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A quasi-analytical method for non-iterative computation of nonlinear controlsAn optimal control solution process was developed for a general class of nonlinear dynamical systems. The method combines control theory, perturbation methods, and Van Loan's recent matrix exponential results. A variety of applications support the practical utility of this method. Nonlinear rigid body optimal maneuvers are routinely solved. Flexible body dynamical systems of an order greater than 40 were solved. The method fails occasionally due to poor convergence of the perturbation expansion or numerical difficulties associated with computing the matrix exponential. The method is attractive because it appears to be a good candidate for semi-automation; no initial guess is required, and it usually converges at 2nd or 3rd order in minutes of machine time.
Document ID
19870013298
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Junkins, J. L.
(Texas A&M Univ. College Station, TX, United States)
Thompson, R. C.
(Texas A&M Univ. College Station, TX, United States)
Turner, J. D.
(Cambridge Research Associates Mass., United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1987
Publication Information
Publication: NASA. Marshall Space Flight Center Structural Dynamics and Control Interaction of Flexible Structures
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
87N22731
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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