Desain Kontrol Pada Lintasan Pesawat Tanpa Awak Menggunakan Metode Abstraksi

'Aini, Zulfa Qurrotul (2018) Desain Kontrol Pada Lintasan Pesawat Tanpa Awak Menggunakan Metode Abstraksi. Undergraduate thesis, Institut Teknologi Sepuluh Nopember.

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Abstract

Pesawat tanpa awak (Unmanned Air Vehicles) yang biasa disingkat UAV merupakan jenis pesawat terbang dengan kedali jarak jauh oleh pilot atau dapat mengendalikan dirinya sendiri. Saat kondisi pesawat tanpa awak dikendalikan secara autopilot, maka membutuhkan sebuah navigasi penerbangan. Nevigasi penerbangan ini yang akan membuat posisi dari pesawat berpindah pada satu titik ke titik yang lain tanpa menabrak suatu halangan. Sehingga, diperlukan suatu pendesainan kontrol pada lintasan pesawat. Dalam desain kontrol yaitu dengan menerapkan metode abstraksi yang menggunakan software Pessoa. Desain kendali dengan abstraksi bertujuan untuk mendesain kendali agar perilaku sistem closed loop memenuhi keinginan atau spesifikasi. Parameter abstraksi dan spesifikasi dalam desain kendali dengan abstraksi diantaranya adalah η = 0:1; µ = 0:5; τ = 0:5;, dan spesifikasi Reach and Stay while Stay. Hasil yang diperoleh dari simulasi desain kontrol metode abstraksi yaitu respon posisi dan sudut heading yang memenuhi spesifikasi. ================================================================================================ Unmanned Air Vehicles (Unmanned Air Vehicles) usually call as UAV is a type of aircraft with a long distance by the pilot or can control itself. When an unmanned air condition is controlled by autopilot, it requires a flight navigation. This flight navigation will make the position of the plane move from one point to another without crashing an obstacle. Thus, it is necessary to design a control on the plane path. In the control design is by applying the abstraction method using software PESSOA. The design of control with abstraction method to design the control for closed loop system behavior to meet the desires or specifications. The abstraction parameters and specifications in the control design with abstractions include η = 0:1; µ = 0:5; τ = 0:5;, and the specificaton is Reach and Stay while Stay. The results obtained from the control design simulation abstraction method that is the position response and the heading angle that satisfying specifications.

Item Type: Thesis (Undergraduate)
Additional Information: RSMa 512.2 Ain d 2018
Uncontrolled Keywords: Pesawat Tanpa Awak, Lintasan, Kontrol Sintesis, software PESSOA
Subjects: Q Science > QA Mathematics > QA159 Algebra
T Technology > TJ Mechanical engineering and machinery > TJ213 Automatic control.
Divisions: Faculty of Mathematics, Computation, and Data Science > Mathematics > 44201-(S1) Undergraduate Thesis
Depositing User: Zulfa Qurrotul 'Aini
Date Deposited: 07 May 2021 05:49
Last Modified: 03 Jul 2021 04:35
URI: https://repository.its.ac.id/id/eprint/59946

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