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The 15Th Workshop on JAXA Astrodynamics and Flight Mechanics PROGRAM 005 The 15th Workshop on JAXA Astrodynamics and Flight Mechanics Jul 25 – Jul 26, 2005 ISAS/JAXA Japan Institute of Space and Astronautical Science (ISAS)/ Japan Aerospace Exploration Agency(JAXA) Welcome to the 15th Workshop on JAXA Astrodynamics and Flight Mechanics Contents ------------------------------------------------------ Map Session Schedule Session Detail July 25, 2005 Registration Starts at 9:30 Conference Room A Conference Room B Conference Room C 「Design of Reference Lissajous 「Tether Controlled Deployment 「Attitude Control of Space Robot using Trajectories around the L2 Point in the Characteristics of Rotationally Skew Backstepping」 10:00 Sun-Earth System」 Fold Membrane for Spinning Solar Sail」 *T. Hashimoto, H. Fujii (Tokyo ~ *M. Utashima (JAXA) *H. Furuya, Y. Inoue (Tokyo Institute of Metropolitan Institute of Technology) 10:30 Technology) A－１ B－１ C－１ 「Low-Thrust Periodic Orbits in the 「Static Deployment Experiment of 「Considerations on Attitude Control of Restricted Three-Body Problem」 Large Membrane for Solar Sail Space Robot Using Manifolds」 10:30 *M. Morimoto (The Graduate Spacecraft」 *S. Hokamoto (Kyushu University) ~ University for Advanced Studies), *O. Mori (JAXA), T. Nakano, K. Tarao 11:00 H. Yamakawa, K. Uesugi (JAXA) (The University of Tokyo), T. Saiki, Y. Tsuda, J. Kawaguchi (JAXA) C－２ A－２ B－２ 「Design of Small Circular Halo Orbit 「Dynamics Analysis of Solar Sail 「Optimization of three axis control of 11:00 around L2」 Membrane Using Improved two wheel satellite with initial angular ~ *K. Tarao (The University Of Tokyo), J. Multi-Particle」 momentum」 11:30 Kawaguchi (JAXA) *Y. Tsuda, O. Mori (JAXA) *T. Endo (JAXA) A－３ B－３ C－３ 「Optimization of Trajectories between 「Solar Sail Navigation with the 「Attitude Control of Multibody Using the Earth to the L2 Point」 Generalized Sail Model」 Coning Effect」 11:30 *S. Aida (The University Of Tokyo), M. *Leonel Rios-Reyes、Daniel J. Scheeres *O. Mori (JAXA), K. Minamikawa (Tokai ~ Matsumoto, Y. Kawakatsu, J. （The University of Michigan） University), J. Kawaguchi (JAXA) 12:00 Kawaguchi (JAXA) A－４ B－４ C－４ 12:00 Lunch ~12:45 12:45 Film Break : ~ － ― ASTRO－Ｅ2 or「HAYABUSA」 13:30 「Orbital Dynamics of Solar Photon 「A Study on Rotation Representations」 「Motion Estimation of a Large Space 13:30 Thrusters」 *R. Hasegawa (Hasegawa Engineering Debris Object Using Image Data」 ~ *H. Yamakawa (JAXA） Office) *F. Terui, H. Kamimura, S. Nishida 14:00 (JAXA) A－５ B－５ C－５ Conference Room A Conference Room B Conference Room C 「Preliminary Analysis of Interplanetary 「Stability of Spinning Solar Sail-craft 「Angular Momentum Control of Transfer Trajectory Using Libration containing A Huge Membran」 Tumbling Spacecraft」 14:00 Points」 *T. Nakanoh (The University Of Tokyo), *S. Yoshikawa (Mitsubishi Electric Co.), ~ *M. Nakamiya (The Graduate O. Mori (JAXA) K. Yamada (Nagoya University) 14:30 University for Advanced Studies), H. Yamakawa (JAXA) A－６ B－６ C－６ 「Orbital maneuvers from the 「Application of Bionics to Imaging 「Distributed Angular Momentum Sun-Earth L2 point」 Sensor-Ⅲ」 Control of Space Robot for Capturing a 14:30 *M. Matsumoto, J. Kawaguchi (JAXA) *H. Koshiishi, M. Naka (AIDS), H. Tumbling Target」 ~ Kurosaki (JAXA), Y. Iwata (Fujitsu FIP), *T. Oki, Dimitrov Dimitar Nikolaev, K. 15:00 A. Uchiyama (Waseda University) Yoshida (Tohoku University) A－７ B－７ C－７ 15:00 Break ~15:15 「Practical Analytic Solution of Relative 「Report of the Spin Axis Control 「Impedance control for the free flying Motion between Formation Flying Experiment」 space robot in the target capture」 15:15 Satellites with Different Ballistic *T. Saiki (JAXA) *H. Nakanishi, K. Yoshida (Tohoku ~ Coefficients in Near-Circular Reference University) 15:45 Orbit」 *T. Yamamoto (JAXA） A－８ B－８ C－８ 「Control of Relative Position Change in 「Design and Functional Model of CMG 「Preliminary Flight Experiment of a Formation Flying」 System for Agile Attitude Maneuver of small-size Parafoil from a Balloon」 15:45 *K. Yamada (Nagoya University), S. 20kg-Class Microsatellite」 *K. Hiraki, Y. Mizuta, Y. Saito, M. Inoue ~ Yoshikawa, T. Shima (Mitsubishi *K. Omagari, T. Usuda, S. Matunaga (Kyushu Institute of Technology) 16:15 Electric Co.) (Tokyo Institute of Technology) A－９ B－９ C－９ 「Piecewise Linear-Quadratic Control 「Experimental and numerical study of 「Wheeled Rover Experiment by using for Clustering Spacecraft」 Fluid Wheel」 Lunar Simulant Terrain in Vaccum *H. Umehara (NICT) *M. Tochimoto (Keio University), A. Environment」 16:15 Iwakura (Tokai University) *K. Iizuka (The Graduate University for ~ Advanced Studies), H. Kanamori 16:45 (SHIMIZU Corporation), T. Kubota (JAXA) A－１０ B－１０ C－１０ 「Study on Formation Flight Control 「Grasping Control of 「Insect-like Rover for Space and Information Propagation Structure」 Grasping/Guiding-type Docking Exploration」 16:45 *T. Saiki (JAXA) Mechanism for Nano-Satellite」 *K. Senda, M. Kimura, K. Fushimi ~ *K. Ui (JAXA), S. Matsunaga (Tokyo ( Kanazawa University), T. Kubota 17:15 Institute of Technology) (JAXA) A－１１ B－１１ C－１１ 「 Formation Flight and Intelligent 「Dynamic Deployment of Solar Sail 「Stabilizing Nonlinear Control of Traffic System」 Membrane with Bending Stiffness」 Spacecraft at Capturing and Docking 17:15 *J. Kawaguchi (JAXA) * K. Nakaya, O. Mori, Y. Tsuda, T. Saiki, Phase」 ～ T. Yamamoto (JAXA) *A. Ito, Y. Ikeda, T. Kida, T. Nagashio 17:45 (The University of Electro-Communications) A－１１´ Ｂ－１１´ Ｃ－１１´ 18:00 ~ Small Party 19:00 July 26, 2005 Registration Starts at 9:30 Conference Room A Conference Room B Conference Room C 「Application of Ballistic Capture 「Ground Evaluation Experiment on 「Nonlinear Mapping of Gaussian State Trajectory for Jovian Outpost Vibration Estimation Algorithm of Uncertainties」 Establishment」 Flexible Space Structures using Image *Ryan S. Park, Daniel J. Scheeres（The 10:00 *Ridanto Eko Poetro、Hiroshi Sensors」 University of Michigan） ~ Hirayama、Tetsuo Yasaka（Kyushu *S. Mitani, H. Ueno, K. Inaba, M. Oda 10:30 University） (JAXA), Matthew D. Lichter、Steven Dubowsky(MIT) A－１２ B－１２ C－１２ 「Orbital Characteristics of Venus 「On-orbit Assembly of a Large Space 「Precise Orbit Determination of GPS Explorer PLANET-C」 Radio Telescope」 Satellites using Carrier Phase 10:30 *N.Ishii, H. Yamakawa (JAXA) *S. Nishida (JAXA), H. Hirabayashi, Measurements」 ~ (Rtsumeikan University), T. Yshikawa *T. Takasu, S. Kasai (Kasai Design 11:00 (JAXA) Office) A－１３ B－１３ C－１３ 「Orbit Design and Simulation for 「Conception of solar sail satellites for 「ppb-precision orbit determination of ASTROD I」 the detection of exoplanets」 LEOs from laser ranging and GPS *Xia Yan（Purple Mountain Observatory, ○Adam SAGLAM（University of Liège, tracking」 Chinese Academy of Sciences）, Tang LPAP） *T. Otsubo, T. Kubooka, T. Goto (NICT) 11:00 Chien -Jen（Department of Physics, ~ Tsing Hua University）, Ni