Influence of Structural Flexibility on Nonlinear Vibrations Induced by Orbital Maneuver for a Tethered Spacecraft-Reference-Cited by-同舟云学术

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Influence of Structural Flexibility on Nonlinear Vibrations Induced by Orbital Maneuver for a Tethered Spacecraft

Published:2023-01 Issue:1 Volume:36 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Fang Bo¹,Cao Dengqing²^ORCID,Chen Chao¹,Tian Yishen³^ORCID,Li Youxia⁴

Affiliation:

1. Ph.D. Student, School of Astronautics, Harbin Institute of Technology, Harbin 150001, PR China.

2. Professor, School of Astronautics, Harbin Institute of Technology, Harbin 150001, PR China (corresponding author). ORCID: .

3. Ph.D. Student, School of Astronautics, Harbin Institute of Technology, Harbin 150001, PR China. ORCID: .

4. Engineer, China Academy of Space Technology, Beijing 100000, PR China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-4607

Reference42 articles.

1. Dynamics of large space debris removal using tethered space tug

2. Dynamics, analytical solutions and choice of parameters for towed space debris with flexible appendages

3. Non-linear dynamics of an elastic cable under planar excitation

4. Modeling and analysis of the in-plane vibration of a complex cable-stayed bridge

5. Natural Frequencies and Global Mode Functions for Flexible Jointed-Panel Structures

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