Hybrid Estimation of Gyro Model Parameters and GEO Satellite Moment of Inertia with Extended Kalman Filter
This paper deals with the estimation of gyro model parameters and GEO satellite moment of inertia at the same time in transfer orbit phase. In order to fuse information of attitude determination subsystem sensors, an extended Kalman Filter has been employed. The estimation variables are including: q...
| 出版年: | فصلنامه علوم و فناوری فضایی |
|---|---|
| 主要な著者: | , , |
| フォーマット: | 論文 |
| 言語: | ペルシア語 |
| 出版事項: |
Aerospace Research Institute
2013-07-01
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| 主題: | |
| オンライン･アクセス: | https://jsst.ias.ir/article_14475_fdafd89c32c1463a86fa94b58130c19b.pdf |