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
收藏
页码：1565 / 1583
页数：19
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