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非线性干扰观测器的高超声速飞行器鲁棒反演控制

王鹏飞 王洁 时建明 贾英杰

火力与指挥控制2017,Vol.42Issue(8):123-127,5.
火力与指挥控制2017,Vol.42Issue(8):123-127,5.DOI:10.3969/j.issn.1002-0640.2017.08.028

非线性干扰观测器的高超声速飞行器鲁棒反演控制

Robust Backstepping Control for Hypersonic Vehicles Based on Nonlinear Disturbance Observer

王鹏飞 1王洁 1时建明 1贾英杰1

作者信息

  • 1. 空军工程大学防空反导学院,西安 710051
  • 折叠

摘要

Abstract

A nonlinear disturbance observer based on robust backstepping controller is designed for hypersonic vehicles. Based on backstepping control method,velocity and altitude controllers are designed respectively. The sliding mode differentiators are introduced to obtain the derivatives of virtual control laws,which avoids the explosion of differentiation teens in the traditional backstepping control. In order to enhance the controllers' robustness,a nonlinear disturbance observer is introduced to estimate and compensate the model uncertainties. Reference trajectory tracking simulation shows the effectiveness of this controller in tracking velocity and altitude commands.

关键词

高超声速飞行器/反演控制/干扰观测器/滑模微分器

Key words

hypersonic vehicles/backstepping control/disturbance observer/sliding mode differentiator

分类

信息技术与安全科学

引用本文复制引用

王鹏飞,王洁,时建明,贾英杰..非线性干扰观测器的高超声速飞行器鲁棒反演控制[J].火力与指挥控制,2017,42(8):123-127,5.

火力与指挥控制

OA北大核心CSCDCSTPCD

1002-0640

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