Mufidah, Mirzaq Khoirul (2019) Model Predictive Control (MPC) Pada Kendali Misil Dengan Target Bergerak. Other thesis, Institut Teknologi Sepuluh Nopember.
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Abstract
Misil atau peluru kendali adalah senjata roket militer yang bisa dikendalikan atau memiliki sistem pengendali otomatis menuju target. Peluru kendali merupakan salah satu contoh Wahana Nir Awak (WANA) yang banyak digunakan untuk kepentingan militer maupun sipil seperti pada misi pengintaian, pengawasan, serta pengamanan hutan dan laut dari pencurian. Pada saat misi penembakan, misil memerlukan kontrol pada kendali misil yang akan diterbangkan menuju ke target dengan menggunakan metode Model Predictive Control (MPC) yang telah diakui kemampuannya dalam menyelesaikan persamaan nonlinier. Pada Tugas Akhir ini, model dinamika misil menuju target diberikan bentuk nonlinier, sedangkan untuk model yang diterapkan dengan metode Model Predictive Control (MPC) yaitu model diskrit linier. Sehingga model dinamika misil menuju target perlu dilakukan pelinieran dan pendiskritan. Selanjutnya, dari model diskrit linier dibentuk ke dalam desain kendali Model Predictive Control (MPC) yang meliputi tahap sistem dinamik, fungsi objektif dan fungsi kendala. Pada tahap sistem dinamik dan fungsi objektif didapatkan persamaan dalam bentuk quadratic programming yang selanjutnya disimulasikan dengan menggunakan MATLAB 2013a. Pada tahap fungsi kendala diberikan kendala yang meliputi kendala variabel state berupa nilai jarak dan kendala input berupa nilai percepatan misil. Sedemikian hingga didapatkan hasil dari rancangan Model Predictive Control ini yaitu nilai jarak misil menuju target yang diharapkan mendekati nilai 0.
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Missile is a military rocket weapon which can be controlled or has an automatic control system towards the target. Missile is one of Wahana Nir Awak (WANA) which is widely used for military and civilian interest, such as surveillance mission, reconnaissance, safeguarding forest and sea from theft. During the shooting mission, missile requires control of its control to be flown towards the target using Model Predictive Control (MPC) method which has been recognized for its ability to solve linear and non linear equation. In the final project, missile dynamics model towards the target is given a non linear form, while for the model applied using the Model Predictive Control (MPC) method, it is a linear discrete model. So that, the missile dynamics model towards the target it required to do linearly and discretely. Furthermore, a linear discrete model is form into the Model Predictive Control (MPC) design which includes the dynamics system, objective function, and constraints function. In the dynamic system and objective function were obtained in the form of quadratic programming equation and then simulated using MATLAB 2013a. In the other hand, constraint function is given constraints which include variable state constraint in the form of distance value and input constraint in the form of missile acceleration value. The result of Model Predictive Control (MPC) design is the distance of missile towards the expected target approaches 0.
| Item Type: | Thesis (Other) |
|---|---|
| Additional Information: | RSMa 511.8 Muf m-1 2019 |
| Uncontrolled Keywords: | Model Predictive Control (MPC), kendali misil (peluru kendali), percepatan misil, jarak misil dan target |
| Subjects: | Q Science Q Science > Q Science (General) > Q180.55.M38 Mathematical models Q Science > Q Science (General) > Q325 GMDH algorithms. Q Science > QA Mathematics > QA278.3 Structural equation modeling. Q Science > QA Mathematics > QA322.2 Normed linear spaces. Banach spaces Q Science > QA Mathematics > QA611.28 Metric spaces Q Science > QA Mathematics > QA640.7 Discrete geometry Q Science > QA Mathematics > QA76 Computer software Q Science > QA Mathematics > QA76.6 Computer programming. Q Science > QA Mathematics > QA9.58 Algorithms |
| Divisions: | Faculty of Mathematics and Science > Mathematics > 44201-(S1) Undergraduate Thesis |
| Depositing User: | Mirzaq Khoirul Mufidah |
| Date Deposited: | 19 Apr 2024 07:58 |
| Last Modified: | 19 Apr 2024 07:58 |
| URI: | http://repository.its.ac.id/id/eprint/64902 |
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