Fixed-time terminal sliding mode control of spinning tether system for artificial gravity environment in high eccentricity orbit-Reference-Cited by-同舟云学术

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Fixed-time terminal sliding mode control of spinning tether system for artificial gravity environment in high eccentricity orbit

Published:2020-12 Issue: Volume:177 Page:834-841
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Li Ai-jun,Tian Hao-chang,Wang Chang-qing

Funder

Fundamental Research Funds for the Central Universities

Shaanxi Science and Technology Program

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference30 articles.

1. Bone mineral and lean tissue loss after long duration space flight;LeBlanc;J. Musculoskel. Neuron.,2000

2. Medical investigations and resulting countermeasures in support of 16-day Space Shuttle missions;Sawin;J. Gravitational Physiol.,1998

3. Artificial Gravity;Clément,2007

4. Dynamic Analysis of Space Tether Missions;Levin,2007

5. Dynamics of Tethered Satellite Systems;Aslanov,2012

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1. The effects of deployment friction on the dynamics of nonconductive space tethers;Acta Astronautica;2024-01

2. Spin-Up and Appointed Time Attitude Control of Tethered Spacecraft for Artificial Gravity;Journal of Aerospace Engineering;2023-09

3. Underactuated attitude tracking control of tethered spacecraft for deployment and spin-up;Advances in Space Research;2023-06

4. Spin deployment of Hub-Spoke tethered satellite formation with sliding mode tether tension control;Advances in Space Research;2023-03

5. Robust adaptive control for rotational deployment of an underactuated tethered satellite system;Acta Astronautica;2023-02

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