Wei-Tou 11:30 (Purple Mountain Observatory, Chinese Academy of Sciences), Li Guang-Yu (Purple Mountain Observatory, Chinese Academy of Sciences） A－１４ B－１４ C－１４ 「EFFICIENT ORBIT INTEGRATION 「Modular SPS Concept using A 「Orbit estimation by using differenced BY MANIFOLD CORRECTION Numerical Simulator for Large Flexible radiometric data types」 11:30 METHOD」 Satellites」 *T. Ichikawa (JAXA) ~ *T. Fukushima(National Astronomical *K. Senda, T. Uwano (Kanazawa 12:00 Observatory of Japan) University), K. Hisaji, N. Kubota (Kawasaki Heavy Industries) A－１５ B－１５ C－１５ 12:00 Lunch ~12:45 12:45 Hayabusa Operation Room : Guided Tour ~13:30 「Autonomous Localization System of 「Dynamic analysis of tethered satellite 「A Basic Study on the Optimal Planetary Lander」 system equipped with a crawler mass」 Trajectory Control of a Dive and Ascent 13:30 *S. Higo (The University of Tokyo) * M. Ohta, (Tokyo Metropolitan Satellite」 ~ University), K. Nakanishi, H. Fujii, D. *Tianshuang Fu, F. Imado ( Shinshu 14:00 Sato (Tokyo Metropolitan Institute Of University) Technology), A－１６ B－１６ C－１６ Conference Room A Conference Room B Conference Room C 「HAYABUSA Orbit Determination 「On-ground experiment of foldaway 「Lateral and Directional Control of Analysis just before the Rendezvous with tape-tether deployment」 Winged Reentry Vehicles – Aileron 14:00 Itokawa」 *T. Watanabe, H. Fujii (Tokyo Adverse Roll and Yaw RCS Roll」 ~ *T. Ohnishi (Fujitsu Co Ltd), M. Metropolitan Institute Of Technology), T. *K. Yonemoto (Kyushu Institute of 14:30 Yoshikawa, T. Kato, T. Ichikawa (JAXA) Kusagaya, T. Kikuchi (Tokyo Technology) Metropolitan University) A－１７ B－１７ C－１７ 「Status Report on VLBI application for 「Dynamics and Control of Very Long 「Proposal of Real-Time Guidance Space Navigation for HAYABUSA」 Space Tether System」 Method on the Aerodynamic Ascent 14:30 *M. Sekido, R. Ichikawa, T. Kondo, H. *A. Watanabe, H. Fujii (Tokyo Path」 ~ Takeuchi, Y. Koyama, E. Kawai Metropolitan Institute Of Technology), T. *T. Yamamoto (JAXA) 15:00 (National Institute of Information and Ishikawa (JAXA) Communications Technology) etc A－１８ B－１８ C－１８ 15:00 Break ~15:15 「Perturbation Analysis of 「Precise Numerical Simulations of 「Analysis of Autonomous Optical Sun-Synchronous Orbit between Electrodynamic Tethers for Debris Guidance and Navigation strategy 15:15 Planets」 Removal」 during flyby」 ~ *S. Nishimaki, K. Kuroshima (The *S. Kawamoto, S. Ohkawa, S. Nishida *K. Tarao (The University Of Tokyo), O. 15:45 University Of Tokyo), T. Saiki, J. (JAXA) Mori, Y. Kawakatsu, J. Kawaguchi Kawaguchi (JAXA) (JAXA) A－１９ B－１９ C－１９ 「Eccentricity of an Asteroid’s Orbit for 「Liberation Control of an 「Feasibility Study for Precise Lunar the Minimum Fuel Exploration」 Electrodynamic Tethered System Landing via Monte Carlo Simulation」 *S. Ueno, T. Kobayashi, S. Koga through Electric Current Switching」 *Y. Hamada, T. Ninomiya, Y. Katayama, 15:45 (Yokohama Nat. University) *N. Takeichi (JAXA) Y. Shinomiya, K. Matsumoto, M. ~ Yamamoto, S. Sawai (JAXA), S. Ueno 16:15 (Yokohama National University), K. Hayashi (MSS) A－２０ B－２０ C－２０ 「Trajectory Analysis of Post-Hayabusa 「Ground Experiment on Formation 「Analysis of High-frequency Asteroid Explorer Mission」 Deployment of Spinning Tethered Oscillations on Infrared Astrometric 16:15 *Y. Kawakatsu, H. Yamakawa, M. Abe Formation Flying」 Nano-class Satellite, "Nano-JASMINE"」 ~ (JAXA) *K. Nakaya (JAXA), M. Iai S. *M.
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