Micro Air Vehicle Nonlinear Simulation | ||||
| International Conference on Aerospace Sciences and Aviation Technology | ||||
| Article 30, Volume 17, AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 17 – April 11 - 13, 2017, April 2017, Page 1-13 PDF (1.05 MB) | ||||
| Document Type: Original Article | ||||
| DOI: 10.21608/asat.2017.22456 | ||||
 View on SCiNiTO | ||||
| Authors | ||||
| Ahmed AboElezz1; Ahmed Desoki2; Basman Elhadidi3; Gamal El-Bayoumi3 | ||||
| 1Aerodynamics laboratory engineer, IAET. | ||||
| 2Assistant professor, Aerospace department, Cairo university. | ||||
| 3Professor Aerospace department, Cairo university. | ||||
| Abstract | ||||
| Micro air vehicle (MAV) is very sensitive to the external disturbances which make the prediction of its dynamics a hard task. In this paper there is a description of nonlinear simulation made for the MAV’s dynamics prediction. Experimental measured data were used in this Simulink simulation, the Aerodynamics forces and moment, Mass moment of inertia, and propulsion system performance were experimentally measured for an accurate simulation of the MAV. The output from the simulation gave accurate prediction for the MAV dynamics. | ||||
| Keywords | ||||
| nonlinear; SIMULINK; MAV; flight dynamics | ||||
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