RANCANG ULANG SISTEM KENDALI AUTOPILOT
PESAWAT BOEING 747 PADA KONDISI CRUISE
MENGGUNAKAN METODE POLE PLACEMENT
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Institusion
INSTITUT TEKNOLOGI DIRGANTARA ADISUTJIPTO
Author
DWI NUGROHO ASRI, ILHAM
Subject
T Technology (General)
Datestamp
2024-06-20 06:15:49
Abstract :
As the development of technology in aviation, an aircraft need a system control, it is called autopilot. Flight control system has a modus motion, there are longitudinal modus motion and lateral modus motion. In this case, the writer create design of autopilot at lateral modus motion with three system of flight control, there are yaw damper, roll attitude hold, and heading hold. Detail of examination method is pole placement to use for moving the location of pole plant to other location previously specified. So, with this method to produce a better plane. Then, also use flight planning using the waypoint following system The results of the design in this study yaw damper control system produces a settling time of 6.86 seconds, the roll resistant control system produces a settling time of 61.9 seconds, the heading control system produces a settling time of 124 seconds. On waypoint flight planning follows the distance difference of 15.17 meters.
As the development of technology in aviation, an aircraft need a system control, it is called autopilot. Flight control system has a modus motion, there are longitudinal modus motion and lateral modus motion. In this case, the writer create design of autopilot at lateral modus motion with three system of flight control, there are yaw damper, roll attitude hold, and heading hold. Detail of examination method is pole placement to use for moving the location of pole plant to other location previously specified. So, with this method to produce a better plane. Then, also use flight planning using the waypoint following system The results of the design in this study yaw damper control system produces a settling time of 6.86 seconds, the roll resistant control system produces a settling time of 61.9 seconds, the heading control system produces a settling time of 124 seconds. On waypoint flight planning follows the distance difference of 15.17 meters.
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