. 2013
津田雄一,國中均,稲場典康,吉川真,倉岡今朝年,南野浩之,中澤暁,櫛木賢一,今村裕志,安部正真,渡邊誠一郎, 小惑星探査機はやぶさ2の開発状況, 第57回宇宙科学技術連合講演会, 1C03, 米子, 2013.10.9. 2013
津田雄一,佐伯孝尚,尾川順子,森本睦子,はやぶさ2の軌道設計,第55回宇宙科学技術連合講演会,1D03,2011.11.30,松山. 2012
津田雄一,「はやぶさ2」のシステム, 第12回宇宙科学シンポジウム,S1-06,2012.1.5,相模原. 2012
Tsuda, Y., Sail Surface Design of Spinning Solar Sail Based on Attitude Dynamics, 22nd JAXA Workshop on Astrodynamics and Flight Mechanics, B-9, 2012.7.30, Sagamihara. 2012
津田雄一,はやぶさ2プロジェクトチーム,はやぶさ2のミッション解析とシステム設計,第56回宇宙科学技術連合講演会,3A02,2012.11.22,別府. 2012
津田雄一,太陽系探査の将来,第11回宇宙科学シンポジウム,S5-06,2011.1.5,相模原. 2011
Tsuda, Y., Ogawa, N., Morimoto, M., Kawaguchi, J., Trajectory Design of Hayabusa-2, JAXA Workshop on Astrodynamics and Flight Mechanics, A-5, 2011.7.26, Sagamihara. 2011
Tsuda, Y., Saiki, T., Funase, R., Mimasu, Y., Shirasawa, Y., Uo, T., Kawauchi, H., Ishibashi, S., Taniguchi, S., Attitude Determination and Control Operation of IKAROS in Initial On-Orbit Phase, JAXA Workshop on Astrodynamics and Flight Mechanics, A-5, 2010.7.26, Sagamihara. 2010
津田雄一,佐伯孝尚,船瀬龍,池田人,三桝裕也,白澤洋次,山口智宏,中宮賢樹,IKAROSにおける姿勢軌道ダイナミクス同定,第54回宇宙科学技術連合講演会,2S16,2010.11.18,静岡. 2010
津田雄一, 特殊環境下の誘導航法, ALL-JAXAシンポジウム, 筑波, 2009.6.24. 2009
Tsuda, Y., Relative Orbit Determination for Formation Flight Based on Unscented Transformation, JAXA Workshop on Astrodynamics and Flight Mechanics, A-12, 2009. 2009
Terui, F., Tsuda, Y., Ogawa, N., Mori, O, Funase, R., Ikeda, S., Guidance and Control of the Spacecraft to Coltdde with the Asteroid 1999JU3, JAXA Workshop on Astrodynamics and Flight Mechanics, C-15, 2009. 2009
津田雄一, ハミルトン系の構造を厳密に保存する軌道の状態遷移行列の計算法, 第53回宇宙科学技術連合講演会, 1I16, 2009.9.9, 京都. 2009
津田雄一, 山本高行, 有人月輸送システムの軌道計画, 宇宙輸送シンポジウム, Sagamihara, 2008.1.28-29. 2008
津田雄一, スピン型ソーラーセイルの姿勢安定性解析, ALL-JAXAシンポジウム, 2008.6.24-25, 相模原 2008
Tsuda, Y. and Matsumoto, M., Globally Optimum Formation Design Strategy for High-Eltdptic Formation Flying, The 17th JAXA Workshop on Astrodynamics and Flight Mechanics, B-17, July 23-24, 2007, Sagamihara. 2007
Tsuda, Y., Pretdminary Orbit Design of Jupiter System Tour for Jovian Magnetospheric Science Mission, The 17th JAXA Workshop on Astrodynamics and Flight Mechanics, C-8, Sagamihara, July 23-24, 2007, Sagamihara. 2007
Shirasawa, Y., Iwakura, A. and Tsuda, Y., Evaluation of the Attitude Control System Using Three Dimensional Reaction Wheel for Micro Sateltdtes, The 17th Workshop on Astrodynamics snd Flight Mechanics, A-19, Ssagamihara, Jul 24, 2007. 2007
