Abstract
In this paper, a satellite celestial navigation which estimates the satellite position on the orbit is proposed. It consists attitude sensor with star-tracker and earth sensor. The proposed algorithm is based on the theory that the position on the surface is determined in the case of having a different observation angle for each star at zenith. The performance of the proposed algorithm is examined via simulation considering error parameters of attitude sensor. The proposed satellite celestial navigation algorithm can estimate the satellite position on the orbit in real time, since it obtains the observation angle and altitude directly by using the attitude sensor.
| Original language | English |
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| Title of host publication | ICCAS 2015 - 2015 15th International Conference on Control, Automation and Systems, Proceedings |
| Publisher | Institute of Electrical and Electronics Engineers Inc. |
| Pages | 461-465 |
| Number of pages | 5 |
| ISBN (Electronic) | 9788993215090 |
| DOIs | |
| State | Published - 23 Dec 2015 |
| Event | 15th International Conference on Control, Automation and Systems, ICCAS 2015 - Busan, Korea, Republic of Duration: 13 Oct 2015 → 16 Oct 2015 |
Publication series
| Name | ICCAS 2015 - 2015 15th International Conference on Control, Automation and Systems, Proceedings |
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Conference
| Conference | 15th International Conference on Control, Automation and Systems, ICCAS 2015 |
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| Country/Territory | Korea, Republic of |
| City | Busan |
| Period | 13/10/15 → 16/10/15 |
Bibliographical note
Publisher Copyright:© 2015 Institute of Control, Robotics and Systems - ICROS.
Keywords
- Autonomous Navigation Algorithm
- Geographic Position
- Observation Angle
- Perturbation Model