Articles
<![CDATA[PUNA Aircraft Static Stability Simulation Using XFLR5 Software ]]>
<![CDATA[Bangga Dirgantara Adiputra]]>;
<![CDATA[Agus Rohmanto]]>
<![CDATA[ Compiler Vol 11, No 2 (2022): November ]]>
Publisher : <![CDATA[Institut Teknologi Dirgantara Adisutjipto ]]>
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DOI: 10.28989/compiler.v11i2.1364
<![CDATA[Currently the development of Uncrewed Aircraft is experiencing a very rapid increase. This is demonstrated by the large number of use of Unmanned Aircraft in several sectors, one of which is for monitoring traffic density. On this mission the aircraft will carry a payload in the form of a camera used to record or display the existing traffic situation. This mission requires aircraft with good stability capabilities so as to be able to provide good monitoring results. So it is necessary to analyze the static stability in longitudinal, lateral and directional motion. Static stability simulation was carried out with the help of XLFR5 software. The simulation results are then compared with the parameters that are a requirement for longitudinal, lateral, and directional static stability.]]>
<![CDATA[Three-Dimensional Flight Simulator Takeoff Movement on Boeing 737-300 Aircraft ]]>
<![CDATA[Muhammad Irfan]]>;
<![CDATA[Nurcahyani Dewi Retnowati]]>;
<![CDATA[Bangga Dirgantara Adiputra]]>
<![CDATA[ Compiler Vol 8, No 2 (2019): November ]]>
Publisher : <![CDATA[Institut Teknologi Dirgantara Adisutjipto ]]>
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DOI: 10.28989/compiler.v8i2.523
<![CDATA[The simulator is a form of imitation of conditions describing a behavior in conformity with the reality in which there is an interaction between the user and the simulation. Simulators are very useful for simulating events that can help the teaching and learning system. The result of this final project is a 3D take off simulator on a desktop-based Boeing 737-300 that serves as a training aid and contains an explanation of Boeing 737-300 take off information. This simulator provides ideal data in the form of weight, take off speed, flap settings and distance data to understand the aircraft performing the V1, VR and V2 processes. The research methods carried out include modeling a Boeing 737-300 aircraft using blueprint, asset modeling, and texturing using Blender 3D software then proceed with the design of simulations using Unity software. Simulation tests include black box testing. The results of the black box testing indicate that all functions of the simulator run according to the Windows 7, Windows 8, and Windows 10 operating system with a 64-bit system. Flight simulator is functioning properly and can show information on the movements and conditions od the aircraft in taking flight in the takeoff phase with weight conditions, the speed at which the aircraft drove on the runway, wind pressure conditions on the runway and flaps that will be arranged in this flight simulator.]]>
<![CDATA[Green Concept of Kulon Progo Airport Development using UMI Simulation ]]>
<![CDATA[Sri Mulyani]]>;
<![CDATA[Rianto Rianto]]>;
<![CDATA[Bangga Dirgantara Adiputra]]>
<![CDATA[ Compiler Vol 12, No 1 (2023): May ]]>
Publisher : <![CDATA[Institut Teknologi Dirgantara Adisutjipto ]]>
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DOI: 10.28989/compiler.v12i1.1654
<![CDATA[High energy consumption on the airport becomes a very crucial issue nowadays. Uninterruptable energy supply is required to support airline’s activity and keep the passenger convenience. Regarding the mentioned problem, there is a need to enhance the current plan of the airport with green airport concept. Green airport concept also known as eco-airport is an airport that adopted green and sustainable ecosystem concept to integrate community and environment that lead to reduction of energy consumption. The blueprint of Kulon Progo airport with green concept located in D.I. Yogyakarta, Indonesia has been made and the construction started in the mid of 2016. The airport has a FAR of 0.16 with 637 hectares land area. This study is simulating the plan to assess the energy consumption and CO2 emission in each part of the building in Kulon Progo Airport using Urban Modeling Interface simulator. From the results, it can be seen that the passenger terminal building is responsible for the highest share with 1,351,861.01 Kwh while second floor of ATC building has the highest CO2 emission 2,679.77 kgCO2/m]]>
