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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