A singular adaptive attitude control with active disturbance rejection

被引:18
作者
Bai, Yuliang [1 ]
Biggs, James D. [2 ]
Wang, Xiaogang [1 ]
Cui, Naigang [1 ]
机构
[1] Harbin Inst Technol, Sch Astronaut, Mailbox 345, Harbin 150001, Peoples R China
[2] Politecn Milan, Dept Aerosp Sci & Technol, I-20156 Milan, Italy
关键词
Nano-spacecraft; Inverse control; Quaternion feedback control; Linear extended state observer; Singular quaternion feedback control; TRACKING CONTROL; CONTROL DESIGN; SPACECRAFT; CONVERGENCE;
D O I
10.1016/j.ejcon.2017.01.002
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper develops a quaternion attitude tracking control with an adaptive gains parameter that can be tuned to compensate for disturbances with known bound. The adaptive gain is described by a simple, but singular, differential equation and the corresponding adaptive control is shown to asymptotically track a reference attitude. However, this control requires the bound on the disturbance torque to be known in order to appropriately tune the controller to compensate for it. Using a linear state observer to estimate the disturbance torque and compensating for the disturbance at each sampling period the adaptive control can achieve asymptotic tracking in the presence of an unknown disturbance torque. In this case the error in the estimation, rather than the entire disturbance, is compensated for by the adaptive gain at each sampling period. Simulations demonstrate that an improved tracking performance can be achieved when compared to standard quaternion tracking controls. (C) 2017 European Control Association. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:50 / 56
页数:7
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