@article{CTT100794155, author = {Ting Hao and Saburo Matunaga}, title = {Performance evaluation of robust attitude control system using control moment gyros for rapid multi-target observation}, journal = {International Journal of Applied Systemic Studies (IJASS)}, year = 2018, } @article{CTT100734387, author = {T. Hao and S. Matunaga}, title = {New Sliding Mode Control Approach for Rapid Attitude Maneuver using Control Moment Gyros}, journal = {Journal of Aerospace Engineering}, year = 2016, } @article{CTT100734388, author = {Ting HAO and Shota KAWAJIRI and Kyosuke TAWARA and Saburo MATUNAGA}, title = {A Practical Rapid Attitude Maneuver Control System using Control Moment Gyros for Microsatellite TSUBAME}, journal = {Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan}, year = 2015, } @misc{CTT100683758, author = {Ting Hao}, title = {A Study on Control Methods of Rapid Attitude Maneuver using Control Moment Gyros for Microsatellites}, year = 2015, } @misc{CTT100698481, author = {Ting Hao}, title = {A Study on Control Methods of Rapid Attitude Maneuver using Control Moment Gyros for Microsatellites}, year = 2015, } @misc{CTT100683759, author = {カクテイ}, title = {コントロールモーメントジャイロを用いた超小型衛星のための高速姿勢変更制御法に関する研究}, year = 2015, } @misc{CTT100683760, author = {Ting Hao}, title = {A Study on Control Methods of Rapid Attitude Maneuver using Control Moment Gyros for Microsatellites}, year = 2015, } @phdthesis{CTT100683758, author = {Ting Hao}, title = {A Study on Control Methods of Rapid Attitude Maneuver using Control Moment Gyros for Microsatellites}, school = {東京工業大学}, year = 2015, } @phdthesis{CTT100698481, author = {Ting Hao}, title = {A Study on Control Methods of Rapid Attitude Maneuver using Control Moment Gyros for Microsatellites}, school = {東京工業大学}, year = 2015, } @phdthesis{CTT100683759, author = {カクテイ}, title = {コントロールモーメントジャイロを用いた超小型衛星のための高速姿勢変更制御法に関する研究}, school = {東京工業大学}, year = 2015, } @phdthesis{CTT100683760, author = {Ting Hao}, title = {A Study on Control Methods of Rapid Attitude Maneuver using Control Moment Gyros for Microsatellites}, school = {東京工業大学}, year = 2015, }