Optimization of Active Disturbance Rejection Control Parameters for Spacecraft Docking in Approach Phase-Reference-Cited by-同舟云学术

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Optimization of Active Disturbance Rejection Control Parameters for Spacecraft Docking in Approach Phase

Published:2024-04-26 Issue: Volume: Page:520-525
ISSN:
Container-title:2024 5th International Conference on Mechatronics Technology and Intelligent Manufacturing (ICMTIM)
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Author:

Zhu Xiao-Guang¹,Jiang Qi-Ying¹,Xu Wei-Chang¹,Luo Jing¹,Chang Zhi-Qiang¹

Affiliation:

1. High-Tech Institute,Qing Zhou,China,262509

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx8/10629219/10629224/10629292.pdf?arnumber=10629292

Reference14 articles.

1. Dongping Three body spin spacecraft formation rendezvous and docking control and ground experiment research;Zhengtao;Chinese Society of Mechanics,2021

2. Single-thrust spacecraft rendezvous and docking trajectory planning and tracking control;Yuanzhuo;Journal of Aeronautics,2020

3. Model prediction and inverse guidance control for spacecraft rendezvous and docking;Tianle;Control and Decision Making (2019),2019

4. Analytical solution and optimal control of relative motion in spacecraft docking in approach phase;Jing;Flight Mechanics (2014),2014

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