Control moment gyro singularity-avoidance steering control based on singular-surface cost function K Takada, H Kojima, N Matsuda Journal of guidance, control, and dynamics 33 (5), 1442-1450, 2010 | 60 | 2010 |
Nonlinear control of librational motion of tethered satellites in elliptic orbits H Kojima, M Iwasaki, HA Fujii, C Blanksby, P Trivailo Journal of Guidance, Control, and Dynamics 27 (2), 229-239, 2004 | 55 | 2004 |
Adaptive deflection-limiting control for slewing flexible space structures H Kojima, W Singhose Journal of guidance, control, and dynamics 30 (1), 61-67, 2007 | 54 | 2007 |
Experimental study on dynamics and control of tethered satellite systems with climber H Kojima, Y Sugimoto, Y Furukawa Acta Astronautica 69 (1-2), 96-108, 2011 | 49 | 2011 |
Sounding rocket experiment of bare electrodynamic tether system HA Fujii, T Watanabe, H Kojima, KI Oyama, T Kusagaya, Y Yamagiwa, ... Acta Astronautica 64 (2-3), 313-324, 2009 | 49 | 2009 |
Stability analysis of in-plane and out-of-plane periodic motions of electrodynamic tether system in inclined elliptic orbit H Kojima, T Sugimoto Acta Astronautica 65 (3-4), 477-488, 2009 | 48 | 2009 |
Spacecraft attitude maneuver using two single-gimbal control moment gyros S Kasai, H Kojima, M Satoh Acta Astronautica 84, 88-98, 2013 | 43 | 2013 |
Space demonstration of bare electrodynamic tape-tether technology on the sounding rocket S520-25 H Fujii, T Watanabe, H Sahara, H Kojima, S Takehara, Y Yamagiwa, ... AIAA Guidance, Navigation, and Control Conference, 6503, 2011 | 39 | 2011 |
Mission-function control of tethered satellite/climber system H Kojima, K Fukatsu, PM Trivailo Acta Astronautica 106, 24-32, 2015 | 33 | 2015 |
Study on acceptable offsets of ejected nets from debris center for successful capture of debris Y Endo, H Kojima, PM Trivailo Advances in Space Research 66 (2), 450-461, 2020 | 31 | 2020 |
Trajectories of in-plane periodic solutions of tethered satellite system projected on van der Pol planes K Nakanishi, H Kojima, T Watanabe Acta Astronautica 68 (7-8), 1024-1030, 2011 | 28 | 2011 |
Fly-around motion control based on exact linearization with adaptive law H Kojima Journal of Guidance, Control, and Dynamics 28 (1), 167-169, 2005 | 28 | 2005 |
Switching delayed feedback control for an electrodynamic tether system in an inclined elliptic orbit H Kojima, T Sugimoto Acta Astronautica 66 (7-8), 1072-1080, 2010 | 27 | 2010 |
Singularity analysis and steering control laws for adaptive-skew pyramid-type control moment gyros H Kojima Acta astronautica 85, 120-137, 2013 | 26 | 2013 |
Experimental verification of periodic libration of tethered satellite system in elliptic orbit H Kojima, Y Fukukawa, PM Trivailo Journal of Guidance, Control, and Dynamics 34 (2), 614-618, 2011 | 25 | 2011 |
Control of attitude and vibration of a tethered space solar power satellite H Fujii, T Watanabe, H Kojima, K Sekikawa, N Kobayashi AIAA Guidance, Navigation, and Control Conference and Exhibit, 5421, 2003 | 24 | 2003 |
Solar Sail Orbital Control Using Reflectivity Variations near the Earth–Moon Point D Tamakoshi, H Kojima Journal of Guidance, Control, and Dynamics 41 (2), 417-430, 2018 | 21 | 2018 |
Optimal trajectory analysis for deployment/retrieval of tethered subsatellite using metric HA Fujii, H Kojima Journal of guidance, control, and dynamics 26 (1), 177-179, 2003 | 21 | 2003 |
Experimental study on delayed feedback control for libration of tethered satellite system H Kojima, Y Furukawa, PM Trivailo Journal of guidance, control, and dynamics 35 (3), 998-1002, 2012 | 17 | 2012 |
Nonlinear control of a double pendulum electrodynamic tether system H Kojima, T Sugimoto Journal of Spacecraft and Rockets 44 (1), 280-284, 2007 | 17 | 2007 |