Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (Senastindo)
Semua inovasi yang berguna dan berkaitan secara langsung maupun tidak langsung terhadap inovasi nasional yang lebih bermutu dengan intisari tidak terbatas pada teknologi apapun, baik yang mengenai Databases System, Data Mining/Web Mining, Datawarehouse, Artificial Integelence, Business Integelence, Cloud & Grid Computing, Decision Support System, Human Computer & Interaction, Mobile Computing & Application, E-System, Machine Learning, Deep Learning, Information Retrievel (IR), Computer Network & Security, Multimedia System, Sistem Informasi, Sistem Informasi Geografis (GIS), Sistem Informasi Akuntansi, Database Security, Network Security, Fuzzy Logic, Expert System, Image Processing, Computer Graphic, Computer Vision, Semantic Web, e-Health, Animation dan lainnya yang serumpun dengan Inovasi Nasional lainnya. AERONAUTIKA antara lain: Aerodinamika, Material dan Komposit, Kelistrikan dan Instrumen Pesawat Terbang, Avionik, Flying Control, Teknologi Rekayasa Material, Termofluida, Fluida Mekanik, Material Komposit Maju, Teknologi Persenjataan, dsb. TEKNIK ELEKTRO antara lain: Sistem Mikroelektronik, Instrumentasi Industri, Optoelektronik, Perancangan Rangkaian Analog, Desain dan Teknologi ASIC, Desain dan Teknologi FPGA, Sensor dan Transducer, Sistem Pembangkit Energi Listrik, Sistem Transmisi dan Distribusi, Sistem Proteksi Listrik, Tegangan Tinggi, Mesin-mesin Listrik, Elektronika Daya, Energi Terbarukan, Modulasi dan Pemrosesan Sinyal Digital, Teori Informasi dan Pengkodean, Saluran Transmisi, Antena dan Propagasi Gelombang, Komunikasi Bergerak dan Nirkabel, Sistem dan Jaringan Komunikasi, Teknologi Jaringan Telekomunikasi, Sistem Otomatisasi, dsb. TEKNIK INDUSTRI antara lain: Ilmu Ergonomi Industri, Industri Pertahanan, dsb. TEKNIK DIRGANTARA antara lain: Ilmu-ilmu Aeronautika dan Astronautika, Aerodinamika, Struktur Pesawat Terbang, Propulsi, Mekanika Terbang, Material Pesawat Terbang, Astrodinamika, Aeroelastisitas, Aeroakustik, Sistem Pesawat Terbang, Proses Desain dan Produksi Pesawat Terbang, dan Sistem Operasi Penerbangan, dsb. TEKNIK KIMIA antara lain: Kimia bahan eksplosif, Kimia logam, Kimia Industri TEKNOLOGI INFORMASI & KOMUNIKASI antara lain: Sistem Informasi, Rekayasa Perangkat Lunak, Arsitektur Komputer, Jaringan Komputer, Security & Cryptography, Mobile & Cloud Computing, Quality of Service (QoS), Network Programming, Remote Sensing & GIS, Pemodelan dan Simulasi, Multimedia Processing, Teknologi Informasi dan Aplikasi, Big Data, dsb. DRONE & ROBOTIKA antara lain: Control theory and applications, embedded system, mechatronic and robotic, Unmanned Aerial System (UAS), mobile robotics, artificial intelligent, neural network, fuzzy logic, intelligent system, swarm intelligent, genetic algorithm, soft robotic, dsb. CYBER antara lain: Teknik Hacking, Cyber Defense, Cyber Security, Cyber Attack System, dsb.
