UNIFIED APPROACH TO ADAPTIVE VARIABLE-STRUCTURE CONTROL FOR ATTITUDE TRACKING IN VARIOUS PARAMETERIZATIONS

被引：0

作者：

Tanygin, Sergei ^{[1
]}

机构：

[1] Analyt Graph Inc, 220 Valley Creek Blvd, Exton, PA 19341 USA

来源：

ASTRODYNAMICS 2015 | 2016年 / 156卷

关键词：

SLIDING-MODE CONTROL; CONTROL INPUT SATURATION; LARGE-ANGLE MANEUVERS; RODRIGUES PARAMETERS; SPACECRAFT; STABILIZATION;

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The adaptive variable-structure control for attitude tracking is examined in general terms. The earlier formulation developed in terms of quaternion components is reexamined in a more general form suitable for other attitude parameterizations. The adaptive control laws are modified to address the unwinding phenomenon and to guarantee that the closed-loop error dynamics evolve along the shortest arcs. It is shown that different parameterizations provide additional degrees of freedom for improving parameter adaptation and closed-loop performance.

引用

页码：1565 / 1583

页数：19

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