ADI PUTRA, JAYA (2018) AUTOPILOT DENGAN ALGORITMA KENDALI L1 PADA PESAWAT FIX WING MENGGUNAKAN SISTEM HARDWARE IN THE LOOP SIMULATION. Skripsi thesis, Institut Teknologi Dirgantara Adisutjipto.
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Abstract
UAV Unmanned Aerial Vehicle is an aircraft that has no built-in aircraft. Functions on the plane are replaced by electronic devices and aircraft control devices. Accordingly the crew that controls the movement of aircraft are on the ground and control the plane with long distance RPS Remotely Piloted System. An UAV aircraft have been developed since 1980s, but UAV can growth faster to the stage of autonomous flying ability. In aviation, autopilot called Automatic Flight Control System AFCS. Qground Control is a control station for aircraft, helicopters and rovers and X-plane is a flight simulator software that can predict aircraft features based on air, the latter Pixhawk is a high-performance autopilot-on-module suitable for fixed wing, multi rotor, helicopter , cars, boats and other robot platforms that can move. Based on data obtained it can be calculated cross track error by comparing the desired y-axis path data with the actual plane position. The result of total cross track error with FW L1 setting DAMPING = 0.75 and FW L1 PERIOD = 12 m is 0.010791028. This results in a very ideal and approaching perfect for applying parameters while performing real aberration
Item Type: | Thesis (Skripsi) |
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Subjects: | T Technology > T Technology (General) |
Divisions: | Institut Teknologi Dirgantara Adisujtipto > Teknik Elektro |
Depositing User: | Mr JAYA ADI PUTRA |
Date Deposited: | 20 Aug 2024 07:51 |
Last Modified: | 20 Aug 2024 07:51 |
URI: | http://eprints.stta.ac.id/id/eprint/2568 |
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