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200 Documents
<![CDATA[ANALISIS KEKUATAN TARIK BOLTED JOINT STRUKTUR KOMPOSIT SANDWICH HIBRID RAMI-E-GLASS/EPOXY DENGAN CORE KAYU BALSA ]]>
<![CDATA[Banowati, Lies]]>;
<![CDATA[Pratama, Yuda Rizki]]>
<![CDATA[ Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (SENASTINDO) Vol. 4 (2022): Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (Senastindo) ]]>
Publisher : <![CDATA[Akademi Angkatan Udara ]]>
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DOI: 10.54706/senastindo.v4.2022.164
<![CDATA[Seiring dengan perkembangan dunia industri, kebutuhan material untuk sebuah produk semakin meningkat. Para ilmuan berlomba-lomba untuk menciptakan material baru yang lebih kuat, ringan, tahan terhadap korosi, dan biaya material yang murah, salah satu material baru yang banyak dikembangkan adalah komposit. Komposit sandwich merupakan salah satu jenis komposit struktur yang memeliki berat yang relatif ringan namun mempunyai kekakuan dan kekuatan yang tinggi. Penelitian ini bertujuan untuk mengetahui kekuatan tarik dari struktur komposit bolted joint sandwich hibrid rami E-glass/epoxy dengan core kayu balsa yang mengacu pada standar ASTM (American Society for Testing Material) D 5961. Metode manufaktur spesimen komposit yang digunakan adalah hand lay-up dan vacuum bangging dengan variasi arah serat 0°, WR 0/90°, dan WR ±45°. Hasil dari analisis komposit bolted joint sandwich hibrid rami E-glass/epoxy dengan core kayu balsa menunjukkan bahwa kekuatan tarik terbesar hingga yang terkecil yaitu pada arah serat WR ±45° dengan rata-rata sebesar 13,05 MPa, arah serat WR 0/90° rata-rata sebesar 12,41 MPa, dan tekecil yaitu pada arah serat 0° dengan rata-rata sebesar 8,09 MPa.]]>
<![CDATA[Analisis Pengaruh Bentuk Wing Tip Terhadap Performa Aerodinamika Sayap Pesawat Terbang Radio Controlled Menggunakan Ansys 2022R1 ]]>
<![CDATA[Firmanto, Bondhan]]>
<![CDATA[ Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (SENASTINDO) Vol. 4 (2022): Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (Senastindo) ]]>
Publisher : <![CDATA[Akademi Angkatan Udara ]]>
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DOI: 10.54706/senastindo.v4.2022.165
<![CDATA[As is the case with actual aircraft production, model aircraft are made in several stages. One of the most important stages in the manufacture of an aircraft is designing the wings and testing their aerodynamic performance. The wing is the main part of the aircraft because it is the part of the aircraft that produces the most lift. Likewise, in the manufacture of model aircraft, the aerodynamic performance of the wings needs to be designed and analyzed so that the aircraft can fly stably and show optimal aerodynamic performance. In this study, three variations of the shape of the NACA2812 wing tip will be analyzed to determine the optimal aerodynamic performance. Aerodynamic analysis was performed numerically using the ANSYS 2022R1 software package. The compute domain was created using the ANSYS DesignModeler software. 3D wing model with NACA2812 airfoil. Mesh was created using ANSYS Meshing software. Simulation using ANSYS Fluent software. The turbulence model used is k-omega SST in transient, incompressible, subsonic, and sea level conditions. The simulation is run at a speed of 8.33 m/s and an angle of attack of 0°. The analysis focuses on the aerodynamic performance of the CL, CD, CL/CD, and visualization of fluid pressure around the wing. The results of the analysis show that the infinite wing tip design produces a lift coefficient value of 0.249437106, a drag coefficient value of 0.032376252, and a lift to drag ratio of 7.704323091 (the lowest value of lift to drag ratio). The design of the cut off wing tip produces a lift coefficient value of 0.292337624, a drag coefficient value of 0.025722932, and a lift to drag ratio value of 11.36486404. The aft swept wing tip shape design produces a lift coefficient value of 0.322231093, a drag coefficient value of 0.027981121, and a lift to drag ratio value of 11.51601789 (the highest lift to drag ratio value). Therefore, the design of radio controlled aircraft will use a wing design with an aft swept wing tip shape.]]>
<![CDATA[Rancang Bangun Content Management System Pada Website Riset Fakultas Teknik Universitas Nurtanio Menggunakan Bahasa Pemrograman PHP Dan MySQL ]]>
<![CDATA[Ali, Abdul Latif]]>;
<![CDATA[Satyawan, Arief Suryadi]]>;
<![CDATA[Wulandari, Ike Yuni]]>;
<![CDATA[Puspita, Heni]]>
