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• W619216786 abstract "In this paper, the attitude tracking control problem is investigated for a rigid spacecraft. Robust finite time controllers based on the quaternion and Lagrange-like model are proposed to solve this problem with model uncertainties and external perturbations. The controllers guarantee the convergence of attitude tracking errors in fixed time, where the settling time can be set in advance, and this merit is different from all the existing controllers for spacecraft attitude tracking problem. The controllers are derived using the Lyapunov theory, so the stability of the closed-loop system is guaranteed. Moreover, the modified controllers are provided to alleviate the chattering phenomenon and eliminate the singular problem. Finally, simulation results are given to demonstrate the efficiency of the proposed methods." @default.
• W619216786 created "2016-06-24" @default.
• W619216786 creator A5000364056 @default.
• W619216786 creator A5054812413 @default.
• W619216786 date "2015-10-01" @default.
• W619216786 modified "2023-10-03" @default.
• W619216786 title "Fixed-time control for spacecraft attitude tracking based on quaternion" @default.
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• W619216786 doi "https://doi.org/10.1016/j.actaastro.2015.05.035" @default.
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