Control Mechanism of Wing Landing Gears Aircraft Using PID Controller

Adi Mulyadi, Adi (2023) Control Mechanism of Wing Landing Gears Aircraft Using PID Controller. EJOURNAL BANYUWANGI, 1: 2022. pp. 293-294.

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Abstract

Introduction. This paper deals with the control mechanism of wing landing gears aircraft. The mechanism consists of wheel assembly deployed/retract and lock position based on an input signal. The mechanism is controlled by using a PID controller. Methods. The PID controller is used to deploy/retract the main column, and to lock or unlock the main column into position. Result & Discussion. The result shows that the parameter values in the deploy/retract control P=17.73, I=2.251 and D=82.33 resulted in a decrease in the main column angle from to and with a time of 1 second with an overshoot of seconds. While the PID parameter values for locking control P=20.23, I=5.001 and D=34.56 resulted in locking landing gear torque occurring at 2.1 seconds and overshoot at 2.6 seconds with delay conditions from 3 to 6 seconds. Conclusion. The deploy/retract control mechanism is slower than the locking torque to achieve the main column into position.

Item Type:	Article
Subjects:	Cek Plagiasi Jurnal Peer Review
Divisions:	F. Fakultas Teknik > Teknik Elektro
Depositing User:	perpus uniba admin
Date Deposited:	04 Sep 2023 03:01
Last Modified:	04 Sep 2023 03:01
URI:	http://repository.unibabwi.ac.id/id/eprint/792

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