<![CDATA[ Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (SENASTINDO) Vol. 4 (2022): Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (Senastindo) ]]>
Publisher : <![CDATA[Akademi Angkatan Udara ]]>
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DOI: 10.54706/senastindo.v4.2022.168
<![CDATA[The development of information and communication technology has had a major impact on human life along with the easier it is to obtain information through the internet. The need for the internet is very high, especially in the world of education and especially universities. The emergence of internet technology that exists today has become a tool used to ease human work, especially in the field of websites. Website is a form of implementation of a programming language. Hypertext Preprocessor (PHP) is a web-based programming language that has the ability to process and process website data that is run by the MySQL server as a database. One that can be used for dynamic website creation is content management system (CMS) technology. This website design aims to make it easier for admin managers and kontributors to provide more interactive information to research students and lecturers in developing an autonomous electric vehicle website. This study uses a system development method in the form of a Software Development Life Cycle (SDLC) with a prototype model, namely software development in the form of a physical system work model and functions as an initial version of the system. In testing the CMS using black-box testing with boundary value analysis techniques that focus on input and output data. Based on the research and testing process that has been carried out successfully, the CMS dashboard page on the engineering faculty research website is able to process data dynamically and provide convenience for admin managers and kontributors in the development of autonomous electric vehicles.]]>
<![CDATA[Pemilihan Pangkalan Induk Skadron Pesawat Tempur TNI AU dengan Menggunakan Metode Analytical Hierarchy Process ]]>
<![CDATA[Riano, Gagat]]>;
<![CDATA[Pradhypta, Aura]]>
<![CDATA[ Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (SENASTINDO) Vol. 4 (2022): Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (Senastindo) ]]>
Publisher : <![CDATA[Akademi Angkatan Udara ]]>
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DOI: 10.54706/senastindo.v4.2022.169
<![CDATA[Determining a location where the facility will be built is one of the important factors in the business and military planning process. Indonesia, as a country that has a large area, has problems in determining the right location to place its squadron of fighter aircraft in the national defense system. This study uses the Analytic Hierarchy Process (AHP) to solve this problem. There are five criteria considered in this study, namely deterrence strategy, counterbalance strategy, flight support facilities, base support facilities and the environment. This research is aimed at getting six out of 10 Indonesian Air Force air bases that meet the requirements to be placed in a squadron of fighter aircraft. The six air bases selected were SPO (15.17%), RSN (15.16%), HND (12.25%), HLM (12.16%), ABD (10.09%) and IWJ (10.07% ).]]>
<![CDATA[Location Optimization of The Fighter Squadron in The National Air Defense System ]]>
<![CDATA[Ar Rifky R, Hakim]]>;
<![CDATA[Aprilia, Sherly]]>;
<![CDATA[Riano, Gagat]]>
<![CDATA[ Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (SENASTINDO) Vol. 4 (2022): Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (Senastindo) ]]>
Publisher : <![CDATA[Akademi Angkatan Udara ]]>
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DOI: 10.54706/senastindo.v4.2022.170
<![CDATA[This study uses the set covering problem (SCP) method to optimize the placement of the F-16 Fighting Falcon fighter in the national air defense system (Sishanudnas). Then the results of the SCP maximize the covering ability by minimizing the average distance between air bases with the P-Median Problem (PMP). The results of this study indicate that the Indonesian Air Force needs nine squadrons of F-16s, to be able to cover all of Indonesia's airspace. However, if the requirements are to include a base that currently operates fighter aircraft as a location for squadron placement, the Indonesian Air Force needs 11 squadrons of F-16 aircraft.]]>
<![CDATA[Rekontruksi Pembelajaran Komunikasi Digital Modulasi QPSK dengan Rewiring Modicom 5/1 dan Modicom 5/2 ]]>
<![CDATA[Pambudi, Wisnu Setyo]]>;
<![CDATA[Setiawan, Rudi]]>
<![CDATA[ Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (SENASTINDO) Vol. 4 (2022): Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (Senastindo) ]]>