Okada, S., Shirasawa, Y., Miwa, Y., Mori, O., Kawakatsu, Y., Tsuda, Y., Yamamoto, T., Funase, R. and Kawaguchi, J., Design of Attitude Control System for H2A piggyback Solar Sail Spacecraft, The 17th Workshop on Astrodynamics snd Flight Mechanics, A-8, Sagamihara, July 23, 2007. 2007
津田雄一, 大型柔軟薄膜を有するスピン型宇宙機の姿勢安定解析, 宇宙構造・材料シンポジウム, 26, 相模原, 2007.11.22. 2007
津田雄一, 中谷幸司, 森治, 佐伯孝尚, 山本高行, 川口淳一郎, 矢野創, 田中真, M-Vサブペイロードを利用したソーラー電力セイル実験小型衛星の開発, 第6回宇宙科学シンポジウム, 相模原, 2006.1. 2006
津田雄一,スピン型ソーラーセイルのダイナミクス解析 ,The 16th Workshop on Astrodynamics and Flight Mechanics, C-18, 相模原, 2006.8.2. 2006
中谷幸司,津田雄一,森治,山本高行,佐伯孝尚,川口 淳一郎,サブペイロード領域を利用したソーラー電力セイル実験とその解析, 第22回宇宙構造材料シンポジウム,Sesson3-9,相模原, 2006.12.1. 2006
津田雄一, 戸田智朗, 市川勉, 斎藤義文, SCOPEにおける編隊飛行のための測距システムと軌道設計, 15th ISAS Workshop on Astrodynamics and Flight Mechanics, C-22, 2005.7. 2005
津田雄一, 森治, 改良多粒子系モデルによるソーラーセイル膜の挙動解析, 15th ISAS Workshop on Astrodynamics and Flight Mechanics, B-3, 2005.7. 2005
西山和孝, 津田雄一, 森治,はやぶさの巡航時運用, 14th ISAS Workshop on Astrodynamics and Flight Mechanics, pp.381-386, 2004.7. 2004
津田雄一, 任意形状に対応した多粒子系モデルによる薄膜挙動解析手法について, The 14th Workshop on Astrodynamics and Flight Mechanics, A-2, 相模原, 2004.7.26. 2004
津田雄一,竹内伸介,森治,川口淳一郎,峯杉賢治,西村祐介,南川幸毅, 観測ロケットを用いたソーラーセール膜展開実験の飛翔結果について, 第48回宇宙科学技術連合講演会, 2C17, 2004.11.5, 福井. 2004
津田雄一, 市川勉, 戸田知朗, 前澤洌, 斎藤義文, SCOPEフォーメーションフライトミッションにおける相対軌道決定手法, 第5回計測自動制御学会システムインテグレーション部門講演会 (SI2004), 2004.12.18. 2004
津田雄一, 大規模フォーメーションフライトを実現する分散型情報アーキテクチャ, The 13th Workshop on Astrodynamics and Flight Mechanics, 相模原, 2003.7.24. 2003
津田雄一, 川口淳一郎, 村上誠典, l310ロケットによるソーラーセール展開実験とその運動解析, The 13th Workshop on Astrodynamics and Flight Mechanics, A-15, 相模原, 2003.7.24. 2003
津田雄一, 澤井秀次郎, 中須賀真一, 寺薗淳也, 実ミッションと宇宙工学教育の効果的な関係について, 第47回宇宙科学技術連合講演会, 2B7, 2003.11.18. 2003
津田雄一, 河原吉伸, 大規模フォーメーションフライトにおける誘導則の大域的最適化手法, 第47回宇宙科学技術連合講演会, 2H4, 2003.11.18. 2003
Tsuda, Y. and Nakasuka, S., Optimal Guidance Law for Stand-by Orbit Insertion for Formation Flying Spacecraft, The 12th ISAS Workshop on Astrodynamics and Flight Mechanics, A-4, 相模原, 2002.7.29 . 2002
津田雄一, 酒匂信匡, 永島隆, 金色一賢, 鵜川晋一, 中須賀真一, 東京大学CubeSat-Iの現状 –開発を終えて-, 2002年度日本機会学会年次大会, 3322, 東京, 2002.9.26. 2002
津田雄一, 酒匂信匡, 永島隆, 伊藤孝浩, 有川善久, 宮村典秀, 金色一賢, 桑田良昭, 鵜川晋一, 小笠原志朗, 村上誠典, 石川早苗, 中須賀真一, 東大CubeSatの意義と現状 ~地上試験と最終インテグレーション~, 第45回宇宙科学技術連合講演会, 01-3D6, 浜松, 2001.10.19. 2001
中須賀真一, 青木隆平, 津田雄一, 川勝康弘, 木下貴博, 長島隆一, 膜状太陽光発電システム(「ふろしき」)衛星を用いた宇宙機システムの概念検討, 平成10年度宇宙輸送シンポジウム, pp194-197, 相模原,1999.1. 1999
