Light Curve Approximation Using an Attitude Model of Solar Sail Spacecraft von Yoshimura, Yasuhiro, Matsushita, Yuri, Arakawa, Ryohei, Hanada, Toshiya

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Estimation of orbital parameters of broken-up objects from in-situ debris measurements von Kodama, Yutaka, Furumoto, Masahiro, Yoshimura, Yasuhiro, Fujita, Koki, Hanada, Toshiya

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Orbital objects detection algorithm using faint streaks von Tagawa, Makoto, Yanagisawa, Toshifumi, Kurosaki, Hirohisa, Oda, Hiroshi, Hanada, Toshiya

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Practical method to identify orbital anomaly as spacecraft breakup in the geostationary region von Uetsuhara, Masahiko, Hanada, Toshiya

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Effective Search Strategy Applicable for Breakup Fragments in the Geostationary Region von Hanada, Toshiya, Uetsuhara, Masahiko, Yanagisawa, Toshifumi, Kitazawa, Yukihito

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Establishment of debris index evaluation criteria and comparison of index effects von Harada, Ryusuke, Kawamoto, Satomi, Hanada, Toshiya

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An environmental estimation model for in-situ measurements of small space debris von Furumoto, Masahiro, Hanada, Toshiya

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Highly Flexible Design to Align Formation of Space Advertisement von Nakajima, Kenta, Yoshimura, Yasuhiro, Chen, Hongru, Hanada, Toshiya

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Formation keeping control for deorbiting an uncooperative satellite by laser ablation von Isobe, Shun, Yoshimura, Yasuhiro, Hanada, Toshiya, Itaya, Yuki, Fukushima, Tadanori

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Corrigendum to “Storm-time atmospheric density modeling using neural networks and its application in orbit propagation” [Adv. Space Res. 53 (2014) 558–567] von Chen, Hongru, Liu, Huixin, Hanada, Toshiya

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Earth Escape from a Sun-Earth Halo Orbit using Unstable Manifold and Lunar Swingbys von CHEN, Hongru, KAWAKATSU, Yasuhiro, HANADA, Toshiya

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Origin identification of sub-millimeter-sized debris from in-situ debris measurements von Tanahashi, Mahiro, Chen, Hongru, Yoshimura, Yasuhiro, Hanada, Toshiya

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Assessments of the impacts of orbital fragmentations using the Near-Earth Orbital Debris Environment Evolutionary Model (NEODEEM) von Harada, Ryusuke, Kawamoto, Satomi, Hanada, Toshiya

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Space solar power satellite for the Moon and Mars mission von Baraskar, Aditya, Yoshimura, Yasuhiro, Nagasaki, Shuji, Hanada, Toshiya

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Improved contactless attitude control law of uncooperative spacecraft by laser ablation von Hayashibara, Ai, Yoshimura, Yasuhiro, Hanada, Toshiya, Itaya, Yuki, Fujihara, Tomoaki, Fukushima, Tadanori

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Precise time estimation of on-orbit satellite fragmentations von Itaya, Yuki, Fujita, Koki, Hanada, Toshiya

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Less fuel strategies for space debris removal in Low Earth Orbit von Itaya, Yuki, Yoshimura, Yasuhiro, Hanada, Toshiya, Fukushima, Tadanori

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Adaptive relative orbit control considering laser ablation uncertainty von Isobe, Shun, Yoshimura, Yasuhiro, Hanada, Toshiya, Itaya, Yuki, Fukushima, Tadanori

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Nonlinear Model Predictive Detumbling of Small Satellites with a Single-Axis Magnetorquer von Kondo, Kota, Kolmanovsky, Ilya, Yoshimura, Yasuhiro, Bando, Mai, Nagasaki, Shuji, Hanada, Toshiya

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Estimation of Orbital Parameters of Broken-Up Objects From In-Situ Debris Measurements von Hanada, Toshiya, Fujita, Koki, Yoshimura, Yasuhiro

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