Publisher : <![CDATA[Akademi Angkatan Udara ]]>
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DOI: 10.54706/senastindo.v4.2022.171
<![CDATA[Communication systems are very decisive in modern warfare, the use of long-range weapons without crew requires a long-distance communication system using digital modulation communication. One of the basics of digital modulation communication that is important is QPSK modulation, so the Department of Electronics develops learning by conducting research on QPSK modulation and demodulation by conducting research on series block systems built on Modicom 5/1 and Modicom 5/2. Modicom 5/1 consists of blocks, namely the separation of serial data into MSB and LSB data, Unipolar to bipolar converters, Modulator I and Modulator Q and the summation of the Op-Amp. The Modicom 5/2 consists of a QPSK detector, a two-order filter, a comparator and a decoder differential. The results of the study prove that serial data from modicom 3/1 is in the form of serial data (D0,D1,D2,D3,D4,D5) separated by MSB data separator blocks (D0,D2,D4) and LSB (D1,D3,D5), serial data MSB and LSB (unipolar data standard (0V/+5V)) are converted to bipolar standard digital data (-4V/+4V) by a unipolar to bipolar converter block system. Balance Modulator (IC 1496) with MSB signal input ( I ) on modulator 1 carrier frequency of 960kHz (∟0º) and 960 kHz (∟-180º) on modulator 2 is LSB (Q) will output data in the form of an analog sine signal with a frequency of 960 KHz with different phase according to carrier signal '0'=∟-90º or '1'=∟-270 . the sum of the Module I and Q signal modules into phase angles of 00(45º),10(135º),11(225º), 01 (315º). The QPSK detector by means of the information signal is generated 4 times, the phase is detected (IC PLL) then divided by 4 , phase difference angle as control switch signal I and Q to get signal I and signal Q . The I and Q signals are filtered by fourth order butterworth then the I and Q signal data as comparator inputs to get a logic 0 or 1. Data I and O as logic data (0/1) as MSB and LSB data are combined again into discrete serial data with blocks differential decoder by using the PISO register (parallel input serial output) using IC 17HC175.]]>
<![CDATA[Efek Lapisan Batas (Boundary Layer) pada Skin Friction Drag ]]>
<![CDATA[Purwadi, Purwadi]]>
<![CDATA[ Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (SENASTINDO) Vol. 4 (2022): Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (Senastindo) ]]>
Publisher : <![CDATA[Akademi Angkatan Udara ]]>
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DOI: 10.54706/senastindo.v4.2022.173
<![CDATA[Telah dilakukan penelitian terhadap pengaruh lapisan batas (boundary layer) terhadap koefisien Skin Friction Drag. Percobaan dilakukan dengan cara mengalirkan variasi kecepatan aliran pada permukaan pelat halus dan kasar, lalu dibandingkan bagaimana karakter lapisan batas dan kaitannya dengan koefisien Skin Friction Drag Cf. Masalah yang diteliti adalah bagaimana ketebalan lapisan batas terhadap variasi kecepatan aliran, besarnya perbedaan antara tebal lapisan teoritik dan real yang diukur, besarnya bilangan Reynold Re pada pelat pada jarak dari leading edge terhadap variasi kecepatan aliran serta bagaimana efek variasi kecepatan terhadap nilai Cf. Didapatkan bahwa tebal lapisan batas untuk pelat kasar memang lebih tebal dibandingkan dengan pelat halus.Variasi kecepatan pada pelat halus dan kasar sama sama menunjukkan sifat aliran laminar dengan nilai Re dibawah 500000, sedangkan yang berkarakter turbulen ditemukan pelat halus dengan kecepatan 30,98 m/s di titik 25 cm. Nilai Cf cenderung menurun untuk kecepatan menaik untuk pelat halus dengan aliran laminar dan naik pada saat kecepatan 30,98 m/s. Sedangkan nilai Cf untuk pelat kasar mengalami penurunan juga untuk kecepatan naik hingga 30,98 m/s. Disarankan penelitian dilakukan dengan variasi kecepatan yang lebih tinggi dari 30,98 m/s untuk memahami perilaku Cf pada pelat halus dan kasar untuk kecepatan yang lebih tinggi terutama yang aliran termampatkan dengan kecepatan sekitar 100 m/s.]]>
<![CDATA[Prediksi Usia Simpan Amunisi Kaliber Kecil dan Uji Performa Balistiknya: Studi Di Gudang Senjata AAU ]]>
<![CDATA[Jati, Rhestu Pradhipta]]>;
<![CDATA[La Ore, Muhammad Sakti]]>
<![CDATA[ Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (SENASTINDO) Vol. 4 (2022): Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (Senastindo) ]]>
Publisher : <![CDATA[Akademi Angkatan Udara ]]>
