| Mission report on the solar power sail deployment demonstration of IKAROS H Sawada, O Mori, N Okuizumi, Y Shirasawa, Y Miyazaki, M Natori, ... 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials …, 2011 | 97 | 2011 |
| Development of a smart reconfigurable reflector prototype for an extremely high-frequency antenna T Hiroaki, H Sakamoto, A Inagaki, K Ishimura, A Doi, Y Kono, T Oyama, ... Journal of Intelligent Material Systems and Structures 27 (6), 764-773, 2016 | 58 | 2016 |
| Significance of 3U CubeSat OrigamiSat-1 for space demonstration of multifunctional deployable membrane K Ikeya, H Sakamoto, H Nakanishi, H Furuya, T Tomura, R Ide, R Iijima, ... Acta Astronautica 173, 363-377, 2020 | 56 | 2020 |
| Feasibility study on a strain based deflection monitoring system for wind turbine blades K Lee, A Aihara, G Puntsagdash, T Kawaguchi, H Sakamoto, M Okuma Mechanical Systems and Signal Processing 82, 117-129, 2017 | 50 | 2017 |
| Development of deployment system for small size solar sail mission O Mori, H Sawada, F Hanaoka, J Kawaguchi, Y Shirasawa, M Sugita, ... Transactions of the Japan Society for Aeronautical and Space Sciences, Space …, 2009 | 48 | 2009 |
| Analysis of Membrane Dynamics using Multi-Particle Model for Solar Sail Demonstrator" IKAROS" Y Shirasawa, O Mori, Y Miyazaki, H Sakamoto, M Hasome, N Okuizumi, ... 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials …, 2011 | 43 | 2011 |
| Conceptual model study using origami for membrane space structures MC Natori, N Katsumata, H Yamakawa, H Sakamoto, N Kishimoto International Design Engineering Technical Conferences and Computers and …, 2013 | 39 | 2013 |
| Finite element modeling of sail deformation under solar radiation pressure H Sakamoto, Y Miyazaki, KC Park Journal of Spacecraft and Rockets 44 (3), 514-521, 2007 | 38 | 2007 |
| Conceptual model study using origami for membrane space structures-a perspective of origami-based engineering MC Natori, H Sakamoto, N Katsumata, H Yamakawa, N Kishimoto Mechanical Engineering Reviews 2 (1), 14-00368-14-00368, 2015 | 37 | 2015 |
| Folding patterns of planar gossamer space structures consisting of membranes and booms H Sakamoto, MC Natori, S Kadonishi, Y Satou, Y Shirasawa, N Okuizumi, ... Acta Astronautica 94 (1), 34-41, 2014 | 36 | 2014 |
| Conserving Finite Element Dynamics of Gossamer Structure and Its Application to Spinning Solar Sail" IKAROS" Y Miyazaki, Y Shirasawa, O Mori, H Sawada, N Okuizumi, H Sakamoto, ... 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials …, 2011 | 35 | 2011 |
| Dynamic wrinkle reduction strategies for cable-suspended membrane structures H Sakamoto, KC Park, Y Miyazaki Journal of spacecraft and rockets 42 (5), 850-858, 2005 | 32 | 2005 |
| Evaluation of membrane dynamics of IKAROS based on flight result and simulation using multi-particle model Y Shirasawa, O Mori, Y Miyazaki, H Sakamoto, M Hasome, N Okuizumi, ... Transactions of the Japan Society for Aeronautical and Space Sciences …, 2012 | 29 | 2012 |
| Transient dynamic analysis of gossamer-appendage deployment using nonlinear finite element method H Sakamoto, Y Miyazaki, O Mori Journal of Spacecraft and Rockets 48 (5), 881-890, 2011 | 25 | 2011 |
| Deployment and steering dynamics of spinning solar sail" IKAROS" O Mori, Y Shirasawa, Y Miyazaki, H Sakamoto, M Hasome, N Okuizumi, ... Journal of Aerospace Engineering, Sciences and Applications 4 (4), 79-96, 2012 | 21 | 2012 |
| A balloon-borne very long baseline interferometry experiment in the stratosphere: Systems design and developments A Doi, Y Kono, K Kimura, S Nakahara, T Oyama, N Okada, Y Satou, ... Advances in Space Research 63 (1), 779-793, 2019 | 19 | 2019 |
| Deformation properties of solar sail IKAROS membrane with nonlinear finite element analyses Y Satou, O Mori, N Okuizumi, Y Shirasawa, H Furuya, H Sakamoto 2nd AIAA Spacecraft Structures Conference, 0436, 2015 | 19 | 2015 |
| Evaluation of membrane structure designs using boundary web cables for uniform tensioning H Sakamoto, KC Park, Y Miyazaki Acta Astronautica 60 (10-11), 846-857, 2007 | 19 | 2007 |
| Development of nano-satellite OrigamiSat-1 with highly functional deployable membrane H Nakanishi, H Sakamoto, H Furuya, M Yamazaki, Y Miyazaki, ... 4th International Symposium on Solar Sailing, 2-5, 2017 | 18 | 2017 |
| Distributed and localized active vibration isolation in membrane structures H Sakamoto, KC Park, Y Miyazaki Journal of spacecraft and rockets 43 (5), 1107-1116, 2006 | 18 | 2006 |
Hiroshi FuruyaProfessor, Tokoyo Insititute of Technology在 enveng.titech.ac.jp 的电子邮件经过验证
