Reviewed Papers

2022
(97) Kojima, H., Keshtkar, S., Baba, F., Kato, Y., Suzukia, H., Kosuge, K.: Design, development and experiment of a novel tether-net release mechanism(to submit)

(96) Trivailo, P. M. and Kojima, H.: Analysis of Dynamic Stresses in the Elastic Nets for Space Debris Capture(submitted)

(95) Kawamoto, R., Kojima, H., Keshtkar, S.: Inverse-Kinematics Steering Law for Double Gimbal Scissored-Pair Control Moment Gyros (submitted).

(94) Endo, Y., Kojima, H., Trivailo, P. M.: New Formulation for Evaluating Status of Space Debris Capture using Tether-net(to be resubmitted).

(93) Kojima, H.: Backstepping-based Steering Control Law for Underactuated Spacecraft Attitude Control Using Two-skewed CMG(submitted)

(92) Trivailo, P. M. and Kojima, H.:Inertial Morphing as a Novel Concept in Attitude Control and Design of Variable Agility Acrobatic Autonomous Spacecraft, Nonlinear Approaches in Engineering Application, pp 119-211;244 (2022).

2021
(91) Kojima, H., Nakamura, R., Keshtkar, S.: Model Predictive Steering Control Law for Double Gimbal Scissored-Pair Control Moment Gyros, Acta Astronautica, Vol.183, pp.273-285(2021).

(90) Kojima, H., Okawara, T., Trivalio, P. M.: Ellipse Detection-based Visual Servo Control for Capturing Upper-Stage Rocket Body, Acta Astronautica, Vol.182, pp.295-309 (2021).

2020
(89) Kojima, H., Nakamura, R., and Keshtkar, S: Steering Control Law for Double-gimbal Scissored-pair CMG, Advances in Space Research, Vol.66, No.4, pp.771-784 (2020).

(88) Endo, Y. Kojima, H., and Trivailo, P. M.: Study on Acceptable Offsets of Ejected Nets from Debris Center for Successful Capture of Debris, Advances in Space Research, Vol.66, No.2, pp. 450-461 (2020).

(87) Hernandez-Maldonado, A., Diaz-Martinez, J.G., Kojima, H., Gutierrez-Carmona, I., Keshtkar, S.: Experimental Platform for Modeling and Control of Articulated Bodies. In: Hernandez E., Keshtkar S., Valdez S. (eds), Industrial and Robotic Systems. LASIRS 2019. Mechanisms and Machine Science, Vol.86. pp. 159-169 (2020), Springer, Cham.

(86) Trivailo, P. M. and Kojima, H.: Enhancement of the Attitude Dynamics Capabilities of the Spinning Spacecraft using Inertial Morphing, The Aeronautical Journal, Vol.124, No.1276, pp. 838-871 (2020). .

2019
(85) Kojima, H. and Trivailo, P. M.: Model Predictive Tether-deployment Control for Precise Landing of Tethered Reentry Body, Advances in Space Research, Vol.64, No.8, pp.1537-1548 (2019).

(84) Kojima, H. and Trivailo, P. M.: Adaptive Time-delay Estimated Sliding-Mode Control for a Bias Momentum Satellite with Two Reaction Wheels, Transactions of JSASS, Vol.62, No.4, pp.236-245(2019)

(83) Tamakoshi, D., and Kojima, H.: Set-oriented Design of Interplanetary Low-thrust Trajectories Using Earth Gravity Assist, Acta Astronautica, Vol.156, pp.208-218(2019).

(82) Trivailo, P. M. and Kojima, H.: Discovering Method of Control of the "Dzhanibekov's Effect" and Proposing its Application for the Possible Future Space Missions, Transactions of JSASS, Aerospace Technology Japan, Vol.17, No.1, pp.72-81(2019).

2018
(81) Kojima, H., Trivailo, P. M., Watanabe, T., and Fujii, H.A.: Numerical Simulation of Tape Tether Deployment from a Storage Container, Transactions of JSASS, Aerospace Technology Japan,Vol.16, No.7, pp.604-612(2018).

