Parameter retrieval of aircraft wake vortex based on its max–min distribution of Doppler velocities measured by a Lidar
Aircraft wake vortex is a sort of turbulence generated by a flying aircraft. It has attracted much attention in aviation safety area because it may cause a following aircraft to roll out of control. This study proposes a simple method to retrieve the characteristic parameters of an aircraft wake bas...
Main Authors: | Hang Gao, Jianbing Li, P.W. Chan, K.K. Hon |
---|---|
Format: | Article |
Language: | English |
Published: |
Wiley
2019-09-01
|
Series: | The Journal of Engineering |
Subjects: | |
Online Access: | https://digital-library.theiet.org/content/journals/10.1049/joe.2019.0539 |
Similar Items
-
Aircraft Wake Vortex Parameter-retrieval System Based on Lidar
by: Chun SHEN, et al.
Published: (2020-12-01) -
SIMULATION OF WAKE VORTEX AIRCRAFT IN GROUND EFFECT
by: Pamfil ŞOMOIAG, et al.
Published: (2011-03-01) -
Review of Radar Characteristics and Sensing Technologies of Distributed Soft Target
by: Jianbing LI, et al.
Published: (2021-02-01) -
Aircraft Wake Vortex Behavior Prediction Based on Data Assimilation
by: Chun SHEN, et al.
Published: (2021-08-01) -
Framework for the estimation of safe wake separation distance between same-track multi-rotor UAS
by: Wang, John Chung-Hung, et al.
Published: (2021)