Control of Flexible Launch Vehicle Based on Singular Perturbation and Reinforcement Learning-Reference-Cited by-同舟云学术

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Control of Flexible Launch Vehicle Based on Singular Perturbation and Reinforcement Learning

Published:2024-05-25 Issue: Volume:19 Page:665-671
ISSN:
Container-title:2024 36th Chinese Control and Decision Conference (CCDC)
language:
Short-container-title:

Author:

Qin Tong¹,Du Lifu²,Ruan Yihui¹,Li Jingqi¹,Liu Lei¹,Fan Huijin¹

Affiliation:

1. Huazhong University of Science and Technology,National Key Laboratory of Multispectral Information Intelligent Processing Technology. School of Artificial Intelligence and Automation,Wuhan,China

2. Beijing Aerospace Automatic Control Institute,Beijing,China

Funder

Research and Development

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx8/10587298/10587321/10587618.pdf?arnumber=10587618

Reference17 articles.

1. The development characteristics and trends of heavy launch vehicles;X;Aerospace China,2018

2. Elastic Dynamic Effects on the Trajectory of a Flexible Launch Vehicle

3. Attitude control of a flexible launch vehicle using an adaptive notch filter: Ground experiment;Wang;Nonlinear incremental control for flexible aircraft trajectory tracking and load alleviation,2022

4. Modified Adaptive Notch Filter Based on Neural Network for Flexible Dynamic Control

5. Flexible spacecraft's active fault-tolerant and anti-unwinding attitude control with vibration suppression

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