Agile flight control under multiple disturbances for quadrotor: algorithms and evaluation
In this article, a scheme of anti-disturbance agile flight control is developed for a maneuverable quadrotor unmanned aerial vehicle, subject to the aerodynamic drag, dynamic shift of center of gravity (CoG), and motor dynamics. A cascaded control framework is adopted. In the translational loop, an...
Saved in:
Main Authors: | Jia, Jindou, Guo, Kexin, Yu, Xiang, Guo, Lei, Xie, Lihua |
---|---|
Other Authors: | School of Electrical and Electronic Engineering |
Format: | Article |
Language: | English |
Published: |
2022
|
Subjects: | |
Online Access: | https://hdl.handle.net/10356/163762 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Nanyang Technological University |
Language: | English |
Similar Items
-
Study of drag reduction in coiled tube flow by polymer additives
by: Arsanchai Sukkuea
Published: (2012) -
Aerodynamic Analysis of Aircraft Wing
by: Nguyen, Minh Triet, et al.
Published: (2017) -
Numerical studies on modeling the near- and far-field wake vortex of a quadrotor in forward flight
by: Nathanael, Joshua Christian, et al.
Published: (2022) -
AERODYNAMICS OF WING-IN-GROUND (WIG) CRAFT
by: YOUHANNA EYLIA WILLIAM ELABD MANKARIOUS
Published: (2021) -
Quadrotor UAV: collision resilience behaviors
by: Fan, Dadong, et al.
Published: (2023)