Spin-Up and Appointed Time Attitude Control of Tethered Spacecraft for Artificial Gravity-Reference-Cited by-同舟云学术

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Spin-Up and Appointed Time Attitude Control of Tethered Spacecraft for Artificial Gravity

Published:2023-09 Issue:5 Volume:36 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Tian Haochang¹^ORCID,Li Aijun²,Wang Changqing²,Wang Yu³,Li Yanfang³

Affiliation:

1. Ph.D. Candidate, School of Automation, Northwestern Polytechnical Univ., Xi’an 710129, China (corresponding author). ORCID: .

2. Professor, School of Automation, Northwestern Polytechnical Univ., Xi’an 710129, China.

3. Ph.D. Candidate, School of Automation, Northwestern Polytechnical Univ., Xi’an 710129, 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-4678

Reference39 articles.

1. Propellant-Free Control of Tethered Formation Flight, Part 2: Nonlinear Underactuated Control

2. Artificial Gravity

3. Fractional order attitude stability control for sub-satellite of tethered satellite system during deployment;Gou X.-W.;Appl. Math. Modell.,2018

4. Overload control of artificial gravity facility using spinning tether system for high eccentricity transfer orbits

5. Integral sliding mode control for Euler-Lagrange systems with input saturation;Guo Y.;Int. J. Robust Nonlinear,2019

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