<![CDATA[Pelatihan Pembuatan Pesawat Outdoor Hand Launched Glider (OHLG) Pada Siswa SMAN 2 Playen Gunungkidul ]]>
<![CDATA[Gunawan Gunawan]]>;
<![CDATA[Bangga Dirgantara Adiputra]]>;
<![CDATA[Maria Asumpta Deny Kusumaningrum]]>;
<![CDATA[Suhanto Suhanto]]>;
<![CDATA[Marni Astuti]]>;
<![CDATA[Riani Nurdin]]>;
<![CDATA[Uyuunul Mauidzoh]]>;
<![CDATA[Rully Medianto]]>
<![CDATA[ Jurnal Penamas Adi Buana Vol 8 No 02 (2025): Jurnal Penamas Adi Buana ]]>
Publisher : <![CDATA[LPPM Universitas PGRI Adi Buana Surabaya ]]>
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DOI: 10.36456/penamas.vol8.no02.a9649
<![CDATA[Sekolah Menengah Atas Negeri (SMAN) 2 Playen yang terletak di Kecamatan Playen, Kabupaten Gunung Kidul mempunyai tujuan untuk mengembangkan bakat dan potensi peserta didik melalui program pengembangan diri dan program Kelas Khusus Olahraga. Namun saat ini bidang olah raga dirgantara khususnya aeromodelling belum ada baik berdasarkan kurikuler maupun ekstrakurikuler. Solusi untuk mengatasi permasalahan diatas, maka diperlukan pendampingan pada siswa SMAN 2 Playen, agar dapat menambahkan kegiatan olah raga lain di bidang aeromodelling khususnya menerbangakan pesawat Outdoor Hand Launched Glider (OHLG). Untuk itu perlu diadakan pelatihan pembuatan Pesawat OHLG pada siswa SMAN 2 Playen, Gunungkidul. Model OHLG atau yang lebih sering disebut dengan Chuck Glider adalah model yang dirancang untuk terbang bebas dengan daya yang ada pada model itu dilempar dengan tangan manusia agar mencapai ketinggian tertentu untuk memulai penerbangannya. Metode yang digunakan dalam pengabdian masyarakat ini yaitu ceramah dan tanya jawab, praktik pembuatan pesawat OHLG, dan praktik menerbangkan pesawat OHLG. Hasil diperoleh dari pengabdian masyarakat ini yaitu siswa antusias dalam mengikuti kegiatan sehingga pengetahuan siswa pesawat OHLG dengan nilai “baik” naik dari 24% menjadi 62%, sedangkan nilai “sangat baik” naik dari 8% menjadi 14%. Siswa Sekolah Menengah Atas Negeri (SMAN) 2 Playen juga mampu membuat dan menerbangkan Pesawat Outdoor Hand Launched Glider (OHLG).]]>
<![CDATA[Estimasi Volume Penumpang Pesawat Udara di Bandar Udara Internasional Adisutjipto Menggunakan Model Gravity ]]>
<![CDATA[Gunawan, Gunawan]]>;
<![CDATA[Mauidzoh, Uyuunul]]>;
<![CDATA[Adiputra, Bangga Dirgantara]]>;
<![CDATA[Dinaryanto, Okto]]>
<![CDATA[ MEDIA KOMUNIKASI TEKNIK SIPIL Volume 31, Nomor 1, JULI 2025 ]]>
Publisher : <![CDATA[Department of Civil Engineering, Diponegoro University ]]>
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DOI: 10.14710/mkts.v31i1.72157
<![CDATA[Demand forecasting is used by airlines to predict the travel behavior of potential passengers. Accurate forecasting is critical to the overall success of an airline. An important element in forecasting is passenger volume estimation. The goal is to predict the number of passengers expected between two cities for a given time interval. Based on this forecast, airlines can make decisions about new routes or additional flights on existing routes. Starting January 2020, all flights to Yogyakarta have landed at Yogyakarta International Airport (YIA) except for flights using propeller aircraft such as ATR which can still use Adisutjipto International Airport (JOG). Adisutjipto International Airport currently only serves 3 routes, namely Yogyakarta (JOG) - Jakarta (HLP) RT., Yogyakarta (JOG) - Bandung (BDO) RT., and Yogyakarta (JOG) - Surabaya (SUB) RT.. The opening of Adisutjipto International Airport to propeller aircraft makes it possible to increase flight frequencies or new routes. For that, it is necessary to estimate the volume of aircraft passengers at Adisutjipto International Airport using the gravity model. The most accurate model is Model 5, where the attraction force is separated into the number of residents of the origin and destination zones and the GRDP of the origin and destination zones, as well as the distance impedance factor and ticket rates are also separated.]]>
