Abstract
An extended Kalman filtering technique for the large angular maneuvering and normal mode attitude determination of a satellite is presented by using gyro, sun sensors and infrared horizon scanners. The attitude quaternion representation is adapted to design an attitude estimator and integration linear error equations are established. The results of the simulation show that attitude determination is accurately achieved by using the attitude determination algorithm.
| Original language | English |
|---|---|
| Title of host publication | Proceedings of the 2004 Chinese Control and Decision Conference (16th CDC) |
| Editors | J.-Y. Yang, H.-W. Cao, J.-L. Li, Y.-H. Sun, Y.-Q. Chang |
| Pages | 295-298 |
| Number of pages | 4 |
| Publication status | Published - 2004 |
| Event | Proceedings of the 2004 Chinese Control and Decision Conference (16thCDC) - Huangshan, China Duration: 29 May 2004 → 1 Jun 2004 |
Publication series
| Name | Proceedings of the 2004 Chinese Control and Decision Conference (16thCDC) |
|---|
Conference
| Conference | Proceedings of the 2004 Chinese Control and Decision Conference (16thCDC) |
|---|---|
| Country/Territory | China |
| City | Huangshan |
| Period | 29/05/04 → 1/06/04 |
Keywords
- Attitude determination
- Attitude quaternion
- Extended Kalman filtering
- Satellite
Fingerprint
Dive into the research topics of 'Attitude determination of extended Kalman filtering based on quaternion'. Together they form a unique fingerprint.Cite this
Li, J. I., Liu, X. D., Zhang, Y. H., & Xiu, C. B. (2004). Attitude determination of extended Kalman filtering based on quaternion. In J.-Y. Yang, H.-W. Cao, J.-L. Li, Y.-H. Sun, & Y.-Q. Chang (Eds.), Proceedings of the 2004 Chinese Control and Decision Conference (16th CDC) (pp. 295-298). (Proceedings of the 2004 Chinese Control and Decision Conference (16thCDC)).