中須賀真一, 青木隆平, 津田雄一, 長島 隆一, 川勝 康弘, 佐藤正雄, 桐谷浩太郎, 谷沢一雄, 大面積膜状太陽電池によるエネルギー獲得 ~ふろしき衛星の提案~, 第18回宇宙エネルギーシンポジウム, 相模原,1999.2. 1999
Tsuda, Y., Fujiwara, T., Nakamura, T.,and Nakasuka, S., The Attitude Control for Motion Synchronization to Capture Free-Flying Object', Proceedings of the 8th ISAS Workshop on Astrodynamics and Flight Mechanics, pp348-354, 相模原,1998.7. 1998
Invited Talks / Keynote Lectures
津田雄一,はやぶさ2における宇宙工学の役割 6th UNISEC Takumi Conference, 2016.2.29. (Invited) 2016
津田雄一,小惑星探査機はやぶさ2の航法誘導技術と地球スイングバイ運用,第3回制御部門マルチシンポジウム(MSCS2016),名古屋・南山大学,2016.3.7.(Invited) 2016
津田雄一, はやぶさ2の技術と運用状況,日本航空宇宙学会北部支部講演会,札幌・北海道大学,2016.3.9. (Invited) 2016
Tsuda,. Y., Yoshikawa, M., Takanao, S., Watanabe, S., Hayabusa2 – Round Trip Exploration to Near-Earth Asteroid ‘Ryugu’, Misasa International Symposium 2016 (Frontiers in Earth and Planetary Materials Research, S4-01, Misasa, 2016.3.10. (Invited) 2016
津田雄一,小惑星探査機はやぶさ2のミッション・開発成果・初期運用状況,深宇宙探査学シンポジウム,柏,2015.3.10. (Invited) 2015
津田雄一,はやぶさ2の深宇宙航行技術,第132回日本航海学会春季講演会, 横浜,2015.5.29,(Keynote) 2015
津田雄一,小天体探査の工学的側面:はやぶさ2と将来計画(英題:Engineering Aspect of Small Body Exploration -Hayabusa2 and Future),日本地球惑星科学連合2013年大会(Japan Geoscience Union Meeting 2013), U07-11,幕張,2013.5.19.(Invited) 2013
Tsuda, Y., Mori, O., Funase, R., Sawada, H., Yamamoto, T., Saiki, T., Endo, T. and Kawaguchi, J., Flight Result of IKAROS Deep Space Solar Sail Demonstrator, 9th Low Cost Planetary Missions Conference, APL, Laurel, MD, USA, 2011.6.21. (Invited) 2011
Tsuda, Y., Mori, O., Funase, R., Sawada, H., Yamamoto, T., Saiki, T., Endo, T., Yonekura, K., Hoshino, H. and Kawaguchi, J., Achievement of IKAROS – Japanese Interplanetary Deep Space Solar Sail Demonstration Mission, 7th IAA Symposium on Reatdstic Near-Term Advanced Scientific Space Missions, Aosta, Italy, 2011.7.12. (Invited) 2011
Tsuda, Y., Mori, O., Funase, R., Saiki, T., Sawada, H., Yamamoto, T., Endo, T., Kawaguchi, J., Minamiono, H., Yonekura, K. and Hoshino, H., Initial Flight Result of IKAROS and Perspective to Future Deep Space Missions by Solar Power Sail Technology, European Planetary Science Conference, MT6, 2010.9.20, Rome. (Invited) 2010
Tsuda, Y., Hayabusa-2 Mission Design and System Engineering, Invited Talk, International Workshop on Small Body Exploration by Physical Interactions, 2009.10.20, Tokyo, Japan. (Invited) 2009
津田雄一, M-Vロケット・サブペイロードによる小型衛星打ち上げについて,日本機械学会2006年度年次大会,F07-3,熊本大学,2006.9.(Keynote) 2006

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