PERANCANGAN AWAL PESAWAT TANPA AWAK R-215 AG UNTUK MISI PEMANTAUAN LAHAN PERTANIAN

AMSAL GINTING, REZA (2018) PERANCANGAN AWAL PESAWAT TANPA AWAK R-215 AG UNTUK MISI PEMANTAUAN LAHAN PERTANIAN. Skripsi thesis, Institut Teknologi Dirgantara Adisutjipto.

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Abstract

The development of unmanned aircraft is currently developing and widely used for certain missions such agricultural monitoring. Data design requirements and objectives DR O are necessary to design taircraft whether the aircraft is in line with its mission objectives. There are several aspects to consider for designing aircraft such as airplane geometry configuration, aircraft aerodynamic characteristics, static stability parameters and range and endurance aircraft from the design aspect of geometry configuration of the aircraft can be seen from the form of geometry configuration as whole in accordance with the conditions required from the aspect of aerodynamics can be seen from the characteristics of flying aircraft from the static stability aspect seen when flying conditions whether the plane is called static or not and from the aspect range and endurance can be seen flying cruising and long flying aircraft. The purpose of the initial design of the aircraft is to produce the configuration of the geometry that the aircraft will use, to know the results of the aerodynamic characteristics of the aircraft while flying, to know the parameters of static stability parameters and to know the range and endurance of the aircraft that can be taken during flight The objectives of the initial design stage of the R-215 AG aircraft are to obtain the result of airplane geometry configuration, to see the aircrafts aerodynamic characteristics, with ANSYS 16 software, to get the parameters of static stability of the aircraft with XLFR5 software and the range and endurance of aircraft which can then be studied with DR O data, The conclusions can be obtained from the initial design analysis of unmanned aircraft R 215 AG that is Result of configuration and geometry according to DR O make, aerodynamic characteristic result on R215 AG to get MTOW according to elevator with angle of incident 3 with elevator 31,344 N with mass 3,198 kg more than 2,735 kg, static stability analysis result concluded to have met static stability criteria with static longitudinal stability Cma is smaller than 0 negative is 0.0137 which means plane in the static stable category of longitudinal matra. Static stability of the matra directional: the value of CnB is greater than 0 positive that is 0,0009 so the plane is included in the category of static stable directional matra. Static stability of the lateral dimension: The value of CIB is smaller than 0 negative ie:0.00001. So the plane is included in the category of static stabilized lateral and lateral Range results: 7,226 km and Endurance: 1,423 hours

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