Design and analysis on payload container for air quality measurement device
The payload design was focusing entirely on making it easy to install based on the given circumstances. The analysis was done to ensure that the drone frame can withstand the weight of the payload, with the structure designed to be as light as possible, while maintaining the strength to carry the lo...
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American Institute of Physics
2025
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| _version_ | 1833349071217098752 |
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| author | Zahari N.M. Khamarudin H.F. Zawawi M.H. Nurhikmah F. Aziz N.A. Abas A. Calvin T.X.L. |
| author2 | 54891672300 |
| author_facet | 54891672300 Zahari N.M. Khamarudin H.F. Zawawi M.H. Nurhikmah F. Aziz N.A. Abas A. Calvin T.X.L. |
| author_sort | Zahari N.M. |
| building | UNITEN Library |
| collection | Institutional Repository |
| content_provider | Universiti Tenaga Nasional |
| content_source | UNITEN Institutional Repository |
| continent | Asia |
| country | Malaysia |
| description | The payload design was focusing entirely on making it easy to install based on the given circumstances. The analysis was done to ensure that the drone frame can withstand the weight of the payload, with the structure designed to be as light as possible, while maintaining the strength to carry the load. Therefore, it is needed to determine whether the drone can hold on while having the payload with the given weight. The payload design needs to be easily secured on to the drone while being able to fit in all the necessary equipment for the air quality measurement system. Numerical Method is used to design and analyze using Finite Element Analysis (FEA) method for drone frame and the payload mount. The FEA method showed the amount of stress and strains on the critical part of the body frame, and it also provides the displacement result of the analysis when the payload is secured onto the drone frame. Based on the results, the study shows that the amount of stress and strain put on the mounting is within the tolerable limits at a maximum value of 4.086e+06 and 6.153e-04 for both stress and strain, respectively. ? 2024 Author(s). |
| format | Conference paper |
| id | my.uniten.dspace-36754 |
| institution | Universiti Tenaga Nasional |
| publishDate | 2025 |
| publisher | American Institute of Physics |
| record_format | dspace |
| spelling | my.uniten.dspace-367542025-03-03T15:44:25Z Design and analysis on payload container for air quality measurement device Zahari N.M. Khamarudin H.F. Zawawi M.H. Nurhikmah F. Aziz N.A. Abas A. Calvin T.X.L. 54891672300 58968178200 39162217600 57204810651 57201665672 56893346700 58968626300 The payload design was focusing entirely on making it easy to install based on the given circumstances. The analysis was done to ensure that the drone frame can withstand the weight of the payload, with the structure designed to be as light as possible, while maintaining the strength to carry the load. Therefore, it is needed to determine whether the drone can hold on while having the payload with the given weight. The payload design needs to be easily secured on to the drone while being able to fit in all the necessary equipment for the air quality measurement system. Numerical Method is used to design and analyze using Finite Element Analysis (FEA) method for drone frame and the payload mount. The FEA method showed the amount of stress and strains on the critical part of the body frame, and it also provides the displacement result of the analysis when the payload is secured onto the drone frame. Based on the results, the study shows that the amount of stress and strain put on the mounting is within the tolerable limits at a maximum value of 4.086e+06 and 6.153e-04 for both stress and strain, respectively. ? 2024 Author(s). Final 2025-03-03T07:44:25Z 2025-03-03T07:44:25Z 2024 Conference paper 10.1063/5.0149386 2-s2.0-85189337424 https://www.scopus.com/inward/record.uri?eid=2-s2.0-85189337424&doi=10.1063%2f5.0149386&partnerID=40&md5=339d785ad4aa5fd3b24b9968401d8ec6 https://irepository.uniten.edu.my/handle/123456789/36754 2750 1 50026 American Institute of Physics Scopus |
| spellingShingle | Zahari N.M. Khamarudin H.F. Zawawi M.H. Nurhikmah F. Aziz N.A. Abas A. Calvin T.X.L. Design and analysis on payload container for air quality measurement device |
| title | Design and analysis on payload container for air quality measurement device |
| title_full | Design and analysis on payload container for air quality measurement device |
| title_fullStr | Design and analysis on payload container for air quality measurement device |
| title_full_unstemmed | Design and analysis on payload container for air quality measurement device |
| title_short | Design and analysis on payload container for air quality measurement device |
| title_sort | design and analysis on payload container for air quality measurement device |
| url_provider | http://dspace.uniten.edu.my/ |