Attitude control of magnetically actuated satellites using optimisation
The work in this thesis investigates the development of novel attitude control laws for satellites with magnetic actuators. Three different control approaches are presented, with a focus on both theoretical study and practical application. The first control approach studies the classical 'torqu...
Saved in:
| Main Author: | |
|---|---|
| Format: | Default Thesis |
| Published: |
2009
|
| Subjects: | |
| Online Access: | https://hdl.handle.net/2134/35959 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|