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All Journal HUKUM BISNIS Teknika STTKD: : Jurnal Teknik, Elektronik, Engine
Andika Wijaya
Unknown Affiliation
Electrical & Electronics Engineering Energy Industrial & Manufacturing Engineering Law, Crime, Criminology & Criminal Justice Materials Science & Nanotechnology Mechanical Engineering

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PERLINDUNGAN HUKUM TERHADAP KREDITOR PEMEGANG JAMINAN FIDUSIA DALAM KEPAILITAN DEBITUR Andika Wijaya; Hendro Juandra; Buyung Ageng Islami; Pius Pati Molan; Cakra P. Octavianus
Jurnal HUKUM BISNIS Vol 4 No 1 (2020): Vol.4 no.1 April 2020
Publisher : Fakultas Hukum Universitas Narotama

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.31090/hukumbisnis.v4i1.1016

Abstract

This study was made to find to find a form of legal protection for Creditors holding fiduciary guarantees in the event that the Debtor is declared bankrupt. Research conducted after the Decision of the Constitutional Court of the Republic of Indonesia Number: 18 / PUU-XVII / 2019 dated January 6, 2020. This decision was carried out in accordance with the fiduciary Guarantee Holder's right to execute objects bound by fiduciary guarantees. This research is a normative juridical study, by statute, conceptual and cases approach. Research contains novelty and original elements, which can be used as a source of reference for Creditors who holding fiduciary guarantees to maximize their right to increase the bankruptcy of the Debtor. Through this research, creditors who receive fiduciary security rights (all financial service institutions both conventional and sharia, such as: banks, finance companies, mortgage companies, etc.) can adjust themselves to bankruptcy procedures without having to violate the provisions of fiduciary guarantee laws that have experienced post-change after Decision of the Constitutional Court of the Republic of Indonesia Number: 18 / PUU-XVII / 2019 dated January 6, 2020.
ANALISIS DAN DESAIN WING UAV VTOL MENGGUNAKAN FINITE ELEMENT ANALYSIS Andika wijaya; Edi Sofyan; Ferry setiawan; Muhammad Kevin Adam
Teknika STTKD: : Jurnal Teknik, Elektronik, Engine Vol 9 No 1 (2023): TEKNIKA STTKD: JURNAL TEKNIK, ELEKTRONIK, ENGINE
Publisher : Sekolah Tinggi Teknologi Kedirgantaraan

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.56521/teknika.v9i1.872

Abstract

Unmanned Aircraft (PTTA) or Unmanned Aerial Vehicle (UAV) is an aircraft that flies without a pilot and is controlled automatically. UAVs have a wide range of applications, including remote sensing, communication links, and natural disaster monitoring. One type of UAV being developed is LSU 05, using a composite of carbon fiber (CFRP) and glass fiber (GFRP) for its wing structure. This study aims to create a 3D model of the UAV VTOL wing, analyze the effect of material variations on the strength of the wing structure, and find the optimal wing design using the finite element analysis method. This study uses the SolidWorks 2021 software with maneuver conditions loading. The results of the analysis show that carbon fiber provides higher strength than fiberglass. In a fiberglass wing, the maximum stress is 229 MPa, while in a carbon fiber wing it is 197 MPa. The biggest displacement occurred in the fiberglass wing, which was 2.661 mm. The safety factor of the carbon fiber wing is 2.7, while that of the fiberglass is 1.9. This research provides an in-depth understanding of the behavior of VTOL UAV wing structures and contributes to the development of better wing designs. The optimized design can increase the performance, efficiency and reliability of VTOL UAV.
Co-Authors Buyung Ageng Islami Cakra P. Octavianus Edi Sofyan Ferry Setiawan Hendro Juandra Muhammad Kevin Adam Pius Pati Molan