Ratnasari, Wiwit (2021) Desain Kontrol pada Model Gerak Lateral-Direksional Unmanned Aerial Vehicle (UAV) Menggunakan Output Feedback Control. Undergraduate thesis, Institut Teknologi Sepuluh Nopember.
![[thumbnail of 06111740000004-Undergraduate_Thesis.pdf]](http://repository.its.ac.id/style/images/fileicons/text.png) |
Text
06111740000004-Undergraduate_Thesis.pdf - Accepted Version Restricted to Repository staff only until 1 October 2023. Download (1MB) | Request a copy |
|
Text
06111740000004-Undergraduate_Thesis.pdf - Accepted Version Restricted to Repository staff only Download (1MB) | Request a copy |
Abstract
Pengembangan teknologi di berbagai bidang dari tahun ke tahun semakin pesat, begitu pula pengembangan teknologi di bidang kedirgantaraan. Salah satu pengembangannya adalah pesawat tanpa awak atau Unmanned Aerial Vehicle (UAV). Dalam penelitian ini dilakukan analisis sistem dan desain kontrol pada model gerak lateral-direksional UAV menggunakan Output Feedback Control. Sistem bersifat tidak stabil, terkontrol, dan teramati. Agar UAV menjadi stabil, maka dilakukan penerapan Pole Placement pada desain kontrol dengan 5 skenario feedback gain (K1,K2, K3, K4, K5) untuk memindahkan nilai eigen yang menyebabkan sistem UAV tidak stabil. Skenario pada sudut selip paling baik adalah desain kontrol dengan K4 yang waktu stabilnya paling cepat yaitu 322 s, begitu pula pada sudut roll skenario terbaik adalah desain kontrol dengan K4 dimana pada waktu 172 s sudah stabil.
==================================================================================================================
Technology development in various field from year to year is increasing rapidly, as well as the development of technology in the field of aerospace. One of its development is Unmanned Aerial Vehicle (UAV). In this study, system analysis and control design were conducted on lateral-directional motion models of UAV using Output Feedback Control. The system is instable, controlled, and observed. In order for the UAV to be stable, pole placement is implemented in the control in the control design with 5 feedback gain scenarios (K1,K2, K3, K4, K5) to move the eigen value that causes the UAV system to be unstable. The scenario at the slip angle is best to design the control with the fastest stable time K4 of 322 s, as well as the best case roll angle is the control design with K4 which at the time of the 172 s is stable
| Item Type: | Thesis (Undergraduate) |
|---|---|
| Uncontrolled Keywords: | UAV, Gerak lateral-direksional, Output feedback control, Pole Placement, Lateral-Directional motion |
| Subjects: | Q Science > QA Mathematics Q Science > QA Mathematics > QA402 System analysis. T Technology > T Technology (General) T Technology > T Technology (General) > T57.62 Simulation T Technology > TL Motor vehicles. Aeronautics. Astronautics U Military Science > UG1242 Drone aircraft--Control systems. (unmanned vehicle) |
| Divisions: | Faculty of Science and Data Analytics (SCIENTICS) > Mathematics > 44201-(S1) Undergraduate Thesis |
| Depositing User: | Wiwit Ratnasari |
| Date Deposited: | 26 Aug 2021 03:45 |
| Last Modified: | 26 Aug 2021 03:45 |
| URI: | http://repository.its.ac.id/id/eprint/89702 |
Actions (login required)
 |
View Item |