cover
Article Per Year (5 Year)
All
Home Page
OAI Link
Editorial Team
Contact
Reviewer
Google Scholar
Contact Name
Irza Sukmana
Contact Email
irza.sukmana@eng.unila.ac.id
Phone
+6281294836432
Journal Mail Official
irza.sukmana@eng.unila.ac.id
Editorial Address
DOPP Research Group FTMD – ITB Labtek II, 2nd Floor | Jl. E-ITB / Jl. Ganesha 10, Bandung, 40132
Location
Kota bandung,
Jawa barat
INDONESIA
International Journal of Aviation Science and Engineering
Published by Institut Teknologi Bandung
ISSN : 27215342     EISSN : 27156958     DOI : https://doi.org/10.47355/avia.v1i1.6
Core Subject : Engineering,
Aerospace Engineering Automotive Engineering Electrical & Electronics Engineering Mechanical Engineering Transportation
AVIA : International Journal of Aviation Science and Engineering is published by Faculty of Mechanical and Aerospace Engineering, FTMD Institut Teknologi Bandung, Indonesia - in cooperation with Faculty of Engineering, Universitas Lampung and Java Scientific Academy, Indonesia. International Journal of Aviation Science and Engineering aims to publish original research articles and critical review manuscript in the field of Aviation Science and Engineering as well as Aerospace and applied Mechanical Engineering. The topics are including, but limited to: aviation sciences and technology, aerospace engineering, aeronautics, defense system and engineering, safety and energy, mechanical engineering, aeronautics education and training, interdisciplinary engineering and applied sciences.
Arjuna Subject : Teknik (semua kategori) - Teknik Ruang Angkasa
Articles 5 Documents
 1 
Search results for , issue "Vol 3, No 2: (Dec, 2021)" : 5 Documents clear
Required Navigation Performance (RNP) Analysis for ADS-B Data of Makassar-Jakarta Flight using Dot Product Method N Ruseno; A Putra
AVIA Vol 3, No 2: (Dec, 2021)
Publisher : Institut Teknologi Bandung

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.47355/avia.v3i2.50

Abstract

Required Navigation Performance (RNP) is known as a performance parameter for a navigation system, where its function is to keep an aircraft within a certain radius of containment. During the flight, an aircraft transmits its real-time location-based on Global Navigation Satellite Systems (GNSS) technology via Automatic Dependence Surveillance Broadcast (ADS-B) protocol. However, there are questions about the flight position accuracy. This research aims to analyze the accuracy of ADS-B flight data about RNP requirements. The flight data used is gathered from the FlightRadar24 website and filtered for each flight phase. The selected route used is Makassar (UPG) – Jakarta (CGK) because the route has the highest number of flights per week. The Dot Product method is proposed to calculate the distance between the flight trajectory to the line of flight procedure towards the destination airport. The analysis is conducted based on the compliance of the flight data to the RNP threshold. It is concluded that the majority of evaluated flights in the selected route fly within the RNP boundary. However, some non-complying flights become within the RNP boundary when they are evaluated with other possible published procedures
Conceptual Design of Unmanned Piston-Propeller Cargo Aircraft F F H B Wiarso; B D Febriansyah; G A Gintings; R D Muhammad; H Muhammad
AVIA Vol 3, No 2: (Dec, 2021)
Publisher : Institut Teknologi Bandung

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.47355/avia.v3i2.51

Abstract

The need for a transportation system to transport goods is increasing, especially for regions in Indonesia that are included in the leading, remote, and disadvantaged (3T) categories. This paper will discuss the conceptual design of an unmanned cargo aircraft with a piston-propeller engine which can later be operated in the 3T area. The design will begin with a discussion of DRO, followed by a concept of the aircraft configuration. After the configuration is formed, the aerodynamic characteristics will be calculated, the weight will be predicted, and flight performance calculations and aircraft stability will be calculated
Enhancement of Human Sensory and Motor Skills using Collaboration of Eye - Ear Focus and Body - Arm - Hand Gesture in No-Touch 3D Interactive Aircraft Game A Infantono; R Ferdiana; H Hartanto; B Zurianto
AVIA Vol 3, No 2: (Dec, 2021)
Publisher : Institut Teknologi Bandung

