Modelling and fixed order robust H∞ control of aerial vehicle: simulation and experimental results-Reference-Cited by-同舟云学术

Modelling and fixed order robust H∞ control of aerial vehicle: simulation and experimental results

Published:2016-03-17 Issue:3 Volume:35 Page:
ISSN:0332-1649
Container-title:COMPEL - The international journal for computation and mathematics in electrical and electronic engineering
language:en
Short-container-title:

Author:

Chabir Alaa,Boukhnifer Moussa,bouteraa yassine,chaibet ahmed,ghommam jawhar

Abstract

Purpose This work focuses on modelling, robust controller design and real time control of 3-DOF Helicopter. Design/methodology/approach This study presents an improved H∞ controller for this aerial vehicle Findings Simulation and experiment results are addressed to demonstrate the capability of this proposed control strategy to counteract the effect of this disturbance Originality/value In order to reduce the complexity of the standard H∞ structure, a fixed order control design is proposed as original approach

Publisher

Emerald

Subject

Applied Mathematics,Electrical and Electronic Engineering,Computational Theory and Mathematics,Computer Science Applications

Reference8 articles.

1. Choudhary, S.K. (2014), “LQR based PID controller design for 3-DOF helicopter system”, International Journal of Computer, Electrical, Automation, Control and Information Engineering , Vol. 8 No. 8, pp. 1438-1443.

2. State-space solutions to standard H/sub 2/ and H/sub infinity / control problems

3. Robust regulation for a 3-DOF helicopter via sliding-mode observation and identification

4. Nonlinear Trajectory Control of Multi-body Aerial Manipulators

5. Robust LQR Attitude Control of a 3-DOF Laboratory Helicopter for Aggressive Maneuvers

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Design, Mathematical Modeling, and Control of an Underactuated 3-DOF Experimental Helicopter;IEEE Access;2024

2. A Novel Flight Dynamics Modeling Using Robust Support Vector Regression against Adversarial Attacks;SAE International Journal of Aerospace;2023-03-24

3. Performance comparison of structured H ∞ based looptune and LQR for a 4-DOF robotic manipulator;PLOS ONE;2022-04-11

4. Lyapunov-based Robust Adaptive Configuration of the UAS-S4 Flight Dynamics Fuzzy Controller;The Aeronautical Journal;2022-02-11