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Kurniawan
National Air and Space Power Center Of Indonesia
Aerospace Engineering Earth & Planetary Sciences Electrical & Electronics Engineering Engineering Environmental Science

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DESIGN OF AN IOT-BASED REMOTE MONITORING SYSTEM FOR YOGYAKARTA AIRPORT LOCALIZER WITH AUTOMATIC CHANGEOVER AND REAL-TIME NOTIFICATION FEATURES Oki Tri Rizki; Muchammad Furqon; Rakin Ghiyat; Kurniawan; Rayhan Kemal; Tia Tsania
Jurnal TNI Angkatan Udara Vol 5 No 1 (2026): Jurnal TNI Angkatan Udara Triwulan Pertama
Publisher : Staf Komunikasi dan Elektronika, TNI Angkatan Udara

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.62828/jpb.v5i1.188

Abstract

This research on remote monitoring design aims to determine the condition and control the Localizer equipment in normal or alarm conditions. It can also assist in changing over during ground checks, accessible via smartphone using the Blynk app. This design uses an optocoupler sensor to detect the electrical current flowing through the LEDs on the Localizer Remote Control Unit (RCU). This allows the indicator readings to be sent to the Internet of Things (IoT) using a NodeMCU Wi-Fi module that communicates serially with an Arduino. The IoT functions to display real-time conditions and control the Localizer equipment in normal or alarm conditions, accessible via smartphone using the Blynk app. The tool I will design is an Internet of Things-based remote monitoring localizer. It is hoped that this remote monitoring tool will facilitate technicians in determining the condition of the Localizer and assist in changing over during ground checks.
PNEUMATIC TEMPERATURE SENSOR FAILURE ANALYSIS P/N 767C0000-01 ON AN AIRBUS 330-300 AIRCRAFT AT PT GMF AEROASIA Muhammad Ghani; Al Hafidz; Ego Widoro; Benny Kurniantoi; Muchammad Furqon; Kurniawan; Tia Dikatama
Jurnal TNI Angkatan Udara Vol 5 No 1 (2026): Jurnal TNI Angkatan Udara Triwulan Pertama
Publisher : Staf Komunikasi dan Elektronika, TNI Angkatan Udara

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.62828/jpb.v5i1.193

Abstract

This study aims to analyze the causes of sensor failure at PT GMF AeroAsia Tbk. The methodology used was observation, interviews, and document analysis. Modern aircraft rely heavily on reliable support systems, including pneumatic systems for regulating cabin temperature and safety. On an Airbus A330-300, a problem with the pneumatic temperature sensor was found, with corrosion on the sensor rod resulting in inaccurate temperature readings that could impact flight safety. This study aimed to analyze the causes of sensor failure at PT GMF AeroAsia Tbk. The methodology used was observation, interviews, and document analysis. Data were analyzed using Pareto charts and Fault Tree Analysis to identify the root cause. The results indicated that corrosion was the primary cause, exacerbated by environmental factors, weak inspection procedures, and a lack of technician understanding. In conclusion, the sensor failure was caused by a combination of technical, procedural, and human factors. This research helps develop better aircraft maintenance strategies to improve safety.
THE ROLE OF AIR POLICING IN ACHIEVING AIR SUPERIORITY: AN ANALYSIS WITH NATO AIR POLICING CASE STUDY Andri Gandhy; Suroso; Andrianto; Kurniawan; Dikatama Tsania; Muchammad Furqon
Jurnal TNI Angkatan Udara Vol 5 No 2 (2026): Jurnal TNI Angkatan Udara Triwulan Kedua
Publisher : Staf Komunikasi dan Elektronika, TNI Angkatan Udara

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.62828/jpb.v5i2.207

Abstract

Air policing serves as a critical mechanism for maintaining airspace integrity within nations or alliances, directly contributing to air superiority in military defense contexts. This paper analyzes the role of air policing in establishing and sustaining air dominance, focusing on the NATO Air Policing case study. Employing qualitative and quantitative approaches, including literature review, historical data, statistical tables, and graphs, we explore how air policing functions as deterrence, rapid response, and a foundation for broader military operations. The NATO case since 2004 demonstrates over 300 annual interceptions in recent periods, reinforcing alliance solidarity and preventing conflict escalation. In-depth analysis, enhanced by Analytic Hierarchy Process (AHP) for prioritizing factors, Monte Carlo simulations for risk assessment, and relevant theories such as deterrence theory and air power theory, reveals air policing as a strategic element supporting modern military doctrines where air superiority is prerequisite for ground and naval operations. Findings emphasize the integration of advanced technologies like radar and fifth-generation fighters to enhance effectiveness. This paper concludes that air policing is a foundational pillar for air superiority, with implications for global defense policies in geopolitical tensions.
ECONOMIC ASYMMETRY IN DRONE WARFARE A CASE STUDY OF IRAN'S SHAHED-136 OPERATION AGAINST ISRAEL'S IRON DOME DEFENSE SYSTEM Ahmad Ilham Kamal; Muchammad Furqon Muchaddats; Ferdy Anggrian; Andromeda; Yoga Pratama; Riza Suseno; Kurniawan; Dikasitama
Jurnal TNI Angkatan Udara Vol 5 No 2 (2026): Jurnal TNI Angkatan Udara Triwulan Kedua
Publisher : Staf Komunikasi dan Elektronika, TNI Angkatan Udara

