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A Light Amphibious Airplane's Drop Test Identification Using Multi Kernel Least Square Support Vector Machines |
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| รหัสดีโอไอ | |
| Creator | 1. S. Chinvorarat 2. B. Watjatrakul 3. P. Nimdum 4. T. Sangpet 5. P. Vallikul |
| Title | A Light Amphibious Airplane's Drop Test Identification Using Multi Kernel Least Square Support Vector Machines |
| Publisher | Thai Society of Mechanical Engineers (TSME) |
| Publication Year | 2566 |
| Journal Title | Journal of Research and Applications in Mechanical Engineering (JRAME) |
| Journal Vol. | 11 |
| Journal No. | 1 |
| Page no. | JRAME-23-11-001 (p.1-15) |
| Keyword | Multi-kernel LS-SVM, Gaussian radial basis, Landing gear drop dynamics, Light amphibious airplane |
| URL Website | https://ph01.tci-thaijo.org/index.php/jrame/index |
| Website title | Journal of Research and Applications in Mechanical Engineering (JRAME) |
| ISSN | 2229-2152 |
| Abstract | This article uses multi-kernel least square support vector machines to determine the drop test dynamics for a light amphibious aircraft's stock strut landing gear. The kernel function to assess system nonlinearity is the Gaussian radial basis. The suggested multi-kernel LS-SVM model has shown to provide more accurate displacement output estimation than the traditional LS-SVM model, with RMSE values of 0.21766 and 0.062726 for the strut and wheel of the landing gear, respectively. The drop test of the light amphibious aircraft is conducted to validate the identification capabilities. |
