Please use this identifier to cite or link to this item:
https://dspace.upt.ro/xmlui/handle/123456789/6797| Title: | Design of flight control for hybrid vehicle [articol] |
| Authors: | Nithiyanantham, K.K. Anitha, G. |
| Subjects: | Stability Agility Unfolded UAV Folded UAV Controller for retraction of arms Controller for extension of arms |
| Issue Date: | 2019 |
| Publisher: | Timișoara : Editura Politehnica |
| Citation: | Nithiyanantham, K.K.; Anitha, G.: Design of flight control for hybrid vehicle. Timişoara: Editura Politehnica, 2019. |
| Series/Report no.: | Journal of Electrical Engineering;Vol 19 No 4 |
| Abstract: | The mission of the paper is to design of flight control for Hybrid Vehicle that is capable of flying in Fold (shorter arm length of the vehicle) and unfold mode (larger arm length of the vehicle). Fold mode is especially required to navigate through narrow passages during indoor navigation The results of eCalc calculator shows that the vehicle exhibits more agility in fold mode of the Vehicle and literature survey reveals that greater the arm length greater the stability in unfold mode. |
| URI: | https://dspace.upt.ro/xmlui/handle/123456789/6797 |
| ISSN: | 1582-4594 |
| Appears in Collections: | Articole științifice/Scientific articles |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| BUPT_ART_Nithiyanantham_f.pdf | 538.55 kB | Adobe PDF | View/Open |
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