General Extended State Observer-Based Robust Integral of Signum of Error Controller for Active Flutter Suppression for Aeroelastic System

Author:

Sharma Balraj12,Agrawal Pooja3,Misra Ajay1

Affiliation:

1. Department of Aerospace Engineering, Defence Institute of Advanced Technology, Pune 411025, India

2. Defence Institute of Advanced Technology

3. School of Robotics, Defence Institute of Advanced Technology , Pune 411025, India

Abstract

Abstract The paper presents a robust integral of signum of error (RISE) controller for active suppression of flutter of a two-dimensional airfoil, and it is integrated with a general extended state observer (GESO). Toward this, airfoil model in state space is first changed into a canonical form. Then, the controller is designed using RISE control technique. As equations of system dynamics are not into integral chain form, a GESO is formulated to observe system states and disturbances. The controller is implemented using estimated states and it is robustified using estimated disturbance. Stability of the proposed general extended state observer-robust integral of signum of error (GESO-RISE) controller is established using the Lyapunov theory. Simulations are performed to check the proposed controller's performance against variations in airspeed, uncertainties in model parameters, external disturbances, time delay, and unmodeled dynamics. Comparison of the proposed GESO-RISE controller is carried out with existing controllers using two performance criteria, i.e., Control Efforts (CoE) and integral of absolute error (IAE). It is discovered from simulations that the proposed GESO-RISE controller significantly reduces IAE and control efforts. Additionally, Monte Carlo method is utilized to check robustness of the proposed GESO-RISE controller. The proposed GESO-RISE controller significantly enhances flutter boundary of airfoil and is completely implementable.

Publisher

ASME International

Reference37 articles.

1. Identification of Flutter Parameters for a Wing Model;J. Braz. Soc. Mech. Sci.,2006

2. Kehoe, M. W., 1995, “ Historical Overview of Flight Flutter Testing,” Report No. NASA TM-4720.

3. Akmese, A., 2006, “ Aeroservoelastic Analysis and Robust Controller Synthesis for Flutter Suppression of Air Vehicle Control Actuation Systems,” Ph.D. thesis, The Middle East Technical University, Turkey.

4. Aeroelastic Analysis and Flutter Control of Wings and Panel: A Review;Int. J. Mech. Syst. Dyn.,2021

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3