DocumentCode
489140
Title
Transmission Zeros of Flexible Spinning Spacecraft
Author
Williams, Trevor
Author_Institution
Department of Aerospace Engineering, University of Cincinnati, Cincinnati, Ohio 45221
fYear
1991
fDate
26-28 June 1991
Firstpage
2479
Lastpage
2480
Abstract
This paper shows that the transmission zeros of flexible spinning spacecraft exhibit properties entirely analogous to those of undamped, non-spinning flexible space structures. Thus, the extensive results concerning the zeros in the undamped case (relationships to the poles; sensitivites; computation) apply without change to the zeros of spinning flexible spacecraft.
Keywords
Actuators; Coaxial components; Filtering theory; Frequency selective surfaces; Matrix decomposition; Poles and zeros; Sensor systems; Space vehicles; Spinning; Transmission line matrix methods;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1991
Conference_Location
Boston, MA, USA
Print_ISBN
0-87942-565-2
Type
conf
Filename
4791849
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