Experiences with dynamic load simulation by means of modal forces in the presence of structural non-linearities

被引:10
|
作者
Goege, Dennis
Sinapius, J. Michael
机构
[1] Inst Composite Struct & Adapt Syst, D-38108 Braunschweig, Germany
[2] German Aerosp Ctr, Inst Aeroelast, D-37073 Gottingen, Germany
关键词
dynamic qualification; modal force combination; structural non-linearities;
D O I
10.1016/j.ast.2006.02.001
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The dynamic qualification of space structures today is performed by means of driven base tests in order to simulate the dynamic environment during launch. This method is limited to structures that fit onto the shaker facility. For large and unwieldy structures an alternative approach can be utilised which applies modal forces for the qualification. Modal forces are patterns of single forces that are able to excite single resonances. These force patterns can be applied by movable electrodynamic shakers. This article reviews the background of the method. A test strategy is proposed which is based on narrow-banded swept sine excitation and considers structural non-linearities observed frequently. The qualification method was utilised during the qualification of the European Robotic Arm (ERA). The experiences gained during the test campaign are compiled in the paper. The advantages and disadvantages of dynamic qualification by means of modal forces are discussed. (C) 2006 Elsevier SAS. All rights reserved.
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页码:411 / 419
页数:9
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