Shock and harmonic response analysis of UAV nose landing gear system with air damper
This research presents a response analysis of a UAV nose landing gear system equipped with an air damper under shock and harmonic excitation. The study begins with dynamic modeling of the UAV landing gear system. The system dynamics consists of a main mass and a wheel mass that are connected to each...
Main Authors: | Lovely Son, Muhammad Surya, Mulyadi Bur, Ubaidillah Ubaidillah, Radon Dhelika |
---|---|
Format: | Article |
Language: | English |
Published: |
Taylor & Francis Group
2021-01-01
|
Series: | Cogent Engineering |
Subjects: | |
Online Access: | http://dx.doi.org/10.1080/23311916.2021.1905231 |
Similar Items
-
Experimental Validation for the Performance of MR Damper Aircraft Landing Gear
by: Bang-Hyun Jo, et al.
Published: (2021-09-01) -
Robust Adaptive Control for an Aircraft Landing Gear Equipped with a Magnetorheological Damper
by: Quoc Viet Luong, et al.
Published: (2020-02-01) -
Analysis of the Static Behavior of a New Landing Gear Model based on a Four-bar Linkage Mechanism
by: Lovely Son, et al.
Published: (2019-12-01) -
Applied research of the multi-stage torsional vibration damper on controlling the gear rattle
by: Lei Wang, et al.
Published: (2016-11-01) -
A Prediction Method for the Damping Effect of Ring Dampers Applied to Thin-Walled Gears Based on Energy Method
by: Yanrong Wang, et al.
Published: (2018-11-01)