10:45
|
11:00
10:45 - 11:00
Paper No. 0101
Ting-Lun Wang, NCKU
Design of a Satellite Attitude Control System with Control Moment Gyroscopes
11:00
|
11:15
11:00 - 11:15
Paper No. 0028
Chung-Chun Ma, NCREE
DYNAMIC MODELING AND ATTITUDE CONTROL OF SINGLE-WINGED DUAL-AXIS SOLAR PANEL SATELLITE
11:15
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11:30
11:15 - 11:30
Paper No. 0002
Yu-Hsiu Lee, National Taiwan University
Presenter:Chun-Yuan Hsueh
Control-Oriented Modelling Techniques of Actuated Double-Wing Satellites
11:30
|
11:45
11:30 - 11:45
Paper No. 0047
Chih Yu Chien, National Yang Ming Chiao Tung University
Active Compensation for the Moment of Inertia of the CubeSat Attitude Control System Test Facility
11:45
|
12:00
11:45 - 12:00
Paper No. 0117
Thomas Yen, Tensor Tech
Control Moment Gyroscopes for Small Satellites - Pros & Cons