Adi Mulyadi, Adi (2023) Control Mechanism of Wing Landing Gears Aircraft Using PID Controller. (International Conference for Aviation Vocational Education and Training), 1 (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 90∘
to
10∘
and 0∘ with a time of 1 second with an overshoot of −0,7 × 105
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 Mesin |
| Depositing User: | perpus uniba admin |
| Date Deposited: | 30 Aug 2023 06:54 |
| Last Modified: | 30 Aug 2023 06:54 |
| URI: | http://repository.unibabwi.ac.id/id/eprint/780 |
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