TD3-Based Model Predictive Control for Satellite Formation-Keeping-Reference-Cited by-同舟云学术

TD3-Based Model Predictive Control for Satellite Formation-Keeping

Published:2024-11 Issue:6 Volume:37 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Hu Xing¹,Zhai Zhi²^ORCID,Liu Jinxin³,Wang Chenxi⁴,Liu Naijin⁵,Chen Xuefeng⁶^ORCID

Affiliation:

1. Master’s Student, National Key Lab of Aerospace Power System and Plasma Technology, School of Mechanical Engineering, Xi’an Jiaotong Univ., Xi’an 710049, China.

2. Associate Professor, National Key Lab of Aerospace Power System and Plasma Technology, School of Mechanical Engineering, Xi’an Jiaotong Univ., Xi’an 710049, China. ORCID: .

3. Professor, National Key Lab of Aerospace Power System and Plasma Technology, School of Mechanical Engineering, Xi’an Jiaotong Univ., Xi’an 710049, China (corresponding author).

4. Assistant Professor, National Key Lab of Aerospace Power System and Plasma Technology, School of Mechanical Engineering, Xi’an Jiaotong Univ., Xi’an 710049, China.

5. Professor, Qian Xuesen Laboratory of Space Technology, China Academy of Space Technology, Beijing 100094, China.

6. Professor, National Key Lab of Aerospace Power System and Plasma Technology, School of Mechanical Engineering, Xi’an Jiaotong Univ., Xi’an 710049, China. ORCID: .

Publisher

American Society of Civil Engineers (ASCE)

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-5646

Reference50 articles.

1. Alfriend, K., S. R. Vadali, P. Gurfil, J. How, and L. Breger. 2009. Spacecraft formation flying: Dynamics, control and navigation. Amsterdam, Netherlands: Elsevier.

2. Tuning Guidelines for Model-Predictive Control

3. Applying autonomy to distributed satellite systems: Trends, challenges, and future prospects

4. Refined dynamical analysis of multi-tethered satellite formations

5. Closed form tuning equations for model predictive control of first-order plus fractional dead time models