Quaternion-Based Non-Singular Terminal Sliding Mode Control for a Satellite-Mounted Space Manipulator

被引:1
作者
Giordano, Jacopo [1 ]
Cenedese, Angelo [1 ]
机构
[1] Univ Padua, Dept Informat Engn, I-35131 Padua, Italy
来源
IEEE CONTROL SYSTEMS LETTERS | 2023年 / 7卷 / 2659-2664期
关键词
Quaternions; Aerospace electronics; Space vehicles; Manipulator dynamics; Uncertainty; Arms; Angular velocity; Space manipulator; quaternions; Index Terms; sliding mode control; robust control; free-flying;
D O I
10.1109/LCSYS.2023.3288260
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In this letter, a robust control solution for a satellite equipped with a robotic manipulator is presented. First, the dynamical model of the system is derived based on quaternions to describe the evolution of the attitude of the base satellite. Then, a non-singular terminal sliding mode controller that employs quaternions for attitude control, is proposed for concurrently handling all the degrees of freedom of the system. Moreover, an additional adaptive term is embedded in the controller to estimate the upper bounds of disturbances and uncertainties. The result is a resilient solution able to withstand unmodelled dynamics and interactions. Lyapunov theory is used to prove the stability of the controller and numerical simulations allow assessing performance and fuel efficiency.
引用
收藏
页码:2659 / 2664
页数:6
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