Desain Kendali Sudut Pitch Dan Roll Pada LSU-05 Dengan Metode Sliding Mode Control (SMC)

Muzaki, M Anas Fikri (2015) Desain Kendali Sudut Pitch Dan Roll Pada LSU-05 Dengan Metode Sliding Mode Control (SMC). Undergraduate thesis, Institut Teknologi Sepuluh Nopember.

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Abstract

Lapan Surveilance Unmanned Aerial Vehicle (LSU-05) adalah pesawat tanpa awak yang didesain dan dikembangkan oleh Pustekbang Lapan dengan misi surveillance (pemotretan dari udara). Spesifikasi LSU-05 mempunyai berat MTOW 75,08 kg dan berat payload 30 kg dengan kecepatan jelajah ratarata 27,28 m/s pada ketinggian terbang 6000 m. Pemodelan matematik sudah dilakukan menggunakan metoda first principle dan diperoleh persamaan keadaan dalam gerak longitudinal dan lateral-direksional. Langkah berikutnya adalah indentifikasi dan validasi persamaan keadaan menggunakan piranti lunak Matlab dengan masukan data dummy. Dalam menjalankan misinya LSU- 05 harus bisa terbang stabil. Oleh karena itu perlu didesain kendali yang didasarkan pada persamaan keadaan yang sudah divalidasi tersebut. Pada penelitian ini dilakukan perancangan kendali Slide Mode Control (SMC) untuk mengendalikan sudut pitch dan roll LSU-05. Dari hasil simulasi diketahui bahwa SMC bisa digunakan untuk mengendalikan sudut pitch dan roll LSU-05. ========================================================================================================= Lapan Surveillance Unmanned Aerial Vehicle (LSU-05) is the unmanned aircraft designed and developed by Pustekbang Lapan with surveillance missions (aerial photography). LSU-05 specifications have MTOWweight of 75.08 kg and a payload weight of 30 kg with an average cruising speed of 27.28 m / s at a height of fly 6000 m. Mathematical modeling has been carried out using the method of first principle and obtained equation of state in the longitudinal and lateral-directional . The next step is the identification and validation of the state equation using Matlab software with dummy data input. LSU-05 should be able to fly stable and therefore it is necessary that the control design is validated. In this research, the Slide Mode Control (SMC) is applied for the pitch and roll angles. From the simulation results it is known that SMC can be used to control the pitch and roll angles LSU-05.

Item Type: Thesis (Undergraduate)
Additional Information: RSMa 511.8 Muz d
Uncontrolled Keywords: LSU-05, Longitudinal, Lateral-direksional, SMC
Subjects: Q Science > Q Science (General) > Q180.55.M38 Mathematical models
Divisions: Faculty of Mathematics and Science > Mathematics > 44201-(S1) Undergraduate Thesis
Depositing User: Yeni Anita Gonti
Date Deposited: 10 Feb 2020 06:06
Last Modified: 10 Feb 2020 07:29
URI: http://repository.its.ac.id/id/eprint/74785

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