Member

Course Name Research theme
D2 Hiroshi Fukumoto Optimal formation guidance of aircraft
D2 Nobutaka Kobayashi Adaptive control for re-entry vehicle
D1 Sachiko Fukushima Optimal air traffic management
M2 Fuka Amano Low noise guidance of arrival aircraft
M2 Kohei Arai Guidance and control of small VTOL
M2 Shunsuke Kuroda Capturing simulation of super multi-link debris capture
M2 Katsuya Saiki Cooperative control of multi-rotor under dynamic constraint
M2 Kazuho Sato Abort guidance of re-entry vehicle
M2 Toshiki Tamura Flight test bed experience for lunar explorer
M2 Wataru Nakayasu Terminal guidance of lunar explorer
M2 Takahiro Yamamoto Development of multi-rotor with wind resistance ability
M2 Tsubasa Yokoyama Development of multi-rotor for ocean activities
M2 Yoshifumi Naka Optimal time attitude control of CMGs
M2 Josui Ando Uncertainty quantification analysis of a wing flutter
M2 Kao Ito Wake flow of atmospheric-entry capsule to deploy a parachute
M2 Akira Katayama Study on robust pressure sensitive paints against spray conditions
M2 Keisuke Taniichi Dynamic stability analysis by a time-spectral CFD
M1 Yoshinori Asada Cooperative control for unmanned observation vehicles
M1 Yuta Kimura Guidance and control of lunar explorer
M1 Shohei Koyama Formation control using polar characterics
M1 Takumi Hoshi Development of attitude control system for multi-rotors
M1 Ryota Suzuki Optimal air traffic management
M1 Chiharu Niwa Development of multi-rotor for flying test bed
M1 Fumiya Dounoshita Shock capturing method for a high-order CFD
B4 Manami Kitahara Guidance and control of lunar explorer
B4 Fuminao Nagasaki Recovery control from stall condition of aircraft
B4 Takuma Miyazaki Optimal air traffic management
B4 Ryuki Otani Guidance and control of lunar explorer
B4 Naoki Kuwahara Guidance and control of debris capture
B4 Kenta Sugauchi Guidance and control of small VTOL
B4 Masato Kim Oct-tree grid divisions towards versatile CFD
B4 Koki Masaoka Aerodynamics of an experimental vehicle for a supersonic engine
B4 Takara Watanabe Transonic LES analysis by a high-order CFD method