The manuscript deals with the fabrication of fixed-wing UAV or drone with solar panel on wings. The research work is to increase the endurance of the UAV using the solar power. The research work begins with a suitable methodology to design a solar UAV. Once the design phase is completed, weight estimation was performed with the available design values. The estimated weight was taken as in the input value to predict the aerodynamic forces such as lift and drag. Further thrust was estimated using a test rig and UAV experiments. These performance values are experimental which was obtained using detailed design. Further the airfoil selection and rib design were made, and finally, the structure of wing was fabricated. Similar manner tail was designed and fabricated. All the components of wings and tail were manufactured using laser cutting technology. Finally, the performance of solar cell was discussed, and their performance values are recorded.


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    Titel :

    Solar-Powered Fixed-Wing UAV: Fabrication Procedures with Design Methods


    Weitere Titelangaben:

    Lect.Notes Mechanical Engineering


    Beteiligte:
    Singh, Sanjay (Herausgeber:in) / Ramulu, Perumalla Janaki (Herausgeber:in) / Gautam, Sachin Singh (Herausgeber:in) / Vishwath, N. C. Ajay (Autor:in) / Dhanwani, Payal (Autor:in) / Baghel, Rajeev Kumar (Autor:in) / Bendale, Ram (Autor:in) / Mehta, Parshva (Autor:in)

    Kongress:

    International Conference on Modern Research in Aerospace Engineering ; 2023 ; Noida, India September 21, 2023 - September 22, 2023



    Erscheinungsdatum :

    28.04.2024


    Format / Umfang :

    19 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Solar-powered wing

    Emerald Group Publishing | 1998


    DESIGN OF A HYDROGEN POWERED SMALL ELECTRIC FIXED-WING UAV WITH VTOL CAPABILITY

    Alves, B. M. / Coelho, V. L. / Silva, P. A. et al. | TIBKAT | 2021

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