DocumentCode
1601603
Title
Stability analysis of reduced-stiffness photovoltaic arrays on MB-6 and MB-15 configurations of space station Freedom
Author
Moseley, Nathan L. ; Graham, Ronald E.
Author_Institution
Analex Corp., Fairview Park, OH, USA
fYear
1992
Firstpage
44
Abstract
Reduced-stiffness photovoltaic (PV) arrays on two configurations of the space station Freedom (SSF) were analyzed to determine stability trends. Flexible modes of the SSF in which array motion is considered dominant were chosen for analysis, and root locus plots were generated. Two symmetric configurations were studied. One had four arrays and a stiff truss, the other had eight arrays and large mass. For both models, three different beta joint control frequencies were found to be stable for nominal array stiffness through root locus analysis at a time-slice. Beta joint roots moved further into the left-half plane with increasing control frequency and/or array stiffness, while other control roots remained stationary. No modes became unstable with decreasing array stiffness
Keywords
aerospace control; attitude control; distributed parameter systems; large-scale systems; root loci; solar cell arrays; space vehicle power plants; stability; tracking systems; MB-15 configurations; MB-6 configuration; array motion; beta joint control frequencies; flexible modes; reduced-stiffness photovoltaic arrays; root locus plots; space station Freedom; stability analysis; stiff truss; symmetric configurations; Eigenvalues and eigenfunctions; Failure analysis; Frequency; Friction; Performance analysis; Photovoltaic systems; Solar power generation; Space shuttles; Space stations; Stability analysis;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Applications, 1992., First IEEE Conference on
Conference_Location
Dayton, OH
Print_ISBN
0-7803-0047-5
Type
conf
DOI
10.1109/CCA.1992.269901
Filename
269901
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