<![CDATA[SIMULASI KESTABILAN PROTOTYPE UAV-SPRAYER BERBASIS QUADCOPTER TERHADAP PENAMBAHAN SEKAT PADA PENAMPUNG CAIRAN ]]>
<![CDATA[Hariyanto, Kris]]>;
<![CDATA[Dirgantara, Bangga]]>
<![CDATA[ Vortex Vol 3, No 2 (2022) ]]>
Publisher : <![CDATA[Institut Teknologi Dirgantara Adisutjipto ]]>
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DOI: 10.28989/vortex.v3i2.1229
<![CDATA[The use of UAVs has begun to penetrate the world of agriculture. One of the functions of UAVs in agriculture is to spray pesticides. The pesticides used are liquid so that when the UAV is airborne and maneuvering, the fluid experiences fluid motion or sloshing. Sloshing that occurs can cause the balance of the UAV to be disturbed. To overcome this, a bulkhead or baffle is needed in the reservoir in order to reduce fluid movement. In the case of the research studied, the simulation of sloshing in the reservoir with the presence of baffles and without the presence of baffles. This research uses different reservoir variations and different water levels, namely 55 mm, 35 mm and 15 mm. Simulations are carried out during cruising and maneuvering flights at a speed of 2 m/s. The container modeling uses the Catia V5R20 software and the simulation uses the Ansys 14.5 software. The simulation results show that the effect of baffle placement is more visible if the baffle is placed in the xy plane, while for the baffle placement in the yz plane, the force caused by sloshing is greater. In spraying the UAV-Sprayer will more often fly forward (cruise), while for maneuvers (right or left) it is only done occasionally/not too often. So that giving baffles is more effective in the xy plane because it can reduce sloshing better than the baffles in the yz plane.]]>
<![CDATA[RELIABILITY ANALYSIS OF MAIN ROTOR EC 155B1 ON PIN BLADE AND ATTACH BEAMS COMPONENTS USING MARKOV ANALYSIS ]]>
<![CDATA[Aditiya, Irvan]]>;
<![CDATA[Pinandhita, Lazuardy Rahendra]]>;
<![CDATA[Adiputra, Bangga Dirgantara]]>
<![CDATA[ Vortex Vol 3, No 1 (2022) ]]>
Publisher : <![CDATA[Institut Teknologi Dirgantara Adisutjipto ]]>
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DOI: 10.28989/vortex.v3i1.1026
<![CDATA[Reliability is used to estimate the conditions of systems or components in the future based on previous conditions. The objects of this research are EC 155B1 aircrafts owned by Indonesia Air Transport & Infrastrucure (IAT), and the method used for analysis is markov analysis. Markov analysis is widely used as an analyzing technique the states of the system that has limited information (memoryless). From this research, ATA chapter 62 Main Rotor that meets the requirements of reliability analysis. The constituent components of main rotor states are Pin Blade, Lower Attach Beam, and Upper Attach Beam. The results of the markov analysis of main rotor system, the states that worked properly are state 1, state 3, and state 4. The probability of the state 1 showed that state has decreased from initial condition, while the state 3 and state 4 have increased from initial condition and subsequently have decreased. The reliability of main rotor system has decreased along with increasing of flight hours with the Mean Time To Failure (MTTF) is 2340.22 flight hours.]]>
<![CDATA[ANALISIS KESIAPAN PKP-PK BANDAR UDARA INTERNASIONAL BANYUWANGI DALAM MENDUKUNG PENANGGULANGAN KEADAAN DARURAT ]]>
<![CDATA[Hilmy, Muhammad Nur]]>;
<![CDATA[Gunawan, Gunawan]]>;
<![CDATA[Adiputra, Bangga Dirgantara]]>
<![CDATA[ Vortex Vol 4, No 1 (2023) ]]>
Publisher : <![CDATA[Institut Teknologi Dirgantara Adisutjipto ]]>
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DOI: 10.28989/vortex.v4i1.1457