(80) Keshtkar, S., Moreno, J. A., Kojima, H., and Hernández E.: Design Concept and Development of a New Spherical Attitude Stabilizer for Small Satellites, IEEE ACCESS, Vol.6, No.1, pp.57353-57365 (2018).

(79) Kuga, T. and Kojima, H.: Self-Position Estimation using Terrain Shadows for Precise Planetary Landing, Acta Astronautica,Vol.148, pp.345-354(2018).

(78) Yoshimura, Y. and Kojima, H.: Optimization of Fault-Tolerant Thruster Configurations for Satellite Control, Advances in Space Research, Vol.61, No.6, pp.1617-1625(2018).

(77) Tamakoshi, D. and Kojima, H.: Solar Sail Orbital Control Using Reflectivity Variations near the Earth-Moon L2 Point, AIAA Journal of Guidance, Control and Dynamics,Vol.41, No.2, pp.417-430(2018).

(76) Kojima, H., Hiraiwa, K., and Yoshimura, Y.: Experimental Study on Line-of-Sight(LOS) Attitude Control Using Control Moment Gyros under Micro-Gravity Environment, Acta Astronautica, Vol.143, pp.118-125(2018).

(75) Keshtkar, S., Moreno, J. A., Kojima, H., Uchiyama, K., Nohmi, M., and Tamaya, K.: Spherial Gyroscopic Moment Stabilizer for Attitude Control of Micro-Satellite, Acta Astronautica, Vol.143, pp.9-15(2018).

(74) Keshtkar, N., Keshtkar, S., Moreno, J. A., Poznyak, A.S., Kojima, H.: LMI-Based Sliding Mode Control of an Underactuated Control Moment Gyroscope System, IFAC-PapersOnLine, Vol. 51, No. 13, pp.291-296, 2nd IFAC Conference on Modelling, Identification and Control of Nonlinear Systems, Guadalajara, Mexico, June 20-22(2018).

2017
(73) Ishikawa, S. and Kojima, H.: Optimal Oscillation Suppression Control for Tether Sling-Shot System, Transactions of JSASS, Aerospace Technology Japan, Vol.15(2017), pp.21-26.

(72) Kojima, H. and Trivailo, P. M.: Feature-based Visual Servo Control Preserving Wide-angle Properties of Super Wide-angle Lens, International Journal of Space Science and Engineering, Vol.4, No.4, pp. 309-329(2017).

2016
(71) Trivailo, P. M. and Kojima, H.: Dynamics of the Net Systems, Capturing Space Debris, Transactions of JSASS, Aerospace Technology Japan, Vol.14, No.ists30, pp.Pr_57-Pr_66(2016).

(70) Trivailo, P. M. and Kojima, H.: Launches and Captures of the Space Frisbees: Dynamics Modelling and Simulation, Transactions of JSASS, Aerospace Technology Japan,Vol.14, No.ists30, pp.Pd_133-Pd_142(2016).

(69) 久我共生, 小島広久, 福田 盛介: 小型月着陸機のための画像を用いた安全着陸領域識別に関する研究, 日本航空宇宙学会論文集,Vol.64, No.6, pp.303-309(2016).

(68) Kojima, H. and Taruoka, Y.: Deployment Control of a Tethered Satellite System for Rendezvous with a Target, Transactions of the Japan Society for Aeronautical and Space Sciences,Vol.59, No.6, pp.313-322(2016).

(67) Kojima, H., Trivailo, P.M. and Yoshimura, Y.: Spacecraft Line of Sight Maneuver Control Using Skew-arrayed Two Single-Gimbal Control Moment Gyros, Transactions of JSASS, Aerospace Technology Japan, Vol.14, No.ists30, pp.Pd_31-Pd_37 (2016).

(66) 青柳祐基, 小島広久: スピン安定型非対称宇宙機の最適2インパルス指向制御, 日本航空宇宙学会論文集, Vol.64, No.4, pp.208-213(2016).

(65) Kojima, H., Kunugi, K. and Trivailo, P. M. : Cluster Filtering/Control of Bending/Torsional Vibrations of a Tape Tether Using Smart-Film Sensors/Actuators, Elsevier Acta Astronautica,Vol.123, pp.213-226(2016).

