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All Journal Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (Senastindo)
Arief Suryadi Satyawan
Badan Riset dan Inovasi Nasional, Universitas Jambi
Computer Science & IT Control & Systems Engineering Engineering Mechanical Engineering Other

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Pembuatan Sistem Informasi Untuk Kendaraan Listrik Otonom Berbasis Website Aprillia Damayanti; Denden Mohamad Arifin; Ardian Infantono; Arief Suryadi Satyawan; Mohammed Ikrom Asysyakuur; Ema Ema; Raden Aditya Satria Nugraha
Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (SENASTINDO) Vol 3 (2021): Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (Senastindo)
Publisher : Akademi Angkatan Udara

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (689.663 KB) | DOI: 10.54706/senastindo.v3.2021.144

Abstract

Current developments have made website technology a means of disseminating information that offers various conveniences and speeds in its presentation. Speed ​​and convenience are positive values ​​of the existence of the internet. The website is more easily accessible by people in various regions just by using the internet. One of them is in terms of marketing the product of a business, the website can be a means of promoting, marketing and conveying information effectively and efficiently to the public. One of the things that can be utilized from website technology is for information purposes of autonomous electric vehicles. This vehicle technology in the future can be integrated on the website for the purpose of information on its existence and condition. In fact, it is possible to create applications for the use of autonomous electric vehicles by making calls through the website, as is the case with applications that are currently popular, namely Gojek or Grab. In this study, a web application was developed for the purposes of a simple autonomous electric vehicle, which operates in the Nurtanio University Bandung campus environment. This website design consists of five pages. The first page contains a homepage where general information on research activities for the development of simple autonomous electric vehicles is found. The second page contains object detection which displays more detailed information about the object detection technology used in autonomous electric vehicles. Information on the existence of autonomous electric vehicles in the campus environment is then shown on the third page, namely Av Tracker. This website design is also equipped with a contributor page (page four) which contains researchers involved in autonomous electric vehicle research. At the end, the fifth page is for contact information for those who are interested in communicating further about matters related to this research. This website design uses a markup language consisting of HTML and CSS, besides that PHP and MySQL programming languages ​​are also used as databases.
Research Civil Aircraft Model (RCAM) Dengan Metode Dinamis 6 Derajat Kebebasan Menggunakan MATLAB Aulia Widya Prameswari; Arief Suryadi Satyawan; Denden Mohamad Ariffin
Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (SENASTINDO) Vol 3 (2021): Prosiding Seminar Nasional Sains Teknologi dan Inovasi Indonesia (Senastindo)
Publisher : Akademi Angkatan Udara

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (655.245 KB) | DOI: 10.54706/senastindo.v3.2021.152

Abstract

The Aircraft Model is an attempt to create or simulate an actual aircraft and this model can be called the Research Civil Aircraft Model (RCAM), which is a twin-engine civil aircraft model developed by the Group for Aeronautical Research and Technology in Europe (GARTEUR). This aircraft model is similar to the Boeing 757-200. Research Civil Aircraft Model created using 6 degrees of freedom. 6 degrees of freedom consist of 3 translations, namely 3 degrees for Cartesian coordinates on the axis (x,y,z) and 3 rotations, namely 3 degrees (pitch, roll, and yaw) which are used to control surface deflection and throttle position. To create a model, parameters are needed, namely the parameters of the mass of the aircraft and the parameters of the aero chord and also the CoG (Center of Gravity) of an aircraft. The algorithm entered comes from control limits/Saturation, Intermediate Variables, Force Coefficients, Moment Coefficients, Propulsion Effects, Gravity Effects until finally simulated using "Simulink" in MATLAB. In order to produce not only graphics, animation is needed to see the attitude of the aircraft, so 3D Animation is used in MATLAB. The results of this civil aircraft modeling are to see a simulation of the stability of the ailerons, rudders, elevators, and throttles when the plane is flying. The results can vary because in 3D Animation, the plane can be controlled from the plane's attitude when tilted right or left and also when the plane rolls. With this, it is hoped that the simulation can be effective in seeing the actual results when the plane is flying and can also be used as a simulator before the plane takes off.
Co-Authors Aprillia Damayanti Aulia Widya Prameswari Denden Mohamad Ariffin Denden Mohamad Arifin Ema Ema Infantono, Ardian Mohammed Ikrom Asysyakuur Raden Aditya Satria Nugraha