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Hybrid coordinate formulation used for the design of attitude control systems for flexible spacecraftFormulation combines certain advantages of discrete and distributed coordinates by using both simultaneously. In report summarizing method, theoretical development is extended as necessary for applications of practical interest. Explicit analyses are presented in sufficient detail to establish utility in flexible space vehicle control system of hybrid coordinate formulation.
Document ID
19730000300
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Likins, P. W. (UCLA)
Fleisher, E. E.
Date Acquired
August 7, 2013
Publication Date
July 1, 1973
Subject Category
Mathematics And Information Sciences
Report/Patent Number
NPO-11714
Accession Number
73B10300
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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