State Feedback Controller Design for a Twin-Rotor Helicopter Model via Real-Time Linearization-Reference-Cited by-同舟云学术

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State Feedback Controller Design for a Twin-Rotor Helicopter Model via Real-Time Linearization

Published:2022-11-24 Issue: Volume: Page:
ISSN:
Container-title:2022 Australian & New Zealand Control Conference (ANZCC)
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Author:

Tahersima Hanif¹,Saleh Mohammad Jafar²,Jafari Masoumeh³,Hamedi Navid⁴,Mesgarisohani Sara⁵

Affiliation:

1. Hong Kong University of Science & Technology,Mechanical Engineering Department,Hong Kong

2. Talachin Agro-Industrial Co,Engineering Department,Tehran,IRAN

3. Shiraz University,Power and Control Engineering Department,Shiraz,IRAN

4. Australian Synchrotron,Controls and Computing Department,ANSTO,Australia

5. London’s Global University,Civil Engineering Department,United Kingdom

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9966854/9966858/09966955.pdf?arnumber=9966955

Reference11 articles.

1. Nonlinear System Identification: From Classical Approaches to Neural Networks and Fuzzy Models;nelles,2001

2. Global linearization of non-linear state equations

3. Nonlinear identification and MIMO control of a laboratory helicopter using genetic algorithm

4. Nonlinear state feedback controller for nonlinear systems: Stability analysis and design based on fuzzy plant model

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