2015
(64) Kojima, H. and Aoki, H.: Stabilisation of In-plane Periodic Motion of Electrodynamic Tether System by Combining Tether Length Control and Current Control, International Journal of Space Science and Engineering, Vol.3, No.4, pp.318-341(2015).

(63) Kasai, S. and Kojima, H.: LMI-based Control Law for Variable-Speed Control Moment Gyros in Flexible Spacecraft, International Journal of Space Science and Engineering, Vol.3, No.3, pp.246-278(2015).

(62) 鎌倉生大, 小島広久: 月・惑星着陸機のための着陸点決定法, 日本航空宇宙学会論文集, Vol.63, No.1, pp.13-19(2015).

(61) Kunugi, K., Kojima, H. and Trivailo, P. M.: Modeling of Tape Tether Vibration and Vibration Sensing Using Smart Film Sensors, Elsevier Acta Astronautica, Vol.107, pp.97-111(2015).

(60) Kojima, H., Fukatsu, K. and Trivailo, P. M.: Mission-Function Control of Tethered Satellite/Climber System, Elsevier Acta Astronautica, Vol.106, pp.24-32(2015).

2014
(59) Kojima, H.: Calculation and Fitting of Boundaries between Elliptic and Hyperbolic Singularities of Pyramid-type Control Moment Gyros, Elsevier Acta Astronautica, Vol.104, pp.33-44(2014).

(58) Kojima, H., Ieda, S., and Kasai, S.: Frequency-Tuning Input-Shaped Manifold-Based Switching Control for Underactuated Space Robot Equipped with Flexible Appendages, Elsevier Acta Astronautica, Vol.101, pp.42-54(2014).

(57) 笠井慎也,小島広久: 適応スキュー角ピラミッド型CMGに対するゲインスケジュールジンバル駆動則, 日本航空宇宙学会論文集, Vol.62, No.2, pp.55-62(2014).

2013
(56) Kojima, H.: Singularity Analysis and Steering Control Laws for Adaptive-skew Pyramid-type Control Moment Gyros, Elsevier Acta Astronautica, Vol.85, pp.120-137(2013).

(55) Kasai, S., Kojima, H., and Satoh, M.: Spacecraft Attitude Maneuver using Two Single-gimbal Control Moment Gyros, Elsevier, Acta Astronautica, Vol.84, pp.88-98(2013).

2012
(54) Watanabe, T., Fujii, A.H. Kusagaya, T., Sahara, H., Kojima, H., Takehara, S., Yamagiwa, Y., Sasaki, S., Abe, T., Tanaka, K., Oyama, K., Ebinuma, T., Johnson, L., Khazanov, G.V., Sanmartin, J.R., Charro, M., Kruijff, M., van der Heide, E.J., Rubin, B., Garcia de Quiros, F.J., Trivailo, P.M., and Williams, P.: T-REX: Bare Electro-Dynamic Tape-Tether Technology Experiment on Sounding Rocket S520, Journal of Space Technology and Science, Vol.26, No.1, pp.14-20(2012).

(53) Kasai, S. and Kojima, H.: Input-Shaped Link Motion Control of Planar Space Robot Equipped with Flexible Appendage, Transactions of the Japan Society for Aeronautical and Space Sciences, Vol.55, No.4. pp.205-213(2012).

(52) Kojima, H., Furukawa, Y. and Trivailo, P. M.: Experimental Study on Delayed Feedback Control for Libration of Tethered Satellite System, AIAA Journal of Guidance, Control, and Dynamics, Vol.35, No.3, pp.998-1002(2012).

(51) 渡部武夫, 藤井裕矩, 佐原宏典, 海老沼拓史, 小島広久: S520-25号機観測ロケット実験におけるベア導電テープテザー展開実験, 宇宙技術, Vol.11, pp.1-6(2012).

2011
(50) Kojima, H. and Kasahara, S.: An Adaptive Invariant Manifold-Based Switching Control for Planar Two-Link Space Robot, Transactions of the Japan Society for Aeronautical and Space Sciences, Vol.54, No.184, pp.144-152(2011).

