STUDI STEERING ALGORITHM UNTUK SINGLE GIMBAL CONTROL MOMENT GYRO (SGCMG) PADA PENGENDALIAN SIKAP SATELIT
Control Moment Gyro (CMG) is a type Attitude Control System (ACS), a system used to change the attitude of satellite along its orbit. CMG generates required gyroscopic torque by spinning a number of rotors, and directs the torque by changing the orientation of those rotors using gimbals. CMG is capa...
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| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/33657 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |