تقرير
Deterministic Global Optimization of Flapping Wing Motion for Micro Air Vehicles
| العنوان: | Deterministic Global Optimization of Flapping Wing Motion for Micro Air Vehicles |
|---|---|
| المؤلفون: | Ghommem, Mehdi, Hajj, Muhammad R., Watson, Layne T., Mook, Dean T., Snyder, Richard D., Beran, Philip S. |
| المساهمون: | Computer Science |
| بيانات النشر: | Department of Computer Science, Virginia Polytechnic Institute & State University |
| سنة النشر: | 2010 |
| المجموعة: | VTechWorks (VirginiaTech) |
| مصطلحات موضوعية: | Algorithms, Data structures |
| الوصف: | The kinematics of a flapping plate is optimized by combining the unsteady vortex lattice method with a deterministic global optimization algorithm. The design parameters are the amplitudes, the mean values, the frequencies, and the phase angles of the flapping motion. The results suggest that imposing a delay between the different oscillatory motions and controlling the way through which the wing rotates at the end of each half stroke would enhance the lift generation. The use of a general unsteady numerical aerodynamic model (UVLM) and the implementation of a deterministic global optimization algorithm provide guidance and a baseline for future efforts to identify optimal stroke trajectories for micro air vehicles with higher fidelity models. |
| نوع الوثيقة: | report |
| وصف الملف: | application/pdf |
| اللغة: | English |
| العلاقة: | Computer Science Technical Reports; http://eprints.cs.vt.edu/archive/00001138Test/; http://hdl.handle.net/10919/19415Test; TR-10-18; http://eprints.cs.vt.edu/archive/00001138/01/dirMAO10.pdfTest |
| الإتاحة: | http://hdl.handle.net/10919/19415Test http://eprints.cs.vt.edu/archive/00001138Test/ http://eprints.cs.vt.edu/archive/00001138/01/dirMAO10.pdfTest |
| حقوق: | In Copyright ; http://rightsstatements.org/vocab/InC/1.0Test/ |
| رقم الانضمام: | edsbas.BF92F25C |
| قاعدة البيانات: | BASE |
| الوصف غير متاح. |