<![CDATA[PKP-PK is a unit that must be owned by every airport. This unit is tasked with carrying out aviation accident rescue and fire fighting in the area or around the airport. Seeing the importance of this unit, it is necessary to conduct research on emergency service facilities, find out the reaction time, analyze PKP-PK categories, analyze fire risk management, and the development of this unit. This research was conducted at the PKP-PK unit located at Bayuwangi International Airport. The research method used is descriptive quantitative where data is obtained from the results of questionnaires given to PKP-PK personnel. These data are then compared with Regulation Nomor KP 14 Tahun 2015 which is used to assess the readiness of the PKP-PK. Whereas for risk mapping using the FAA Risk Matrix table. The results show that there is still a shortage of operational facilities while the reaction time and PKP-PK categories are in accordance with regulations. Risk mapping obtains 4 events that have a potential hazard.]]>
<![CDATA[ANALISIS BENDING PADA KOMPOSIT SERAT ALAM DAUN AGEL DENGAN RESIN EPOXY ]]>
<![CDATA[Sahuburua, Stevward Norenssio]]>;
<![CDATA[Hartini, Dwi]]>;
<![CDATA[Adiputra, Bangga Dirgantara]]>
<![CDATA[ Vortex Vol 4, No 2 (2023) ]]>
Publisher : <![CDATA[Institut Teknologi Dirgantara Adisutjipto ]]>
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DOI: 10.28989/vortex.v4i2.1696
<![CDATA[The use of composite materials, especially those developed by natural fibers in various equipment, has begun to develop a lot, the use of natural agel leaf fibers as composite materials can reduce the use of synthetic materials and increase the utilization of agel leaf natural fibers which are still a lot of wasted. This study aims to determine the stages or processes of agel leaf natural fiber composite using 2 methods of hand lay up, vacuum bag and to determine the value of the bending strength of agel leaf natural fiber material between variations of the epoxy matrix in the direction of the fibers 0^° and 〖90〗^°.Based on the data from the test results, it can be concluded that the average value of maximum bending strength in agel leaf natural fiber composites using the vacuum bag manufacturing method with a volume fraction of 60% and fiber direction 0^° and 〖90〗^° has an average maximum bending strength value that is the highest, namely 11.006 MPa and 11.057 MPa and the composite of agel leaf natural fiber using the hand lay up method (non vacuum bag) with a volume fraction of 50%, 60%, 70% and fiber direction 0^° has the lowest average maximum bending strength values of 3.413 MPa, 5.404 MPa, 4.625 MPa.]]>
<![CDATA[Karakterisasi sifat bending komposit hibrid serat alam daun nanas dan serat bambu untuk aplikasi struktur UAV ]]>
<![CDATA[Pangkey, Calvin Delano Immanuel]]>;
<![CDATA[Hartini, Dwi]]>;
<![CDATA[Adiputra, Bangga Dirgantara]]>
<![CDATA[ Vortex Vol 5, No 2 (2024) ]]>
Publisher : <![CDATA[Institut Teknologi Dirgantara Adisutjipto ]]>
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DOI: 10.28989/vortex.v5i2.2510
<![CDATA[Pengembangan teknologi ramah lingkungan sedang banyak mendapatkan perhatian dari berbagai bidang. Salah satunya ialah pemanfaatan serat alam dalam pembuatan bahan komposit. Pemanfaatan serat daun nanas dan serat bambu sebagai bahan penguat komposit dapat menjadi alternatif bahan penguat sintetis yang banyak digunakan. Penelitian ini berfokus pada pengujian bending untuk mengetahui kekuatan bending dari komposit hybrid serat alam daun nanas dan serat bambu. Pembuatan komposit hybrid serat alam daun nanas dan serat bambu menggunakan metode hand lay-up, dengan orientasi serat 0ᵒ, resin Epoxy, dan fraksi volume 50%, 60%, dan 70%. Hasil pengujian bending menunjukkan kekuatan bending maksimum tertinggi didapatkan pada fraksi volume 50%, dengan nilai kekuatan bending sebesar 86,116 MPa. Sedangkan kekuatan bending maksimum terendah diperoleh pada fraksi volume 60% yaitu sebesar 49,653 MPa. Fraksi volume 70% berada ditengah-tengah dengan nilai kekuatan bending maksimum sebesar 68,115 MPa.]]>
