DESAIN DAN PENGEMBANGAN UAV FIXED WING MENGGUNAKAN SUMBER DAYA HYBRID SOLAR CELL DAN BATERAI

AL AZER, ABDO and Hikmarika, Hera (2019) DESAIN DAN PENGEMBANGAN UAV FIXED WING MENGGUNAKAN SUMBER DAYA HYBRID SOLAR CELL DAN BATERAI. Undergraduate thesis, Sriwijaya University.

[thumbnail of RAMA_20201_03041381419139.pdf] Text
RAMA_20201_03041381419139.pdf - Accepted Version
Restricted to Repository staff only
Available under License Creative Commons Public Domain Dedication.

Download (9MB) | Request a copy
[thumbnail of RAMA_20201_03041381419139_TURNITIN.pdf] Text
RAMA_20201_03041381419139_TURNITIN.pdf - Accepted Version
Restricted to Repository staff only
Available under License Creative Commons Public Domain Dedication.

Download (14MB) | Request a copy
[thumbnail of RAMA_20201_03041381419139_0007127801_01_front_ref.pdf] Text
RAMA_20201_03041381419139_0007127801_01_front_ref.pdf - Accepted Version
Available under License Creative Commons Public Domain Dedication.

Download (1MB)
[thumbnail of RAMA_20201_03041381419139_0007127801_02.pdf] Text
RAMA_20201_03041381419139_0007127801_02.pdf - Accepted Version
Restricted to Repository staff only
Available under License Creative Commons Public Domain Dedication.

Download (1MB) | Request a copy
[thumbnail of RAMA_20201_03041381419139_0007127801_03.pdf] Text
RAMA_20201_03041381419139_0007127801_03.pdf - Accepted Version
Restricted to Repository staff only
Available under License Creative Commons Public Domain Dedication.

Download (621kB) | Request a copy
[thumbnail of RAMA_20201_03041381419139_0007127801_04.pdf] Text
RAMA_20201_03041381419139_0007127801_04.pdf - Accepted Version
Restricted to Repository staff only
Available under License Creative Commons Public Domain Dedication.

Download (1MB) | Request a copy
[thumbnail of RAMA_20201_03041381419139_0007127801_05.pdf] Text
RAMA_20201_03041381419139_0007127801_05.pdf - Accepted Version
Restricted to Repository staff only
Available under License Creative Commons Public Domain Dedication.

Download (187kB) | Request a copy
[thumbnail of RAMA_20201_03041381419139_0007127801_06_ref.pdf] Text
RAMA_20201_03041381419139_0007127801_06_ref.pdf - Bibliography
Restricted to Repository staff only
Available under License Creative Commons Public Domain Dedication.

Download (133kB) | Request a copy
[thumbnail of RAMA_20201_03041381419139_0007127801_07_lamp.pdf] Text
RAMA_20201_03041381419139_0007127801_07_lamp.pdf - Accepted Version
Restricted to Repository staff only
Available under License Creative Commons Public Domain Dedication.

Download (5MB) | Request a copy

Abstract

UAV (Unmanned Aerial Vehicle) is an unmanned flying vehicle technology developed and used to help human’s work in many aspects such as for mapping system, logistics, defence and security and other sectors. UAV is inseparable from battery usage as a power source with long-period usage purposes. Which means UAV’s flight time influences the power source needed. The long flight time will need a bigger power source. The increasing demand for power will need an additional power source for the UAV which in this case has chosen solar cell as a solution to the problem. A fixed-wing UAV is chosen as it aligns with solar cells’ thin shape which can be taped to the UAV’s wings. The purpose of this research is to apply the design of the fixed wing which can take flight with the usage of solar cell as an additional power source to increase its flight time. Research result shows the PWM value required to fly the fixed wing is 1730 with a flight time for 789 seconds or 13 minutes and 9 seconds.

Item Type: Thesis (Undergraduate)
Uncontrolled Keywords: UAV, Fixed Wing, Baterai, Solar Cell, PWM, Flight Time
Subjects: T Technology > TL Motor vehicles. Aeronautics. Astronautics > TL1-4050 Motor vehicles. Aeronautics. Astronautics
Divisions: 03-Faculty of Engineering > 20201-Electrical Engineering (S1)
Depositing User: Users 577 not found.
Date Deposited: 01 Aug 2019 13:22
Last Modified: 02 Aug 2019 03:02
URI: http://repository.unsri.ac.id/id/eprint/1661

Actions (login required)

View Item View Item