坂東 麻衣 (Mai Bando)
京都大学 宇宙総合学研究ユニット 特定助教
京都大学 宇宙総合学研究ユニット
〒611-0011 京都府宇治市五ヶ庄
宇治地区研究所本館南ブロック HS307
Tel: 0774-38-3848, Fax: 0774-31-8463
Journal Papers
Conference Papers
解説
外部資金
受賞
Journal Papers
Mai Bando and Akira Ichikawa, "Graphical Generation of Periodic Orbits of Tschauner-Hempel Equations," AIAA Journal of Guidance, Control, and Dynamics, (accepted)
Hiroshi Yamakawa and Shinji Hachiyama, and Mai Bando, "Attitude Dynamics of a Pendulum-Shaped Charged Satellite," Acta Astronautica, Vol. 70, January-February, pp. 77--84, 2012.
Mai Bando and Hiroshi Yamakawa, "Near-Earth Asteroid Flyby Survey Mission Using Solar Sailing Technology," Journal of Astronautical Sciences, (accepted)
Ryo Jifuku and Akira Ichikawa, and Mai Bando, "Satellite Formation by Pulse Control Along a Circular Orbit," AIAA Journal of Guidance, Control, and Dynamics, (accepted)
Mai Bando and Hiroshi Yamakawa, "Orbital Design for Multiple Flyby Missions," Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, Vol. 8, 2010. [Full text]
Mai Bando and Hiroshi Yamakawa, "A New Lambert Algorithm Using the Hamilton-Jacobi-Bellman Equations," AIAA Journal of Guidance, Control, and Dynamics, Vol. 33 No. 3, pp. 1000--1008, 2010. [Full text]
Mai Bando and Akira Ichikawa, "Periodic Orbits of Nonlinear Relative Dynamics along an Eccentric Orbit," AIAA Journal of Guidance, Control, and Dynamics, Vol. 33 No. 2, pp. 385--395, 2010. [Full text]
Mai Bando and Akira Ichikawa, "Satellite Formation and Reconfiguration with Restricted Control Interval," AIAA Journal of Guidance, Control, and Dynamics, Vol. 33, No. 2, pp. 607--615, 2010. [Full text]
Mai Bando and Akira Ichikawa, "Periodic Orbits of Nonlinear Relative Dynamics and Satellite Formation," AIAA Journal of Guidance, Control, and Dynamics, Vol. 32, No. 4, pp. 1200--1208, 2009. [Full text]
Mai Bando and Akira Ichikawa, "Adaptive Regulation of Nonlinear Systems by Output Feedback," Journal of Robotics and Mechatronics, Vol. 20, No. 5, pp. 719--725, 2008. [Abstract & Full text]
Mai Bando and Hiroaki Nakanishi, "A Stable Approach for Modular Learning and Its Application to Autonomous Aero-Robot," Journal of Robotics and Mechatronics, Vol. 18, No. 1, pp.44--50, 2006.[Abstract & Full text]
Conference Papers
Mai Bando, Koichi Osuka, Takao Fujii and Hiroshi Yamakawa, "Orbital Maintainance for Observation mission of Peanut-Shaped Asteroid," SICE Annual Conference, Tokyo, 2011. (to appear)
Mai Bando and Akira Ichikawa, "Formation Flying Along a Circular Orbit with Control Constraints," AIAA/AAS Astrodynamics Specialist Conference, Alaska, 2011.
Mai Bando and Hiroshi Yamakawa, "Optimal Trajectory Design for Asteroid Deflection Mission,"
27th International Symposium on Space Technology and Science, Okinawa, 2011.
Shinji Hachiyama, Mai Bando and Hiroshi Yamakawa, "Attitude Dynamics of a Pendulum-shape Charged Satellite Using Lorentz and Gravity Forces,'' 27th International Symposium on Space Technology and Science, Okinawa, 2011.
Mai Bando and Hiroshi Yamakawa, "Application of Global Solution of Hamilton-Jacobi Equations to Optimal Low-Thrust Multiple Rendezvous Problem," IAC, Prague, 2010.
Hiroshi Yamakawa and Mai Bando, "Attitude Dynamics of a Pendulum-Shaped Charged Satellite," IAC, Prague, 2010.
Hiroshi Yamakawa and Mai Bando, "Gravity-Coulomb Force Combined Three-Body Problem,"
IFAC Automatic Control in Aerospace, Nara, 2010.
Mai Bando and Akira Ichikawa, "Active Formation Along an Eccentric Orbit,"
IFAC Automatic Control in Aerospace, Nara, 2010.