(49) Kojima, H., Sugimoto, Y. and Furukawa, Y.: Experimental Study on Dynamics and Control of Tethered Satellite Systems with Climber, Elsevier Acta Astronautica, Vol.69, Nos.1-2, pp.96-108(2011).

(48) Kojima, H., Iwashima, H. and Trivailo, P. M.: Libration Synchronization Control of Clustered Electrodynamic Tether System Using Kuramoto Model, AIAA Journal of Guidance, Control, and Dynamics, Vol.34, No.3, pp.706-718(2011).

(47) Kojima, H., Furukawa, Y. and Trivailo, P. M.: Experimental Verification of Periodic Libration of Tethered Satellite System in Elliptic Orbit, AIAA Journal of Guidance, Control, and Dynamics, Vol.34, No.2. pp.614-618(2011).

(46) Nakanishi, T., Kojima, H. and Watanabe, T.: Trajectories of In-plane Periodic Solutions of Tethered Satellite System Projected on van der Pol Planes, Elsevier Acta Astronautica, Vol.68, Nos.7-8, pp1024-1030(2011).

2010
(45) Takada, K., Kojima, H. and Matsuda, N.: Control Moment Gyro Singularity-Avoidance Steering Control Based on Singular-Surface Cost Function, AIAA Journal of Guidance, Control, and Dynamics, Vol.33, No.5, pp.1442-1450(2010).

(44) 小島広久,笠原梓司: 平面2リンク宇宙ロボットに対する適応不変マニフォールドベースト切替制御(第2報:実験検証),日本航空宇宙学会論文集, Vol.58, No.679, pp.233-238(2010).

(43) トリバイロ・バベル,藤井裕矩,小島広久,渡部武夫: 3次元ロボットマニピュレータの多数制約最適制御,航空宇宙技術, Vol.9, pp.23-27(2010).

(42) Watanabe, T., Fujii, H. A., Kojima, H., Takikawa, H., Yukizane, M., and Ito, K.: Micro Gravity Experiment and 3 Dimensional Dynamic Analysis of Tethered Sampler, Transactions of Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, Vol.7, No.ists26, Pk_17-Pk_22(2009).

(41) Kojima, H., and Sugimoto, T.: Switching Delayed Feedback Control for an Electrodynamic Tether System in an Inclined Elliptic Orbit, Elsevier Acta Astronautica, Vol.66, Nos.7-8, pp.1072-1080(2010).

(40) Trivailo, P. M., Fujii, H. A., Kojima, H., and Watanabe, T.: Multi-Constrained Optimal Control of 3D Robot Arm Manipulator, Transactions of Japan Society for Aeronautical and Space Sciences, Space Technology Japan, Vol.7, No.ists26, Pd_95-Pd_104(2010).

2009
(39) 小島広久: 平面2リンク宇宙ロボットに対する適応不変マニフォールドベースト切替制御,日本航空宇宙学会論文集, Vol.57, No.669,pp.383-390(2009).

(38) Kojima, H., Matsuda, N., and Takada, K.: Adaptive Skewing Pyramid-type CMGs for Fast Attitude Maneuver, Transactions of the Japan Society for Aeronautical and Space Sciences, Space Technology Japan, Vol.7, pp.19-24(2009).

(37) Kojima, H., and Sugimoto,T.: Stability Analysis of In-plane and Out-of-plane Periodic Motions of Electrodynamic Tether System in Inclined Elliptic Orbit, Elsevier, Acta Astronautica, Vol.65, Nos.34, pp.477-488(2009).

(36) Takada, K., and Kojima, H.: Receding Horizon Control on Steering of Control Moment Gyro for Fast Attitude Maneuvers, Transactions of the Japan Society for Aeronautical and Space Sciences, Vol.52, No.175,pp.1-10(2009).

(35) Kojima, H., and Tomikawa, M.: Model Predictive Control for Deflection Limiting Maneuver of Flexible Structure, Transactions of the Japan Society for Aeronautical and Space Sciences, Vol.51, No.174, pp.267-274(2009).

