AI Chat Paper
Note: Please note that the following content is generated by AMiner AI. SciOpen does not take any responsibility related to this content.
{{lang === 'zh_CN' ? '文章概述' : 'Summary'}}
{{lang === 'en_US' ? '中' : 'Eng'}}
Chat more with AI
PDF (3 MB)
Collect
Submit Manuscript AI Chat Paper
Show Outline
Outline
Show full outline
Hide outline
Outline
Show full outline
Hide outline
Publishing Language: Chinese

Trajectory tracking control of multiple parafoil formation based on fuzzy PID

Qi CHEN1( )Chang ZHANG1Hongjin ZHANG1Jiyu HU1Like ZHAO2
College of Electronic Information Engineering, Huai’an University, Huai’an 223003, China
Jiangsu Keweida Intelligent Equipment Co., Ltd., Huai’an 211622, China
Show Author Information

Abstract

To address the issues of low control accuracy, weak disturbance rejection capability, and poor cooperative stability in trajectory tracking control of multiple parafoil formation, a fuzzy PID-based trajectory tracking control method for multiple parafoil formation is proposed. Firstly, a particle model of the multiple parafoil system is established, and the Dryden turbulence wind field model is introduced. Then, a three-dimensional trajectory tracking control strategy for parafoil formation is constructed. The tracking errors obtained from the reference command and measured output are fuzzified using triangular membership functions, and fuzzy inference is performed based on a predefined rule base. Through defuzzification, precise control gain parameters are obtained. The guidance control system is decoupled into two subsystems: horizontal-plane control and altitude control. The horizontal-plane control takes lateral deviation and heading angle error as inputs and outputs the heading angle command, while the altitude control takes longitudinal deviation and flight path angle error as inputs and outputs the flight path angle command. Finally, the proposed method is validated on the RflySim simulation platform. Simulation results demonstrate that, compared with the traditional PID control method, the fuzzy PID controller can still maintain a smooth trajectory and small deviations under turbulent wind disturbances, and it improves formation stability by 21.3%. Therefore, the fuzzy PID adaptive control algorithm can effectively suppress the influence of complex external environmental factors on parafoil formation, exhibiting high robustness and strong anti-disturbance capability.

CLC number: V249.1 Document code: A Article ID: 1000-6893(2026)S1-732897-13

References

【1】
【1】
 
 
Acta Aeronautica et Astronautica Sinica

{{item.num}}

Comments on this article

Go to comment

< Back to all reports

Review Status: {{reviewData.commendedNum}} Commended , {{reviewData.revisionRequiredNum}} Revision Required , {{reviewData.notCommendedNum}} Not Commended Under Peer Review

Review Comment

Close
Close
Cite this article:
CHEN Q, ZHANG C, ZHANG H, et al. Trajectory tracking control of multiple parafoil formation based on fuzzy PID. Acta Aeronautica et Astronautica Sinica, 2026, 47(S1). https://doi.org/10.7527/S1000-6893.2025.32897

0

Views

0

Downloads

0

Crossref

0

Scopus

0

CSCD

Received: 11 October 2025
Revised: 20 November 2025
Accepted: 08 December 2025
Published: 30 December 2025
© 2026 The Journal of Acta Aeronautica et Astronautica Sinica