Development and attitude control of a 3-axis satellite platform using redundant reaction wheel system | |
| Author | Phawaphol Udompitayatorn |
| Call Number | AIT Thesis no.ISE-19-36 |
| Subject(s) | Control Systems Automation Mechatronics |
| Note | A thesis submitted in partial fulfillment of the requirements for the degree of Master of Engineering in Mechatronics, School of Engineering and Technology |
| Publisher | Asian Institute of Technology |
| Series Statement | |
| Abstract | The control system is an important part of a spacecraft mission. The control system keeps the body in the desired attitude and designed orbit, which both of the requirements are designed by control engineers for the control missions. For attitude control, most of them investigate the satellite behaviors based on simulation. If the attitude control system can be investigated via the real experiment, some problem which does not occur in the simulation is possible to occur. In this project, the testing platform and the attitude controller were made. However, the experiments were conducted on a terrestrial condition in which the gravity effects were inevitably included, creating the constant distribution torque. As a result, the saturation limitation handler was developed to cope with the fore-mentioned problem. |
| Year | 2019 |
| Corresponding Series Added Entry | |
| Type | Thesis |
| School | School of Engineering and Technology (SET) |
| Department | Department of Industrial Systems Engineering (DISE) |
| Academic Program/FoS | Industrial Systems Engineering (ISE) |
| Chairperson(s) | Manukid Parnichkun; |
| Examination Committee(s) | Abeykoon, A. M. Harsha S. ;Nakamura, Tai ; |
| Scholarship Donor(s) | Royal Thai Government;Asian Institute of Technology Fellowship; |
| Degree | Thesis (M. Eng.) -- Asian Institute of Technology, 2019 |