Orbit Determination via a Deeply- Coupled UKF/GNSS Filter
This paper is dedicated to determining the orbit of a satellite by using Unscented Kalman Filter (UKF), in which, a GNSS is used as the observation sensor. During this goal, firstly we have simulated the satellite orbit; considering oblations effect. Secondly, exploiting a nonlinear model of orbit d...
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| Autori principali: | , , |
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| Natura: | Artigo |
| Lingua: | Persa |
| Pubblicazione: |
Aerospace Research Institute
2016-11-01
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| Serie: | فصلنامه علوم و فناوری فضایی |
| Soggetti: | |
| Accesso online: | https://jsst.ias.ir/article_44472_82d57b3de3b310bdfd7b33d32dc189bf.pdf |
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