Astuti, Restu Tri (2012) Analisis Model Kinematik Peluru Kendali Pada Penembakan Target Menggunakan Metode Kendali Optimal. Other thesis, Institut Teknologi Sepuluh Nopember.
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Abstract
Peluru kendali merupakan salah satu wahana nir awak (WANA) yang dapat dikendalikan atau memiliki system pengendali otomatis untuk mencari target atau menyesuaikan arab. Masalah pengendali dengan kendala sudut dan waktu akhir dikaji dalam Tugas Akhir ini. Variabel bebas pada model kinematik tak-linear peluru kendali ke target diubah dari waktu terbang ke sudut hadap peluru kendali. Kemudian pengendali diperoleh pada transformasi model kinematik peluru kendali ke target dengan prinsip minimum Pontryagin. Tujuan pengendali adalah menepatkan arab gerak peluru kendali ke target dengan memenuhi kendala sudut dan waktu akhir. Selanjutnya, daerah range pada beberapa parameter kendala dianalisis untuk memeriksa kelayakan pengendali. Dalam Tugas Akhir ini, simulasi numerik diberikan untuk menunjukkan keefektifan metode kendali optimal pada performansi sistem
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A guided missile is an unmanned aerial vehicle (UAV) that can be controlled or has an automatic control system to find a target or adjust the trajectory. The control problem with angle and final time constraints is studied in this Final Project. The independent variable in the nonlinear kinematic model of the guided missile to the target is changed from the flight time to the missile's facing angle. Then the controller is obtained by transforming the kinematic model of the guided missile to the target with the Pontryagin minimum principle. The goal of the controller is to adjust the trajectory of the guided missile to the target by satisfying the angle and final time constraints. Furthermore, the range region of several constraint parameters is analyzed to check the feasibility of the controller. In this Final Project, numerical simulations are given to demonstrate the effectiveness of the optimal control method on system performance.
| Item Type: | Thesis (Other) |
|---|---|
| Additional Information: | RSMa 515.642 Ast a-1 2012 (weding) |
| Uncontrolled Keywords: | daerah range, sudut hadap, wahana nir awak (WANA), waktu akhir; feasibility, impact angle, impact time, range region, unmanned aerial vehicle (UAV) |
| Subjects: | Q Science > QA Mathematics > QA401 Mathematical models. |
| Divisions: | Faculty of Mathematics and Science > Mathematics > 44201-(S1) Undergraduate Thesis |
| Depositing User: | EKO BUDI RAHARJO |
| Date Deposited: | 16 Sep 2025 06:37 |
| Last Modified: | 16 Sep 2025 06:37 |
| URI: | http://repository.its.ac.id/id/eprint/128263 |
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