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.47355/avia.v3i2.52

Abstract

Nowadays, human sensory and motor skills enhancement is very important to be alert from the effect of the Society 5.0 era. We propose the novel approach to enhance human sensory and motor skills using collaboration of senses focus and body parts gesture in no-touch3D interactive aircraft game. A player interacts with a virtual display using gestures of his body, arm, hand, or collaboration of them as a controller to engage in a 3D game. This game is based on an aircraft education theme. By sweeping the hand to the left or right, a player can select one of many different aircraft models according to its specification and performance are shown on the screen based on the estimation of his current skill. The mission is to control aircraft avoiding the random balls attack to prevent a collision. Hand and arm are positioned above a leap motion sensor and in front of a camera. The body, arm, and hand gesture directions are to forward or backward from the screen to the right or left, and also to up or down freely. This system is developed by using Unity 3D, OpenCV, and Python. Many skills are possible to be improved, e.g., motivation, discipline, safety awareness, endurance management, strategy, precision, intelligence, creativity, reliability, toughness, and vision. This project has been tested in the Air Force Museum of Dirgantara Mandala involving more than 1000 visitors as testing participants, and they all feel satisfied. The score is calculated by time in second. The results show endurance time is 32% (<60 s), 31% (<120 s), 25% (<160 s), and 12 % (180 s) of the total300 seconds of the game
Development of an Aerial Fire Identification System Based on Visual Artificial Intelligence H Afifa; K Ummah; J Sembiring
AVIA Vol 3, No 2: (Dec, 2021)
Publisher : Institut Teknologi Bandung

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.47355/avia.v3i2.48

Abstract

To reduce losses due to fire, it is necessary to extinguish and rescue immediately. However, in the dense area fire trucks were unable to reach the fire site due to narrow road access. In this case, drones that can fly by themselves to the point of fire then release fire-fighting bombs automatically can help fire disaster management. This means it needs a system where it can identify whether there is a fire. This study explores the idea of identifying fire using computer vision approach by making 8 identification models with each dataset of day, night, day, and night, thermal, day filter, night filter, day and night filter, and thermal filter, which had been tested by a set of data that corresponded to each dataset. YOLOv4 algorithm and Google Colaboratory were used, where each model took 8-10 hours to be trained. Results show that the day and night model was the most robust by having the highest average F1-score, 0.37. And will be performing the best on thermal data test with the value of F1-score is 0.6. This can be a representation for exploring new ideas on further study of how to obtain the most suitable dataset and data test.
Design Modification of the Horizontal Tail and Performance Simulation of LSU-05NG Drone A Vianto; S Tobing; K Hidayat
AVIA Vol 3, No 2: (Dec, 2021)
Publisher : Institut Teknologi Bandung

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.47355/avia.v3i2.49

Abstract

LSU-05NG is a drone manufactured and developed by LAPAN. The horizontal tail of the aircraft is used to maintain longitudinal stability, however, there has been no study on a tail modification that could improve the performance. The study of tail modification will examine the impact of modifying the airfoil to NACA 2412 and NACA 63-215. The base model of LSU-05NG uses NACA 0012 as the airfoil profile which is used in the horizontal tail. The performance is measured from the value of the lift coefficient, drag coefficient, and longitudinal stability. The results are obtained using ANSYS CFX Software. Based on the study, the modification of the horizontal tail has no impact on the lift and drag coefficient, however, impacts greatly on the pitching coefficient which determines the longitudinal stability. The airfoil profile that produces the highest longitudinal stability is NACA 63-215, followed by NACA 2412, and the last is the basic model using NACA 0012

Page 1 of 1 | Total Record : 5

 1 

Filter by Year

2021 2021


Reset
Filter By Issues
All Issue Vol. 6 No. 2: (December, 2024) Vol. 6 No. 1: (June, 2024) Vol. 5 No. 2: (December,2023) Vol. 5 No. 1: (June 2023) Vol. 4, No. 2 (December 2022) Vol 4, No 1: (June, 2022) Vol 3, No 2: (Dec, 2021) Vol 3, No 1: (June, 2021) Vol. 3 No. 1: (June, 2021) Vol 2, No 2: (Dec, 2020) Vol 2, No 1: (June, 2020) Vol 1, No 1: (Dec, 2019) More Issue