PRELIMINARY DESIGN OF UNMANNED AIRLAND (PUNA)

Abstract

The development of the number of vehicles exceeding the capacity of highways in urban areas causes frequent traffic jams and increases the risk of accidents. This often happens during year-end holidays and Eid holidays. So it is very necessary to monitor traffic density during the annual holiday period to reduce the number of fatalities due to traffic accidents. Monitoring traffic density using helicopters is expensive because of the high fuel consumption and maintenance. So we need a new alternative, namely using Unmanned Aircraft (PUNA) because it is easy to operate and cheap to maintain. So it is very necessary to design PUNA for traffic density monitoring missions. Aircraft for this purpose are classified as small because the payload, namely the camera, only weighs 2 kg. Study obtained the following results: fuselas/body length 1.94 m, wingspan 1.46 m, airfoil NACA 2412. engine OS MAX-40FX, engine located in the nose, take-off Gross Weight 6.11 kg, material weight 321.09 grams, use an Oblique Camera type camera, the camera weight is 2 kg, and the camera position is 3 ft from the nose. Keywords drone; puna; design Full Text: PDF References Daniel P. Raymer. (1989). Aircraft Design: A Conseptual Approach,. California: President, Conceptual Research Corporation Sylmar. John D. Anderson, J. (1999). Aircraft Performance and Design. Tata McGraw Hill. Putra, A. N. (2018). Desain Awal dan Analisis Aerodinamika Pesawat UAV V- SKY 14. Yogyakarta: Sekolah Tinggi Teknologi Adisutjipto. Wildan (2018). Desain dan Analisis Aerodinamika Pesawat UAV Cargo X. Yogyakarta: Sekolah Tinggi Teknologi Adisutjipto. Syamsuar, S. (2015). Studi Kasus Prestasi Terbang Takeoff-Landing. Jurnal Perhubungan Udara , 49-58. Mohammad H.Sadraey (2013). Aircraft Design A Systems Engineering Approach,.USA, New Hampshire, Daniel Webster Collage. http://dx.doi.org/10.28989/vortex.v3i1.1186 Refbacks There are currently no refbacks.