International Journal of Technology | |
A Novel Method for Moments of Inertia Tuning for Free-flying Dynamically Similar Models via Simulated Annealing | |
AliShakoori1  | |
关键词: Dynamically similar/scaled model; Moments of inertia; Optimization; Simulated annealing; Tuning; | |
DOI : 10.14716/ijtech.v8i3.2058 | |
学科分类:工程和技术(综合) | |
来源: Universitas Indonesia | |
【 摘 要 】
In this study, a method was developed for tuning moments of inertia for a free-flying dynamically similar/scaled model of an aircraft. For this method, the simulated annealing optimization algorithm was used to obtain similar mass-inertial properties of the model and the full-scale aircraft utilizing ballast weights. For a scaled model of a Su-27 fighter, the ballast arrangement were designed and weights were determinedto achieve the required center of gravity position and the moments of inertia based on the similitude requirements. A computer code was developed, and the task of tuning inertia properties was performed. The results showed that the proposed optimization approach was successfully used to determine a feasible ballast weight and position. Moreover, the ballast weight reduced from 8.66 kg to 4.86 kg using the proposed technique, and the inertia characteristics’ non-similarity was minimized.
【 授权许可】
CC BY-NC-ND
【 预 览 】
Files | Size | Format | View |
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RO201901219041415ZK.pdf | 1042KB | download |