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On the shape and orientation control of an orbiting shallow spherical shell structureA proposed method for controlling the shape and orientation of very large shallow dish type receiver/reflectors to be used in communication, radiometry and in electronic orbital based mail systems involves connecting a rigid light weight dumbell with heavy tip masses to the shell at its apex by a spring loaded double gimballed joint with dampling. To completely damp the system transient motion in all of the important lower frequency modes, an active control system is required. A mathematical model is extended to include the effects of point actuators located at preselected positions on the shell surface. The formulation of the uncontrolled dynamics assumes an a priori knowledge of the frequencies of all the elastic modes to be incorporated within the system model. As an example, three rigid body modes and six elastic modes are included in the model and six actuators are assumed, none of which lies on a nodal line or circle.
Document ID
19820003227
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bainum, P. M.
(Howard Univ. Washington, DC, United States)
Reddy, A. S. S. R.
(Howard Univ. Washington, DC, United States)
Date Acquired
September 4, 2013
Publication Date
July 9, 1981
Subject Category
Ground Support Systems And Facilities (Space)
Report/Patent Number
NASA-CR-164970
Report Number: NASA-CR-164970
Meeting Information
Meeting: Joint IFAC/ESA Symp. on Automatic Control in Space
Location: Noordwijkerhout
Country: Netherlands
Start Date: July 5, 1981
End Date: July 9, 1981
Accession Number
82N11100
Funding Number(s)
CONTRACT_GRANT: NSG-1414
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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