Stable and accurate tracking control of tail-sitter aircraft in all flight modes

Author:

Zou Xu,Liu Zhenbao,Dang Qingqing,Wang Lina

Abstract

Purpose This paper aims to design a global controller that is operational throughout all flight modes and less dependent on an accurate model. Design/methodology/approach By adopting the interconnection and damping assignment passivity-based control (IDA-PBC) technology and compensating extra inputs for handling the unknown dynamics and time-varying disturbances, a model-free control (MFC)-based global controller is proposed. Findings Test results indicate that the designed controllers are more suitable for actual flight as they have smaller position tracking errors and energy consumption in all flight phases than the excellent model-free controller intelligent-PID. Practical implications The designed global controller, which works in all flight modes without adjusting its structure and parameters, can realize a stable and accurate tracking control of a tail-sitter and improve the resistance to unknown disturbances and model uncertainties. Originality/value The newly-designed controller is considered as an enhanced version of the traditional MFC. It further improves the control effect by using the poorly known dynamics of the system and choosing the IDA-PBC as the control auxiliary input. This method eliminates the unnecessary dynamics to continuously stabilize the vehicle with suitable energy consumption covering its entire flight envelope.

Publisher

Emerald

Subject

Aerospace Engineering

Reference23 articles.

1. Adaptive trajectory tracking control for VTOL-UAVs with unknown inertia, gyro-bias, and actuator LOE;International Journal of Robust and Nonlinear Control,2018

2. Model-free control applied for position control of quadrotor using ROS,2019

3. Model-free control;International Journal of Control,2013

4. A novel induction motor control scheme using IDA-PBC;Journal of Control Theory and Applications,2008

5. Model-free control using nonlinear extended state observer and non-singular fast terminal sliding mode for quadrotor position and attitude,2020

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