Abstract
The final goal of this study is to develop a small and low altitude solar powered UAV. In the first step, the main design parameters were considered and the dynamic modeling was carried out. For the small size and low altitude operation, the design parameters were derived from the literature study. The fundamental aerodynamics of the selected airfoil was investigated. The energy consumption for mission profile and level flight are estimated according to the various altitudes. The flight motion equation by Lagrange-Euler was derived.
| Original language | English |
|---|---|
| Title of host publication | ICCAS 2011 - 2011 11th International Conference on Control, Automation and Systems |
| Pages | 1085-1088 |
| Number of pages | 4 |
| State | Published - 2011 |
| Event | 2011 11th International Conference on Control, Automation and Systems, ICCAS 2011 - Gyeonggi-do, Korea, Republic of Duration: 2011.10.26 → 2011.10.29 |
Publication series
| Name | International Conference on Control, Automation and Systems |
|---|---|
| ISSN (Print) | 1598-7833 |
Conference
| Conference | 2011 11th International Conference on Control, Automation and Systems, ICCAS 2011 |
|---|---|
| Country/Territory | Korea, Republic of |
| City | Gyeonggi-do |
| Period | 11.10.26 → 11.10.29 |
UN SDGs
This output contributes to the following UN Sustainable Development Goals (SDGs)
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SDG 7 Affordable and Clean Energy
Keywords
- Selected keywords relevant to the subject
Quacquarelli Symonds(QS) Subject Topics
- Computer Science & Information Systems
- Engineering - Electrical & Electronic
- Engineering - Petroleum
- Data Science
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