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Design and Dynamic Analysis of a Coaxial Thrust Vectored Rotor VTOL Drone

Foroozannejad, Mahdi | 2022

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  1. Type of Document: M.Sc. Thesis
  2. Language: Farsi
  3. Document No: 55727 (45)
  4. University: Sharif University of Technology
  5. Department: Aerospace Engineering
  6. Advisor(s): Sagafi, Freeborz
  7. Abstract:
  8. There is a class of small vertical take-off and landing flying vehicles that only have a dual coaxial engine on top and move based on the thrust vector control method. In this project in order to have better insight about the physical mechanism we are dealing with, a conceptual design of a prototype vehicle is first carried out. It is then followed by extraction of two and three dimensional dynamic models of the vehicle. By computer simulation and a simple dynamic analysis, the equations are verified and the movement of the aircraft is discussed for different flight phases
  9. Keywords:
  10. Dynamic Analysis ; Vertical Take-Off and Landing (VtOL) ; Dynamic Modeling ; Dynamic Simulation ; Thrust Vectoring Control System (TVCS) ; Coaxial Motors

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