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 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 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
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
30 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 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 
Pavel M. TrivailoRMIT UniversityBestätigte E-Mail-Adresse bei rmit.edu.au
