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- Type of Document: M.Sc. Thesis
- Language: Farsi
- Document No: 55408 (45)
- University: Sharif University of Technology
- Department: Aerospace Engineering
- Advisor(s): Banazadeh, Afshin
- Abstract:
- In the present study, an attempt has been made to design and develop a nano drone using the dynamics of single-wing drones. To reduce the noise associated with nano-drone motors, a unique magnetic system has been developed for the drone's propulsion system, which has technology similar to magnetic trains and uses the theory of magnetic suspension, which is one of the main innovations of this dissertation. The drone designed in this research will have a blade with a radius of 15 cm and its total weight will be 170 grams, which according to the thrust of the blade will be able to carry a load of 50 grams for 14 minutes. In this research, after the initial design of the drone and related systems and its three-dimensional modeling, by developing the dynamic relationships related to single-wing drones, the dynamic modeling of this drone has been attempted. With the development of modeling relationships and their implementation in the software environment, it was observed that the drone climb well in a state without any external disturbance. In order to validate the developed equations, by changing the initial conditions, changing the geometry and applying different thrusts, it was shown that the developed model can well show the physics governing the subject. Finally, in order for the drone to be able to move in the longitudinal and transverse directions, by modeling the movement of the flap considered on the design as a cyclic flap, it was shown that the drone will be able to move in the longitudinal and transverse directions as well.
- Keywords:
- Electromagnetic ; Simulation ; Modeling ; Design ; Nano Single Wing ; Unmanned Aerial Vehicles (UAV)
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