Attitude determination system for nano-satelite
The thesis focuses on the attitude determination system of a satellite. Attitude determination is the process of computing the spacecraft orientation relative to inertial reference frame such as the Earth center inertial frame. The attitude determination process is critical in satellite operation...
Saved in:
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Theses and Dissertations |
| Language: | English |
| Published: |
2014
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/10356/60707 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| Institution: | Nanyang Technological University |
| Language: | English |
| Summary: | The thesis focuses on the attitude determination system of a satellite. Attitude determination is the
process of computing the spacecraft orientation relative to inertial reference frame such as the Earth
center inertial frame. The attitude determination process is critical in satellite operation as it is
required to control the satellite attitude in a specified direction. |
|---|