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DOI: 10.54706/senastindo.v4.2022.174
<![CDATA[Research has been carried out on small caliber ammunition (MU1-JHP, MU2-TJ, and MU5-TJ) produced by PT. Pindad to predict the remaining shelf life of ammunition with the propellant stability test method and calculate the shelf life using the Berthelot equation. In addition, ballistic performance tests are also carried out to determine the feasibility of ammunition with predetermined specification standards. From the research results showed that on the MU1-JHP ammunition caliber 9 mm 2010 (the oldest lot number in stock in the warehouse for the same type) and lot number 2015 (youngest) was predicted that the remaining shelf life was 14.69 and 16.16 years, respectively. The MU2-TJ ammunition caliber 7.62 mm lot number 1992 (oldest) and 1994 (youngest) was predicted the remaining shelf life was 4.41 years and 5.88 years, respectively. The MU5-TJ ammunition caliber 5.56 mm lot number 2015 (oldest) and 2017 (youngest) was predicted to have a remaining shelf life of 19.10 years and 11.75 years, respectively. The results of the ballistic performance test (gas pressure, speed and accuracy) of small caliber ammunition on the MU1-JHP ammunition caliber 9 mm lot number 2010 and 2015 both still meet the standard specifications. The ballistic performance of the MU2-TJ ammunition caliber 7.62 mm lot number 1992 and 1994 both did not meet the specifications. The ballistic performance of the MU5-TJ ammunition caliber 5.56 mm lot number 2015 and 2017 both still meet the standard specifications.]]>
<![CDATA[IMPLEMENTASI GAME THEORY PADA PEMILIHAN METODE PEMBELAJARAN YANG TEPAT BAGI TARUNA AAU ]]>
<![CDATA[Pudjianto, Agus]]>
<![CDATA[ Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (SENASTINDO) Vol. 4 (2022): Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (Senastindo) ]]>
Publisher : <![CDATA[Akademi Angkatan Udara ]]>
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DOI: 10.54706/senastindo.v4.2022.180
<![CDATA[The Air Force Academy is one of the highest educational institutions in the Indonesian Air Force which is tasked with producing Indonesian Air Force officers who have good personalities, qualified academic abilities, supported by excellent physical abilities in accordance with the slogan "Tri Sakti Viaratama". In supporting learning activities, collaboration between lecturers and cadets is required to achieve learning objectives. There are 3 types of learning methods applied, namely: Conventional, Discussion and demonstration. By using game theory, it will be seen what method is most suitable to be applied in AAU.Of the three types of competition in the game above, it produces different game values and strategy probabilities with varying game values. But the biggest game value, 3.68, was found in the third competition, namely between Demonstration and Conventional. This shows that the majority of respondents do not like the Discussion learning strategy. But prefers Demonstration and Conventional strategies]]>
<![CDATA[PENGAMANAN DATA MENGGUNAKAN EMAIL TERENKRIPSI DI AKADEMI ANGKATAN UDARA ]]>
<![CDATA[Fahrurozi, Muhammad]]>;
<![CDATA[Ridho, Mavel]]>;
<![CDATA[Setiyono, Setiyono]]>
<![CDATA[ Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (SENASTINDO) Vol. 4 (2022): Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (Senastindo) ]]>
Publisher : <![CDATA[Akademi Angkatan Udara ]]>
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DOI: 10.54706/senastindo.v4.2022.182
<![CDATA[Confidentiality of information and communication to protect sensitive data is an absolute thing and must be fulfilled when this will not exist in the military world. Confidentiality of data in exchanging information will protect institutions from unwanted things. As a military educational institution, the Air Force Academy requires a data security system to guarantee an institution. In securing data, confidentiality and security remain, namely confidentiality, integrity and availability so that the information content is maintained. The rapid development of data security tools, one of which uses the Pretty Good Privacy method. This system uses yahoo RSA cryptographic techniques to protect data sent via email. Several AAU work units that use the PGP method in carrying out e-mail data exchange are the financial unit, the health unit and the personnel unit that manages human resources. This PGP method can protect data or information on email. This technique is expected to be the first step in data security at the Air Force Academy]]>
