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基于模型预测控制的翼伞航迹跟踪

李之翰 南英 万金诚

航空科学技术2024,Vol.35Issue(4):74-82,9.
航空科学技术2024,Vol.35Issue(4):74-82,9.DOI:10.19452/j.issn1007-5453.2024.04.010

基于模型预测控制的翼伞航迹跟踪

Parafoil Trajectory Tracking Based on Model Predictive Control

李之翰 1南英 1万金诚2

作者信息

  • 1. 南京航空航天大学,江苏 南京 210016
  • 2. 航空工业航宇救生装备有限公司,湖北 襄阳 441003
  • 折叠

摘要

Abstract

A parafoil is an umbrella-like device that can be unfolded in the air and folded on the ground.Its inherent high instability and complex aerodynamic characteristics pose significant challenges for parafoil control.This paper proposed a parafoil trajectory tracking control method based on Model Predictive Control(MPC).First,a kinematic and dynamic model of the parafoil is established,including the state variables such as position,velocity,acceleration,and the aerodynamic forces and moments acting on the parafoil's motion.Then,the model predictive control method is employed to predict the parafoil's behavior using the known parafoil model and environmental model,and the optimal control inputs are calculated through an optimization algorithm to achieve parafoil trajectory tracking control.Finally,the effectiveness of the proposed control method is verified through simulation experiments.Compared to traditional parafoil tracking methods,the method proposed in this paper shows better tracking performance.This method can effectively suppress the influence on external disturbances,has good control accuracy and robustness,and has certain engineering application value.

关键词

翼伞/模型预测控制/航迹跟踪/优化算法/仿真验证

Key words

parafoil/MPC/trajectory tracking/optimization algorithm/simulation

分类

航空航天

引用本文复制引用

李之翰,南英,万金诚..基于模型预测控制的翼伞航迹跟踪[J].航空科学技术,2024,35(4):74-82,9.

基金项目

航空科学基金(201929052002) Aeronautical Science Foundation of China(201929052002) (201929052002)

航空科学技术

1007-5453

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