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.62828/jpb.v5i2.210

Abstract

The advent of low-cost loitering munitions has revolutionized modern warfare,creating a profound economic imbalance between offensive and defensive capabilities. In the Middle East, the deployment of Iran's Shahed-136 drone against Israel's Iron Dome defense system serves as a prime example of a "cost-imposing" strategy in asymmetric warfare. Objective: This study aims to quantify the economic disproportion between the production and deployment costs of the Shahed-136 drone and the operational costs of the Iron Dome system. It explores how this cost ratio impacts long-term national defense budgets andstrategic sustainability. Methodology: This study uses a qualitative-descriptive approach supported by comparative economic modelling. Data are synthesized from defense budget reports, estimates of the Shahed-136 manufacturing costs, and the unit cost of the Iron Dome Tamir interceptor missile. The analysis uses the Cost- xchange Ratio (CER) to evaluate the economic efficiency of both sides. Results: The study's findings reveal a sharp economic asymmetry, with a single Shahed-136 estimated to cost between $20,000 and $50,000, depending on configuration, while a single Tamir interceptor missile costs approximately $40,000 to $100,000, depending on configuration. When factoring in "saturation attacks" (ordrone swarms), defense costs increase exponentially, not only through missile expenditure but also through the economic disruption caused by airstrike warnings and collateralinfrastructure damage if interceptions fail. Conclusion: The study concludes that while Iron Dome remains tactically effective in saving lives, its current economic trajectory is unsustainable against the threat of low-cost, mass-produced drones. The study suggests that to maintain strategic stability, the defense framework must transition to lower-cost interception technologies, such as directed energy weapons (lasers/Iron Beam), to neutralize the economic advantage currently held by offensive drone platforms.
EXPERIMENTAL FIGHTER AIRCRAFT GROUND MANEUVER SIMULATION Ida Farida; Kukuh Prasetyo; Eka Irianto Bhiftime; Nick Holson Manggiring Silalahi; Ahmad Hasan Fauzi; Kurniawan; Tia Dikatama Tsania
Jurnal TNI Angkatan Udara Vol 5 No 2 (2026): Jurnal TNI Angkatan Udara Triwulan Kedua
Publisher : Staf Komunikasi dan Elektronika, TNI Angkatan Udara

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.62828/jpb.v5i2.211

Abstract

This study aims to explore and analyze various factors that affect ground maneuvers on fighter aircraft, focusing on the steering system and landing gear design. Fighter aircraft, as a major component in military operations, must not only have optimal air maneuverability, but also be able to maneuver on the ground effectively and efficiently. The ability to move quickly and precisely on the ground is essential. Precise ground maneuvers not only ensure the safety of the aircraft, but also affect operational efficiency and response time in dealing with emergency situations. In this study, simulations were conducted using a mathematical model developed in MATLAB/Simulink software to model and analyze aircraft movements during the ground operation phase. This model considers various important parameters such as aircraft speed, nose landing gear deflection, and weight distribution settings to obtain more accurate results. The results of this simulation show that changes in the nose landing gear deflection affect aircraft movements, including the ability to change direction with a smaller radius and shorter time. Thus, the results of this study are expected to provide new insights into fighter aircraft design to improve ground maneuver performance and improve fighter aircraft operational efficiency in various field conditions.
Co-Authors Ahmad Hasan Fauzi Ahmad Ilham Kamal Al Hafidz Andri Gandhy Andrianto Andromeda Benny Kurniantoi Dikasitama Dikatama Tsania Ego Widoro Eka Irianto Bhiftime Ferdy Anggrian Ida Farida Kukuh Prasetyo Muchammad Furqon Muchammad Furqon Muchammad Furqon Muchammad Furqon Muchaddats Muhammad Ghani Nick Holson Manggiring Silalahi Oki Tri Rizki Rakin Ghiyat Rayhan Kemal Riza Suseno Suroso Tia Dikatama Tia Dikatama Tsania Tia Tsania Yoga Pratama