Özet
In this paper, a basic CubeSat model is tried to be controlled with optimizing gain parameters of linear quadratic regulator. Noisy sensor measurements are used to determine attitude by using TRIAD. To reduce the effects of noise in optimization process, a two-step optimization approach is implemented. As a result of this approach, particle swarm optimization achieved to tune gain parameters of the controller.
| Orijinal dil | İngilizce |
|---|---|
| Ana bilgisayar yayını başlığı | 2023 5th International Conference on Problems of Cybernetics and Informatics, PCI 2023 |
| Yayınlayan | Institute of Electrical and Electronics Engineers Inc. |
| ISBN (Elektronik) | 9798350319064 |
| DOI'lar | |
| Yayın durumu | Yayınlandı - 2023 |
| Etkinlik | 5th International Conference on Problems of Cybernetics and Informatics, PCI 2023 - Baku, Azerbaijan Süre: 28 Ağu 2023 → 30 Ağu 2023 |
Yayın serisi
| Adı | 2023 5th International Conference on Problems of Cybernetics and Informatics, PCI 2023 |
|---|
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| ???event.eventtypes.event.conference??? | 5th International Conference on Problems of Cybernetics and Informatics, PCI 2023 |
|---|---|
| Ülke/Bölge | Azerbaijan |
| Şehir | Baku |
| Periyot | 28/08/23 → 30/08/23 |
Bibliyografik not
Publisher Copyright:© 2023 IEEE.
Parmak izi
Development of Satellite Attitude Controller with TRIAD and Particle Swarm Optimization Using Only Magnetic Actuators' araştırma başlıklarına git. Birlikte benzersiz bir parmak izi oluştururlar.Alıntı Yap
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