(34) Fujii, H. A., Watanabe, T., Kojima, H., Oyama,K., Kusagaya, T., Yamagiwa, Y., Ohtsu, H., Cho, M., Sasaki, S., Tanaka, K., Williams, J., Binyamin, R., Les Johnson, C., Khazanov, G., Sanmartin, J.R., Lebreton, J-P., van der Heide, J.E., Kruijff, M., Pascal,F., and Trivailo, P.: Sounding rocket experiment of bare electrodynamic tether system, Elsevier, Acta Astronautica, Vol.64, Nos.2-3, pp.313-324(2009).

2008
(33) 小島広久,米川豊: 特徴ベースト視覚サーボにおける首ふり・後退量のファジィ決定,日本ロボット学会誌, Vol.26, No.3, pp.284-293(2008).

2007
(32) Kojima, H.: Stabilization of Angular Velocity of Asymmetrical Rigid Spacecraft Using Two Constant Torques, AIAA Journal of Guidance, Control, and Dynamics, Vol.30, No.4, pp.1163-1168(2007).

(31) Kojima, H., and Sugimoto,T.: Nonlinear Control of a Double Pendulum Electrodynamic Tether System, AIAA Journal of Spacecraft and Rockets, Vol.44, No.1, pp.280-284(2007).

(30) Kojima, H., Fujiki, T., and Fujii, H. A. :H∞ Compensated Minimum Bending Moment Control for Flexible Space Structures, Transactions of the Japan Society for Aeronautical and Space Sciences,Vol.49,No.166,pp.254-257(2007).

(29) Kojima, H., and Singhose, W.: Adaptive Deflection-Limiting Control for Slewing Flexible Space Structures, AIAA, Journal of Guidance, Control, and Dynamics, Vol.30, No.1,pp.61-67(2007).

(28) 高田尚,小島広久: 機能不全衛星の角運動量減衰のための自律学習型衝撃スラスト法,日本航空宇宙学会論文集, Vol.55, No.636,pp.27-33(2007).

2006
(27) 小島広久,青山修平:バーチャルストラクチャとバックステッピング法を用いた分散型フォーメーションフライト制御,日本機械学会論文集C編,Vol.72, No.723, pp.3533-3539(2006).

(26) Kusagaya, T., Kojima, H., Fujii, H. A.: Estimation of Flyable Regions for Planetary Airships, AIAA Journal of Aircraft,Vol.43,No.4, pp.1177-1181(2006).

(25) 今村俊介, 小島広久, 土屋武司, 久保田弘敏: Hybrid-GAを用いた二段式スペースプレーンの最適設計, 日本航空宇宙学会論文集, Vol.54, No.630,pp.279-287(2006).

(24) 小島広久,米川豊:中間画像を利用した特徴ベースト法,日本機械学会論文集C編,Vol.72, No.717, pp.1544-1551(2006).

(23)小島広久,瓜生研史:フォーメーションフライトにおける太陽輻射圧の利用,東京都立科学技術大学 紀要,Vol.19, pp.129-132(2006).

2005
(22) 渡部武夫,藤井裕矩,小島広久,William Singhose :エレクトロダイナミックテザー推進における電流入力整形, 日本航空宇宙学会論文集, Vol.53, No.623, pp.569-576(2005).

(21) 小島広久, 藤木尊明, 藤井裕矩 :柔軟宇宙構造物の最短時間スルーマヌーバに対するH∞トラッキング制御, 日本航空宇宙学会論文集, Vol.53, No.621, pp.482-489(2005).

(20) 小島広久: 厳密線形化された宇宙機の相対位置・姿勢運動に対する最小エネルギー制御,日本機械学会論文集(C)編, Vol.71, No.702, pp.462-468(2005).

(19) Kojima, H.:Fly-around Motion Control Based on Exact Linearization with Adaptive Law, AIAA, Journal of Guidance, Control, and Dynamics, Vol.28, No.1, pp.167-169(2005).

2004
(18) Kojima, H., and Nakajima, N.:Multi-Objective Trajectory Optimization by a Hierarchical Gradient Algorithm with Fuzzy Decision Logic, - Application to slew maneuver problems of a flexible space structure, Transactions of the Japan Society for Aeronautical and Space Sciences, Vol.47, No.155, pp.66-74(2004).

