Desain Sistem Kontrol Fixed-Wing Untuk Manuver Ekstrem Menggunakan Model Predictive Control

Rachmawati, Rossa Marsaulina (2026) Desain Sistem Kontrol Fixed-Wing Untuk Manuver Ekstrem Menggunakan Model Predictive Control. Other thesis, Institut Teknologi Sepuluh Nopember.

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Abstract

Manuver ekstrem merupakan aspek krusial dalam sistem kontrol Unmanned Aerial Vehicle (UAV), terutama pada misi yang menuntut kemampuan manuver cepat dan tajam untuk menghindari ancaman udara seperti intersepsi rudal. Penelitian ini berfokus pada pengendalian lintasan ekstrim seperti climbing turn, sharp break-dive, dan Immelmann like yang umum digunakan saat UAV menjalani misi tertentu. Climbing turn merupakan manuver UAV menanjak dikombinasikan dengan berbelok, sharp-break dive dilakukan dengan UAV secara cepat melakukan putar balik arah heading lalu melakukan dive, Immelman like merupakan manuver UAV dengan secara tajam menanjak ke atas lalu melakukan perubahan heading dengan memanfaatkan bank besar. Sistem kontrol yang diusulkan terdiri atas Model Predictive Control (MPC) untuk menghasilkan referensi posisi berdasarkan lintasan ekstrem, dan Proportional-Integral-Derivative (PID) sebagai pengendali untuk merealisasikan manuver melalui aktuasi kontrol. Model UAV akan dikembangkan dengan mempertimbangkan dinamika translasi dan rotasi, dengan asumsi bahwa UAV memiliki batas kecepatan maksimum sebesar 300 km/jam. Model ini akan disimulasikan menggunakan MATLAB dan Simulink. Desain sistem kontrol ini diharapkan mampu mendukung UAV fixed-wing melakukan manuver ekstrem secara stabil sesuai dengan skenario yang dirancang, serta membuka peluang pengembangan lebih lanjut dalam bidang penelitian ini.
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Extreme maneuvers are an important aspect of the control system of Unmanned Aerial Vehicles (UAVs), especially in missions that demand rapid and sharp maneuvering to evade aerial threats such as missile interception. This research focuses on controlling extreme trajectories such as the climbing turn, sharp break-dive, and Immelmann-like maneuvers commonly used during specific UAV missions. A climbing turn is a maneuver where the UAV climbs combined with a turn; a sharp break-dive is performed by the UAV rapidly reversing its heading direction and then diving; an Immelmann-like maneuver is where the UAV climbs sharply upward and then changes heading by utilizing a large bank angle. The proposed control system consists of Model Predictive Control (MPC) as to generate a position reference based on the extreme trajectory, and Proportional-Integral-Derivative (PID) as a controller to realize the maneuver through control actuation. The UAV model will be developed by considering translational and rotational dynamics, assuming that the UAV has a maximum speed limit of 300 km/hr. This model will be simulated using MATLAB and Simulink. The design of this control system is expected to be able to support the delta fixed-wing UAV to perform extreme maneuvers stably and precisely according to the designed scenario, and open up further development opportunities in this field of research.

Item Type:	Thesis (Other)
Uncontrolled Keywords:	UAV Fixed-Wing, Extreme Manuevers, Model Predictive Control, PID Controller
Subjects:	T Technology > TL Motor vehicles. Aeronautics. Astronautics > TL521 Aerodynamics, Hypersonic.
Divisions:	Faculty of Intelligent Electrical and Informatics Technology (ELECTICS) > Electrical Engineering > 20201-(S1) Undergraduate Thesis
Depositing User:	Rossa Marsaulina Rachmawati
Date Deposited:	28 Jan 2026 03:03
Last Modified:	28 Jan 2026 03:03
URI:	http://repository.its.ac.id/id/eprint/130658

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