Design and Analysis the Strength of the Structure Fixed Wing Vertical Take Off-Landing UAV

Djarot Wahju Santoso, Aditya Nurcholis Putra

Abstract


To respond to traffic conditions in the city traffic jam so as to resolve the density it is necessary to observe these conditions which are monitored at all times. For this reason, it is necessary to design UAV (Unmanned Aerial Vehicle) that is capable of flexible maneuvering, which can take off and land vertically and move quickly to reach traffic in different places. The stages of research for designing fixed wing VTOL aircraft are carried out determining the geometry of the aircraft as the desired criteria, the analysis stage by 3D modeling with CATIA software. Simulation of structural analysis in the form stress and calculating the Margin of Safety from this design. The results of the aircraft design have 1.32 m fuselage length, 1.71 m wing span and aircraft weight 2.865 kg. The results of the analysis show that the aircraft structure is safe in cruise and vertical take-off load.

Full Text:

PDF

References


Patra, Aswini Kumar, Patel, Kandarp, Bundela, Gourav Singh, Vinay. P. (2017). Design and Development of Transition Autopilot for VTOL UAV, International Journal Of Innovations In Engineering Research and Technology (IJIERT), Vol. 4, Issue 6.

Sandilya, B. Vijay, Kumar K, Sachin, Kumar P., Sampath, Shyam Y, Santosh. (2014). Design And 3D Modelling Of Vertical Take Off And Landing (VTOL) Tilt Quad Rotor RC Aircraft, Proceedings of 5th SARC-IRF International Conference, Bangalore, India.

Raymer, D. P. (1999). Aircraft design: a conceptual approach, American Institute of Aeronautics and Astronautics. Inc., Reston, VA, 21.

Niu, M. C. Y. (1997). Airframe stress analysis and sizing (p. 795). Hong Kong: Conmilit Press.

Australia, C. A. S. A. (2000). Design Standards: Unmanned Aerial vehicles–Aeroplane.

Kamil, Sulaeman, Beban Pesawat, Penerbit ITB.




DOI: http://dx.doi.org/10.28989/senatik.v4i0.232

Article Metrics

Abstract view : 19 times
PDF - 0 times

Refbacks

  • There are currently no refbacks.




Creative Commons License
This work is licensed under a Creative Commons Attribution 4.0 International License.

Conference SENATIK P-ISSN :2337-3881 and  E-ISSN : 2528-1666