Abstract
This paper aims a first order comparative study between two different attitude determination methods. Study is accomplished in terms of accuracy and time required for computation. A test case satellite is chosen. Gravity gradient torque is taken into consideration as an external moment. Earth oblateness J2 is taken. Sensors are magnetometer and Sun sensor.
Original language | English |
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Title of host publication | RAST 2013 - Proceedings of 6th International Conference on Recent Advances in Space Technologies |
Number of pages | 4 |
ISBN (Electronic) | 978-1-4673-6396-9 |
DOIs | |
Publication status | Published - 2013 |
Externally published | Yes |
Keywords
- small satellites
- TRIAD
- qmethod
- attitude determination