Abstract
Contemporary land-survey micro-satellites have general mass up to 100 kg and are placed on the orbit altitudes from 600 up to 800 km. For such spacecraft some principle problems on attitude determination, in-flight calibration and alignment are considered and elaborated methods are presented for their solving. We present discrete algorithms for calibration and alignment of the low cost strap-down inertial navigation systems with correction by signals from multi-head Sun sensor, magnetic sensor and the GPS/GLONASS satellites.
| Original language | English |
|---|---|
| Title of host publication | 19th IFAC World Congress IFAC 2014, Proceedings |
| Editors | Edward Boje, Xiaohua Xia |
| Publisher | IFAC Secretariat |
| Pages | 7941-7946 |
| Number of pages | 6 |
| ISBN (Electronic) | 9783902823625 |
| DOIs | |
| Publication status | Published - 2014 |
| Event | 19th IFAC World Congress on International Federation of Automatic Control, IFAC 2014 - Cape Town, South Africa Duration: 24 Aug 2014 → 29 Aug 2014 |
Publication series
| Name | IFAC Proceedings Volumes (IFAC-PapersOnline) |
|---|---|
| Volume | 19 |
| ISSN (Print) | 1474-6670 |
Conference
| Conference | 19th IFAC World Congress on International Federation of Automatic Control, IFAC 2014 |
|---|---|
| Country/Territory | South Africa |
| City | Cape Town |
| Period | 24/08/14 → 29/08/14 |
Bibliographical note
Publisher Copyright:© IFAC.
Funding
★This work was supported by TUBITAK (The Scientific and Technological Research Council of Turkey, Grant 113E595), RFBR (Russian Foundation for Basic Research, Grant 14-08-91373), and also by Division on EMMCP of the RAS (Program 14)
| Funders | Funder number |
|---|---|
| TUBITAK | |
| Royal Astronomical Society | |
| Russian Foundation for Basic Research | 14-08-91373 |
| Türkiye Bilimsel ve Teknolojik Araştirma Kurumu | 113E595 |
Keywords
- Attitude determination
- In-flight calibration
- Spacecraft