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All Journal Jurnal TNI Angkatan Udara
Eka Irianto Bhiftime
Departemen Teknik Mesin, Fakultas Sains dan Teknologi Pertahanan UNHAN RI,
Aerospace Engineering Earth & Planetary Sciences Electrical & Electronics Engineering Engineering Environmental Science

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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.
STATISTICAL ANALYSIS OF SPACESHIP LAUNCH SUCCESS RATE Ida Farida; Kukuh Prasetyo; Eka Irianto Bhiftime; Victoriano Jonathan Lendeng; Ahmad Hasan Fauzi; Kurniawan; Tia Dikatama Tsania
Jurnal TNI Angkatan Udara Vol 5 No 4 (2026): Jurnal TNI Angkatan Udara Triwulan Keempat
Publisher : Staf Komunikasi dan Elektronika, TNI Angkatan Udara

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.62828/fc401092

Abstract

This research aims to determine and prove the role of international policies and government programs in influencing technical decisions and the impact of successful launches on costs and risk reduction. In recent decades, spacecraft launch success rates have become a critical topic for analyzing the efficiency and technological advancements within the aerospace industry. This study explores historical data regarding spacecraft launch success rates, considering the influence of technical factors, government policies, and advancements in rocket design. By utilizing launch data from various space agencies such as NASA, SpaceX, and Roscosmos, the analysis highlights significant trends in increasing success rates, which align with innovations in technology and policies that support safer and more efficient space exploration. Additionally, this research examines the role of international policies and government programs in influencing technical decisions and the impact of successful launches on cost reduction and risk mitigation. Through statistical analysis and historical data modeling, this study provides in-depth insights into how technology and policy can shape higher success rates in future launches.
Co-Authors Ahmad Hasan Fauzi Ida Farida Ida Farida Kukuh Prasetyo Kukuh Prasetyo Kurniawan Kurniawan Nick Holson Manggiring Silalahi Tia Dikatama Tsania Tia Dikatama Tsania Victoriano Jonathan Lendeng