Numerical studies on modeling the near- and far-field wake vortex of a quadrotor in forward flight
The operation of Unmanned Aerial Systems (UAS) is expected to keep increasing in the future with its rapid advancement and ever-expanding applications. One of the safety measures that need to be put into place for safe UAS operations is separation requirements. This article presents the results from...
Main Authors: | Nathanael, Joshua Christian, Wang, John Chung-Hung, Low, Kin Huat |
---|---|
Other Authors: | School of Mechanical and Aerospace Engineering |
Format: | Journal Article |
Language: | English |
Published: |
2022
|
Subjects: | |
Online Access: | https://hdl.handle.net/10356/155247 |
Similar Items
-
Numerical investigation on influence of fuselage on multirotor wake vortex structures in forward flight
by: Wang, John Chung-Hung, et al.
Published: (2022) -
Tracking of a moving ground target by a quadrotor using a backstepping approach based on a full state cascaded dynamics
by: Tan, Chun Kiat, et al.
Published: (2017) -
Simulation of wind field in a building complex for evaluation of the wind effect along UAS flight path
by: Nathanael, Joshua Christian, et al.
Published: (2023) -
Active control of wakes and vortex-induced vibration of a circular cylinder at Re = 100
by: Wang, Chenglei
Published: (2016) -
Robust linear output feedback controller for autonomous landing of a quadrotor on a ship deck
by: Tan, Chun Kiat, et al.
Published: (2019)