Spacecraft Attitude Control with Input Quantization

被引：76
|
作者：
Wu, Baolin [1 ]
机构：
[1] Harbin Inst Technol, Res Ctr Satellite Technol, Harbin 150080, Peoples R China
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2016年 / 39卷 / 01期
基金：
中国国家自然科学基金;
关键词：
TRACKING;
D O I：
10.2514/1.G001427
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A feedback control scheme is proposed for a spacecraft attitude stabilization system with quantized control torque. A logarithmic type quantizer is studied, which has sufficient precision and requires a low communication rate. The quantization parameter is chosen based on the given controller design parameters and inertial matrix of spacecraft, which ensure the system stability and stabilization error within an adjustable bound. Simulation results demonstrate the effectiveness of the proposed control scheme.
引用
收藏
页码：176 / 180
页数：5
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