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Nonlinear modeling, identification and estimation of slew induced structural deformationThis proposal discusses a new nonlinear, nonparametric method for off-line modeling and on-line estimation of the deformation of a flexible structure undergoing rapid retargeting maneuvers. In these circumstances, the structural stiffness and damping coefficients depend on the angular acceleration omega(dot), the angular rate omega, and the square of the angular rate omega. In the single axis case, the excitation of the structure is represented by the vector u(exp T) = (omega(dot), omega(exp 2), 2(omega)), to which the structural dynamics responds as a 'bilinear' (i.e., parametrically excited) system. A similar technique for multiaxial rotations yields a bilinear model with respect to matrix valued excitations. Three methods of estimation and modeling are described in this proposal to achieve deformation state determination: (1) a method based on a feedback linearized procedure which gives an estimate of the state by means of observers installed in the deformable body; (2) off-line modeling of the deformation state of the structure by means of topological interpolators; and (3) an on-line structural state estimation method based on a combination of the two previous techniques.
Document ID
19930075296
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Dwyer, Thomas A., III
(Illinois Univ. Urbana-Champaign, IL, United States)
Karray, Fakhreddine
(Illinois Univ. Urbana-Champaign, IL, United States)
Date Acquired
August 16, 2013
Publication Date
March 24, 1988
Publication Information
Publication: JPL, Model Determination for Large Space Systems, Volume 3
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
93N72743
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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