Journal of Aerospace Engineeringhttp://yetl.yabesh.ir/yetl1/handle/yetl/190112026-08-23T23:49:57Z2026-08-23T23:49:57ZSuppression of the Vortex-Induced Vibration of a Circular Cylinder with Low Mass DampingShe, YuqiXie, FanWang, XiangjunHu, PengHan, Yanhttp://yetl.yabesh.ir/yetl1/handle/yetl/43142052026-08-20T21:16:06Z2026-01-01T00:00:00ZSuppression of the Vortex-Induced Vibration of a Circular Cylinder with Low Mass Damping
She, Yuqi; Xie, Fan; Wang, Xiangjun; Hu, Peng; Han, Yan
AbstractNumerical simulations are carried out to investigate the aerodynamic coefficients
of a stationary circular cylinder with bypass channels and its vortex-induced vibration
(VIV) under low mass-damping conditions. A progressive increase in the bypass ...
2026-01-01T00:00:00ZModeling and Analysis of Static–Dynamic Mechanical Characteristics of a Rigid–Flexible Coupled Lunar Transfer MechanismAn, XiaokangJia, QingxuanChen, GangHan, Yuhttp://yetl.yabesh.ir/yetl1/handle/yetl/43142042026-08-20T21:16:04Z2026-01-01T00:00:00ZModeling and Analysis of Static–Dynamic Mechanical Characteristics of a Rigid–Flexible Coupled Lunar Transfer Mechanism
An, Xiaokang; Jia, Qingxuan; Chen, Gang; Han, Yu
AbstractAddressing the challenge of real-time mechanical state evaluation for rigid–flexible
coupled lunar transfer mechanisms due to their time-varying configurations and complex
working conditions, this paper proposes a comprehensive mechanical ...Practical ApplicationsThis study tackles the key challenge of transferring scientific payloads on the lunar
surface. Similar to how cranes handle heavy loads on Earth, moving delicate instruments
across the Moon’s complex terrain requires precision and ...
2026-01-01T00:00:00ZAutonomous Collision Evasion Strategy for Satellites Based on Line-of-Sight RateZhou, XiaoliBei, Chaohttp://yetl.yabesh.ir/yetl1/handle/yetl/43142032026-08-20T21:16:02Z2026-01-01T00:00:00ZAutonomous Collision Evasion Strategy for Satellites Based on Line-of-Sight Rate
Zhou, Xiaoli; Bei, Chao
AbstractThe line of sight (LOS) is defined as the relative direction from the spacecraft to
the target as measured by the optical sensor. The LOS rate represents the speed of
change in the LOS angle. This paper presents an autonomous in-orbit collision ...Practical ApplicationsThis research introduces a satellite collision avoidance strategy based on line-of-sight
(LOS) rate, which simplifies the decision-making process in space navigation. By using
event cameras to measure real-time LOS data, the strategy ...
2026-01-01T00:00:00ZDual-Layer Actuator Coordination Attitude Control for Reentry Hypersonic Flight Vehicles under Intermittent FaultsXiang, ZikunDu, LifuLiu, XiaoyuChen, Fuyanghttp://yetl.yabesh.ir/yetl1/handle/yetl/43142022026-08-20T21:16:00Z2026-01-01T00:00:00ZDual-Layer Actuator Coordination Attitude Control for Reentry Hypersonic Flight Vehicles under Intermittent Faults
Xiang, Zikun; Du, Lifu; Liu, Xiaoyu; Chen, Fuyang
Abstract This paper proposes a fault-tolerant control scheme for the attitude tracking of reentry
hypersonic flight vehicles (HFVs) subject to intermittent faults and actuator constraints.
Due to the fluctuating detection delays induced by the stochastic ...
2026-01-01T00:00:00Z