Adaptive flight control for unmanned autonomous helicopter with external disturbance and actuator fault

Adaptive flight control for unmanned autonomous helicopter with external disturbance and actuator fault

A backstepping-based robust adaptive fault tolerant control (FTC) scheme is proposed for the altitude and attitude dynamic model of the medium-scale unmanned autonomous helicopter (UAH) subjected to external disturbance and actuator fault. The external disturbance and actuator fault are integrated i...

Full description

Bibliographic Details
Main Authors: Kun Yan, Mou Chen, Qingxian Wu, Yuhui Wang
Format: Article
Language:English
Published: Wiley 2019-11-01
Series:The Journal of Engineering
Subjects:
control system synthesis
adaptive control
robust control
nonlinear control systems
control nonlinearities
fault tolerant control
helicopters
uncertain systems
attitude control
actuators
aircraft control
autonomous aerial vehicles
adaptive flight control
external disturbance
actuator fault
backstepping-based robust adaptive fault tolerant control scheme
attitude dynamic model
medium-scale unmanned autonomous helicopter
adaptive control approach
backstepping control technique
robust adaptive ftc law
controller design
tracking property
Online Access:https://digital-library.theiet.org/content/journals/10.1049/joe.2019.1080

Similar Items

Similar Items