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Elimination of uncontrollable rigid body mode, appendix CThe planar system model is examined which reveals two rigid body modes. One is due to the pure translation of the whole experiment assembly and is uncontrollable because the only control input is a torque at the gimbal. The other rigid body mode is due to the pointing of the gimbal and is the one for which control is sort. The problem arises from the Vector V2 which relates the control input to the modal coordinates. Since its fifth and sixth elements are both nonzero, neither body mode can be thrown away as is. The two rigid body modes must be transformed so that one is unaffected by the control input and one is left controllable. The uncontrollable mode can then be eliminated from the model for design purposes. A process is described to accomplish the elimination of the uncontrollable rigid body mode.
Document ID
19850005533
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Date Acquired
August 12, 2013
Publication Date
November 1, 1984
Publication Information
Publication: Definition of Ground Test for Verification of Large Space Struct. Control
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
85N13842
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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