Mai Bando and Hiroshi Yamakawa, "Low-Thrust Trajectory Optimization Using Second-Order Generating Functions,"
SICE Annual Conference, Taipei, 2010.
Mai Bando and Akira Ichikawa, "Formation Flying Along a Circular Orbit with Pulse Control,"
AIAA/AAS Astrodynamics Specialist Conference, Tronto, 2010.
Hiroshi Yamakawa, Mai Bando, Katsuyuki Yano and Shu Tsujii, "Spacecraft Relative Dynamics under the Infuluence of Geomagnetic Lorentz Force"
AIAA/AAS Astrodynamics Specialist Conference, Tronto, 2010.
Mai Bando and Hiroshi Yamakawa, "Near-Earth Asteroid Survey Mission Concept Using Solar Sailing Technology,"
12th International Space Conference of Pacific-basin Societies (ISCOPS), Montreal, 2010.
Mai Bando and Hiroshi Yamakawa, "Solution to Lambert's Problem Using Generalized Canonical Transformations,"
20TH AAS/AIAA Space Flight Mechanics Meeting, SanDiego, 2010.
Akira Ichikawa and Mai Bando, "Satellite Formation and Reconfiguration with Restricted Control Interval,"
The Seventh Asian Control Conference, HongKong, 2009.
Mai Bando and Akira Ichikawa, "From Elliptic Restricted Three-Body Problem to Tschauner-Hempel Equations:A Control Strategy Based on Circular Problems,"
AAS/AIAA Astrodynamics Specialist Conference, Pittsuburg, 2009.
Mai Bando and Hiroshi Yamakawa, "Orbital Design for Multiple Flyby Mission,"
27th International Symposium on Space Technology and Science, Tsukuba, 2009.
Hiroshi Yamakawa, Katsuyuki Yano and Mai Bando, "Spacecraft Formation Dynamics under the Influence of Geomagnetic Lorentz Force,"
27th International Symposium on Space Technology and Science, Tsukuba, 2009.
Mai Bando and Hiroshi Yamakawa, "A New Optimal Orbit Control for Two-Point Boundary-Value Problem Using Generating Functions,"
Advances in the Astronautical Sciences, Vol. 134, pp. 245-260, Savannah, 2009.
(presented at AAS/AIAA Space Flight Mechanics Meeting 2009)
Mai Bando and Akira Ichikawa, "Adaptive Output Regulation of Nonlinear Systems described by Multiple Linear Models," 9th IFAC Workshop on Adaptation and Learning in Control and Signal Processing (ALCOSP' 07), St.Petersburg, 2007.
Mai Bando and Akira Ichikawa, "Adaptive Output Regulation for Linear Systems,"
Proceedings of SICE-ICASE International Joint Conference 2006 (SICE-ICCAS2006)，pp.3217-3222, Pusan, 2006.
Mai Bando and Hiroaki Nakanishi, "Modular Learning Based on Lyapunov Design Method for Control System of Autonomous Robot," Proceedings of the IASTED International Conference on Artificial Intelligence and Applications, pp. 609--614, Innsbruck, 2005.
Mai Bando, Hiroaki Nakanishi and Koichi Inoue, "A Study on Designing Control System by Modular Learning,"
Proceedings of SICE Annual Conference 2004, pp. 1071-1074, Sapporo, 2004.
解説
坂東麻衣, ``惑星間航行・編隊飛行のための宇宙機軌道設計," ISASニュース, No. 351, pp. 1-3, 2010.
中西弘明, 坂東麻衣, 井上紘一, 佐藤彰, ``防災用インテジェントエアロロボットの研究開発," NPO 国際レスキューシステム研究機構季刊誌 Quaterly Report創刊号, pp. 14-23, 2005.
外部資金
科学研究費補助金
若手研究(B)
研究期間 ：平成２１年４月〜平成２３年３月
研究課題名：母関数を用いた宇宙機の非線形軌道最適化問題の効率解法
研究者代表者：坂東麻衣
研究助成金（直接経費）：2460千円 (1100千円)
特別研究員奨励費
研究期間 ：平成１８年４月〜平成２０年３月
研究課題名：環境適応型自律ロボットのシステム構成原理
研究者代表者：坂東麻衣
研究助成金（直接経費）：1900千円（1900千円）
受賞
財団法人宇宙科学振興会 宇宙科学奨励賞（2010年3月9日）
研究課題名：惑星間航行・地球周回編隊飛行のための最適軌道制御理論