(17) Kojima, H., Iwasaki, M., Fujii, H. A., Blanksby, C. and Trivailo, P.: Nonlinear Control of Librational Motion of Tethered Satellites in Elliptic Orbits, AIAA, Journal of Guidance, Control, and Dynamics, Vol.27, No.2, pp.229-239(2004).

2003
(16) 小島広久,中嶋伸幸:ファジィ化階層勾配法による多目的軌道最適化,柔軟宇宙構造物のスルーマヌーバ問題への適用,日本航空宇宙学会論文集, Vol.51, No.598, pp.589-596(2003).

(15) Kojima, H:Target Capture via Sliding-Mode Control Incorporating a Reaction Control System, Transactions of the Japan Society for Aeronautical and Space Sciences,Vol.46, No.154, pp.133-142(2003).

(14) 小島広久,田中成和,藤井裕矩:柔軟宇宙構造物のスルーマヌーバにおける感度最小制御,日本機械学会論文集C編, Vol.69, No678, pp.396-401(2003).

(13) Fujii, H. A., Kojima, H., and Nakajima, N. : Slew Maneuver of a Flexible Space Structure with Constraint on Bending-Moment, AIAA, Journal of Guidance, Control, and Dynamics, Vol.26, No.2, pp.259-266(2003).

(12) Fujii, H. A., Kojima, H.:Optimal Trajectory Analysis for Deployment/Retrieval of Tethered Subsatellite using Metric, AIAA, Journal of Guidance, Control, and Dynamics, Vol.26, No.1, pp.177-179(2003).

2002
(11) 小島広久:柔軟付加物を有する二次元多剛体のオーダーnの定式化,Simulinkへの実装によるモデル変更作業の低減化,日本航空宇宙学会論文集,Vol.50, No.586, pp.466-473(2002).

(10) 小島広久,中嶋伸幸,藤井裕矩: 柔軟宇宙構造物のスルーマヌーバに対する最小曲げモーメント制御(階層勾配法による解析と実験的検証),日本航空宇宙学会論文集,Vol.50, No.585, pp.387-393(2002).

(9) 小島広久,向井拓幸: 平滑規範モデル適応スライディングモード制御によるターゲット衛星への姿勢追従,日本航空宇宙学会論文集,Vol.50, No.583, pp. 301-309(2002).

(8) 小島広久,江口幸弘: 楕円ポテンシャル場の局所最小点検出によるロボットの動作計画法,日本機械学会論文集C編, Vol.68, No.670, pp.1798-1804(2002).

(7) 小島広久: 重力傾斜安定化宇宙構造物に対する最短時間伸展制御,日本機械学会論文集C編,Vol.68, No.669, pp.1435-1440, (2002).

(6) 小島広久,向井拓幸:適応スライディングモード制御による姿勢追従マニューバ,日本機械学会論文集C編,Vol.68, No.668, pp.1113-1118(2002).

(5)
小島広久,荒井直広: 特徴ベースト視覚サーボに対するファジィ制御補償,日本機械学会論文集C編,Vol.68, No.668, pp.1119-1126(2002).

2001
(4) 小島広久: 姿勢変動と衝撃力の低減を目的としたエンドエフェクタ軌道の最適化, 日本航空宇宙学会論文集,Vol.49, No.566,pp.92-99(2001).

1996
(3) 鈴木真二,小島広久:速度不連続を伴う三次元多体剛体の運動解析(第3報),宇宙ロボットの物体捕獲問題,日本航空宇宙学会誌,Vol.44, No.514,pp.655-661(1996).

1994
(2) 鈴木真二,小島広久,松永大一郎: 速度不連続を伴う三次元多体剛体の運動解析(第2報)order-n の定式化の利用,日本航空宇宙学会誌,Vol.42, No.490, pp.686-691(1994).

(1) Suzuki, S. and Kojima, H. : Application of Order -n Formulation to Panel Deployment Problem of a Spacecraft, Journal of Guidance, Control, and Dynamics, Vol.17, No.3 pp.634-636(1994).

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