Optimum spacecraft attitude control methods for a combined attitude and thermal control system
Spacecraft missions need efficient and precise attitude control systems. With the aim of reducing the vehicle volume and mass, and for a greater reliability, a system combining the conventional spacecraft attitude control and thermal control systems in a single system is proposed. The combined attit...
| Main Author: | |
|---|---|
| Format: | Thesis |
| Language: | English |
| Published: |
2011
|
| Subjects: | |
| Online Access: | http://psasir.upm.edu.my/id/eprint/41781/ http://psasir.upm.edu.my/id/eprint/41781/1/FK%202011%206R.pdf |