Model-free Adaptive Control for Spacecraft Attitude

被引：0

作者：

Ran Xie ^{[1
]}

Ting Song ^{[2
,3
]}

Peng Shi ^{[1
]}

Yushan Zhao ^{[1
]}

机构：

[1] School of Astronautics,Beihang University

[2] Shanghai Institute of Spaceflight Control Technology

[3] Shanghai Key Laboratory of Aerospace Intelligent Control

来源：

Journal of Harbin Institute of Technology | 2016年 / 23卷 / 06期

关键词：

D O I：

暂无

中图分类号：

V448.22 [姿态控制系统];

学科分类号：

摘要：

A model-free adaptive control method is proposed for the spacecrafts whose dynamical parameters change over time and cannot be acquired accurately. The algorithm is based on full form dynamic linearization.A dimension reduction matrix is introduced to construct an augmented system with the same dimension input and output. The design of the controller depends on the system input and output data rather than the knowledge of the controlled plant. The numerical simulation results show that the improved controller can deal with different models with the same set of controller parameters,and the controller performance is better than that of PD controller for the time-varying system with disturbance.

引用

页码：61 / 66

页数：6

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