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OPTIMASI KONTROL PADA MANEUVERING KAPAL MENGGUNAKAN NI SB-RIO Siwindarto, Ponco; Eritha, Fadila Norasarin; Aswin, M.
Wave: Jurnal Ilmiah Teknologi Maritim Vol 13, No 2 (2019)
Publisher : Badan Pengkajian dan Penerapan Teknologi

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (784.275 KB) | DOI: 10.29122/jurnalwave.v13i2.3883

Abstract

Maneuvering kapal merupakan karakteristik dari sebuah kapal. Uji manever kapal sangat penting dan salah satu pengujiannya adalah zigzag. Jurnal ini menyodorkan salah satu sistem kontrol pada maneuvering kapal menggunakan NI SB-RIO yang memiliki dimensi kecil dan terkategori ringan dibandingkan pendahulunya. Perancangan sistem autopilot ini divalidasi melalui simulasi uji zigzag model kapal dan dari hasil validasi ini didapatkan bahwa sistem kontrol ini berfungsi dan mampu melakukan lintasan zig-zag sesuai yang diharapkan.
Fatigue Life Amphibious Floater based on RAO Slamming Pressure Priohutomo, Kusnindar; Nugroho , Wibowo Harso; Arianti, Erdina; Hidayat, Dony; Pinindriya, Sinung Tirtha; Yulfani, Rosi Dwi; Sugiarto, Muria Armansyah; Ismail, Muhammad Fajariansyah; Eritha, Fadila Norasarin; Choiriyah, Isma
International Journal of Marine Engineering Innovation and Research Vol. 11 No. 1 (2026): In Progress
Publisher : Department of Marine Engineering, Institut Teknologi Sepuluh Nopember

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.12962/j25481479.v11i1

Abstract

Floater is one of the most important part of amphibious version plane and conducting study of it becomes one of the featured research to support Indonesia’s transportation. This paper examined general study of amphibious floater slamming load when landing on the water in the various plane landing situation, starting from stern 5°, stern 10°, bow 5°, bow 10°, heel 0°, heel 5° and heel 10°. Carbon Fiber Reinforced Polymer (CFRP) material is used with 20 and 40 mm thickness. Floater consists of three main parts which are base, keel, and frame. Seaplane is designed to withstand 1000 cycle (500 landing and 500 take off cycle) in a year. This paper confirms that with the thickness of 20 and 40 mm, and heel position of 0°, floater can withstand up to 65,535 years. In contrary, using the 20 and 40 mm layer when landing with any combination position, the floater can’t last and only has 0.01 year of fatigue life.