PENERAPAN PARAMETER PID PADA HARDWARE IN THE
LOOP SIMULATION UNTUK SIMULASI KENDALI
ATTITUDE PESAWAT
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Institusion
INSTITUT TEKNOLOGI DIRGANTARA ADISUTJIPTO
Author
SATRYA KARDELI, MUHAMMAD
Subject
T Technology (General)
Datestamp
2024-08-20 07:50:54
Abstract :
The design of the Hardware In The Loop Simulation by simulation using a computer. Each plane has different characteristics with the help of PID tuning (Proportional Integral Derivative) and Ziegler Nichols is intended to know, analyze, and get an overview of responses generated in the aircraft (response) output. The simulation flight test is done by connecting two laptops, the flight simulator Xplane and qgroundcontrol which is controlled by the use of RC (remote control). PID control tuning system works well in the time constant pamater of 0.65 because the aircraft plane has followed the waypoint has been determined and fly the plane very well and Ziegler Nichols method of the resulting wave response yields the best response ie with the value of Kp = 1.10464, Ki = 0.000675211, Kd = 451.8
The design of the Hardware In The Loop Simulation by simulation using a computer. Each plane has different characteristics with the help of PID tuning (Proportional Integral Derivative) and Ziegler Nichols is intended to know, analyze, and get an overview of responses generated in the aircraft (response) output. The simulation flight test is done by connecting two laptops, the flight simulator Xplane and qgroundcontrol which is controlled by the use of RC (remote control). PID control tuning system works well in the time constant pamater of 0.65 because the aircraft plane has followed the waypoint has been determined and fly the plane very well and Ziegler Nichols method of the resulting wave response yields the best response ie with the value of Kp = 1.10464, Ki = 0.000675211, Kd = 451.8
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