Technical Papers
Sep 5, 2017

Deployment of Tethered Satellites in Low-Eccentricity Orbits Using Adaptive Sliding Mode Control

Publication: Journal of Aerospace Engineering
Volume 30, Issue 6

Abstract

Tethered-satellite systems have great potential in completing various space missions. However, existing researches mainly focus on the deployment of satellites in a circular orbit, whereas deployment in an elliptical orbit, especially with disturbances, is rarely studied. This study develops a new control strategy to deploy tethered satellites in a low-eccentricity elliptical orbit that also considers system uncertainties and external disturbances. First, the periodical solution of the librational motion of a tethered-satellite system in an elliptic orbit is calculated. Because there is no fixed equilibrium point for deployment in elliptical orbits, the periodical solution is set as the end condition for deployment. After that, the controllability of the system is verified and an open-loop tension-control law is optimized by particle swarm optimization (PSO) and the Nelder-Mead method. To eliminate effects from uncertainties in initial states and errors from the deployment mechanism, an adaptive sliding mode controller is designed to achieve high-precision trajectory tracking. The performance of the proposed controller is compared quantitatively with a proportion-derivative (PD) controller and normal sliding mode controller. Furthermore, Monte Carlo simulations are conducted to demonstrate the effectiveness and robustness of the proposed controller when subjected to uncertain initial states. The simulation results indicate that the proposed control strategy enables the stable deployment of tethered-satellite systems despite the uncertainties and perturbations.

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Acknowledgments

This work was supported by the 2011 International Science and Technology Cooperation Program of China and the Research and Development Program of Science and Technology of Shanxi Province, China (No. 2013KW09-02).

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 30Issue 6November 2017

History

Received: Feb 23, 2017
Accepted: May 30, 2017
Published online: Sep 5, 2017
Published in print: Nov 1, 2017
Discussion open until: Feb 5, 2018

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Authors

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Changqing Wang [email protected]
Associate Professor, School of Automation, Northwestern Polytechnical Univ., Xi’an 710072, China. E-mail: [email protected]
Ph.D. Candidate, Dept. of Mechanical and Biomedical Engineering, City Univ. of Hong Kong, Hong Kong SAR 999077, China (corresponding author). ORCID: https://orcid.org/0000-0003-1152-2456. E-mail: [email protected]
Professor, School of Automation, Northwestern Polytechnical Univ., Xi’an 710072, China. E-mail: [email protected]
Assistant Professor, School of Automation, Northwestern Polytechnical Univ., Xi’an 710072, China. E-mail: [email protected]

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