Kendali Surface to Surface Rudal (Missile) dengan Menggunakan Nonlinear Model Predictive Control (NMPC)

Bestari, Dinda Siti Nuraida Ayu (2026) Kendali Surface to Surface Rudal (Missile) dengan Menggunakan Nonlinear Model Predictive Control (NMPC). Masters thesis, Institut Teknologi Sepuluh Nopember.

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Abstract

Indonesia merupakan negara kepulauan, sehingga sangat penting untuk meningkatkan sistem pertahanan negara. Salah satu contohnya adalah rudal (missile) yang dapat dikendalikan dari jarak jauh. Rudal (missile) merupakan senjata roket militer yang memiliki sistem kendali otomatis untuk menemukan sasarannya atau mengatur arahnya. Rudal jarak jauh dapat digunakan untuk menunjang pertahanan dan keamanan NKRI. Namun, konsekuensinya untuk dioperasikan di wilayah Indonesia, apabila terjadi kesalahan dalam menentukan sasaran akan menimbulkan kerugian bagi wilayah negaranya sendiri. Jenis rudal (missile) yang digunakan pada penelitian ini adalah cruise missile dimana targetnya diserang dari atas dengan bentuk umum lintasan optimalnya adalah: terbang datar, memanjat, menyelam (menukik) atau bisa disebut dengan bunt manoevre. Pada penelitian ini akan dilakukan kontrol pada rudal (missile) dengan tujuan agar rudal (missile) dapat bergerak menuju target sesuai lintasan (trajectory) yang siinginkan. Model matematika pada rudal (missile) berupa nonlinear. Metode kontrol yang digunakan adalah Nonlinear Model Predictive Control (NMPC). Extended Kalman Filter digunakan untuk memberikan estimasi pada state agar input kendali lebih akurat. Hasil estimasi yang didapatkan akan digunakan pada metode kendali NMPC.
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Indonesia is an archipelagic country, so it is very important to improve aerospace technology which is the main tool for the defense system to defend the country’s sovereignty. One example is a missile that can be controlled remotely. A missile is a military rocket weapon that has an automatic control system to find its target or adjust its direction. Logically, the existence of defense equipment (main weapon system) or rather long-range missiles is acceptable to support the defense and security of the Republic of Indonesia, but the consequences are for it to be operated in Indonesia’s own territory. If there is an error in determining the target, it will cause losses to the country’s own territory. The type of missile used in this research is a cruise missile. Where the target must be struck from above, subject to missile dynamics and path constraints. The generic shape of the optimal trajectory is: level flight, climbing, dive; this combination of the three flight phases is called the bunt manoeuvre. In this research, control will be carried out on the missile with the aim that the missile can move towards the target according to the desired trajectory. The mathematical model for missiles is nonlinear. The control method used is Nonlinear Model Predictive Control (NMPC). Extended Kalman Filter is used to provide an estimate of the state so that the control input is more accurate. The estimation results obtained will be used in the NMPC control method.

Item Type:	Thesis (Masters)
Uncontrolled Keywords:	rudal (missiles), Bunt Manoeuvre, Extended Kalman Filter, Nonlinear Model Predictive Control
Subjects:	Q Science > QA Mathematics > QA401 Mathematical models. Q Science > QA Mathematics > QA402 System analysis. Q Science > QA Mathematics > QA402.3 Kalman filtering.
Divisions:	Faculty of Science and Data Analytics (SCIENTICS) > Mathematics > 44101-(S2) Master Thesis
Depositing User:	Dinda Siti Nuraida Ayu Bestari
Date Deposited:	10 Aug 2026 05:20
Last Modified:	10 Aug 2026 05:20
URI:	http://repository.its.ac.id/id/eprint/144284

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