MODELING OF THE SLEWING CONTROL OF A FLEXIBLE STRUCTURE

被引:34
作者
GARCIA, E
INMAN, DJ
机构
[1] State University of New York at Buffalo, Department of Mechanical and Aerospace Engineering, Buffalo, NY
基金
美国国家航空航天局;
关键词
D O I
10.2514/3.20707
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper presents a formulation for the modeling of a single-link flexible beam that is undergoing slewing motion at an actively controlled pinned end, where the other end of the beam is free. This pinned end, or slewing axis, is of fixed orientation such that the beam rotates in the horizontal plane. A geared DC electric motor is connected to the beam at the slewing axis. A position and a velocity sensor are placed at this hinged location, and their proportional feedback provides a position control system about the slewing axis. The motor characteristics, gear ratio, and the position feedback constant determine an equivalent rotational spring constant, often called the servo stiffness. This paper generalizes the structure's boundary conditions at the slewing axis to include the effects of the servo system. It is shown that the clamped-free beam assumption for the dynamics of the structure is a valid assumption if the ratio of the servo stiffness to beam flexibility is high. However, for moderate or low values of this ratio, the clamped-free beam leads to erroneous system models so that it becomes necessary to consider the effects of the driving servo on the dynamics of the flexible beam.
引用
收藏
页码:736 / 742
页数:7
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