Robust Control for Non-Minimum Phase Systems with Actuator Faults: Application to Aircraft Longitudinal Flight Control

Robust Control for Non-Minimum Phase Systems with Actuator Faults: Application to Aircraft Longitudinal Flight Control

This study is concerned with developing a robust tracking control system that merges the optimal control theory with fractional-order-based control and the heuristic optimization algorithms into a single framework for the non-minimum phase pitch angle dynamics of Boeing 747 aircraft. The main contro...

Full description

Bibliographic Details
Main Authors: Aisha Sir Elkhatem, Seref Naci Engin, Amjad Ali Pasha, Mustafa Mutiur Rahman, Subramania Nadaraja Pillai
Format: Article
Language:English
Published: MDPI AG 2021-12-01
Series:Applied Sciences
Subjects:
actuator fault-tolerant
aircraft dynamics
heuristic optimization
fractional-order control
non-minimum phase
optimal control
Online Access:https://www.mdpi.com/2076-3417/11/24/11705

Internet

https://www.mdpi.com/2076-3417/11/24/11705

Similar Items