Finite-time relative pose tracking control for uncertain spacecraft rendezvous and docking
This study investigates the robust finite-time pose tracking control for spacecraft autonomous rendezvous and docking with parametric uncertainties and bounded external disturbances. Based on the uncertainly coupled relative pose dynamics, a fast terminal sliding mode controller is developed to achi...
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rr-article-140349052021-11-30T00:00:00Z Finite-time relative pose tracking control for uncertain spacecraft rendezvous and docking Liang Sun (92795) Jinwei Wang (299321) Jingjing Jiang (5731739) Spacecraft This study investigates the robust finite-time pose tracking control for spacecraft autonomous rendezvous and docking with parametric uncertainties and bounded external disturbances. Based on the uncertainly coupled relative pose dynamics, a fast terminal sliding mode controller is developed to achieve the finite-time convergence of the pose tracking errors. To reduce the control chattering results from the signum function in the controller, an exponential reaching law is employed to achieve the decreasing of the reaching time towards the sliding surface. The explicit tuning rules for designing parameters are derived based on the stability analysis of the closed-loop system. It is proved in Lyapunov framework that all closed-loop signals are always kept bounded and the pose tracking error converges to small neighborhood of zero in finite time. Simulation results validate the performance of the proposed robust finite-time control strategy. 2021-11-30T00:00:00Z Text Conference contribution 2134/14034905.v1 https://figshare.com/articles/conference_contribution/Finite-time_relative_pose_tracking_control_for_uncertain_spacecraft_rendezvous_and_docking/14034905 All Rights Reserved |
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Spacecraft Liang Sun Jinwei Wang Jingjing Jiang Finite-time relative pose tracking control for uncertain spacecraft rendezvous and docking |
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This study investigates the robust finite-time pose tracking control for spacecraft autonomous rendezvous and docking with parametric uncertainties and bounded external disturbances. Based on the uncertainly coupled relative pose dynamics, a fast terminal sliding mode controller is developed to achieve the finite-time convergence of the pose tracking errors. To reduce the control chattering results from the signum function in the controller, an exponential reaching law is employed to achieve the decreasing of the reaching time towards the sliding surface. The explicit tuning rules for designing parameters are derived based on the stability analysis of the closed-loop system. It is proved in Lyapunov framework that all closed-loop signals are always kept bounded and the pose tracking error converges to small neighborhood of zero in finite time. Simulation results validate the performance of the proposed robust finite-time control strategy. |
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Default Conference proceeding |
author |
Liang Sun Jinwei Wang Jingjing Jiang |
author_facet |
Liang Sun Jinwei Wang Jingjing Jiang |
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Liang Sun (92795) |
title |
Finite-time relative pose tracking control for uncertain spacecraft rendezvous and docking |
title_short |
Finite-time relative pose tracking control for uncertain spacecraft rendezvous and docking |
title_full |
Finite-time relative pose tracking control for uncertain spacecraft rendezvous and docking |
title_fullStr |
Finite-time relative pose tracking control for uncertain spacecraft rendezvous and docking |
title_full_unstemmed |
Finite-time relative pose tracking control for uncertain spacecraft rendezvous and docking |
title_sort |
finite-time relative pose tracking control for uncertain spacecraft rendezvous and docking |
publishDate |
2021 |
url |
https://hdl.handle.net/2134/14034905.v1 |
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1797459192164909056 |