Abstract
We present discrete algorithms for in-flight identification, calibration and alignment of a low cost strap-down inertial navigation system with correction by signals from the Sun and magnetic sensors. Proposed algorithms are simulated through attitude dynamics of a small land-survey satellite.
| Original language | English |
|---|---|
| Pages (from-to) | 16-21 |
| Number of pages | 6 |
| Journal | IFAC-PapersOnLine |
| Volume | 48 |
| Issue number | 11 11 |
| DOIs | |
| Publication status | Published - 2015 |
Bibliographical note
Publisher Copyright:© 2015
Keywords
- attitude determination
- calibration
- identification
- mini-satellite
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