NASA NTRS ยท 19840016411
Mathematical analysis
Abstract
Simple continuum models used in the design, analysis, and control of large space structures are examined. Particular emphasis is placed on boundary value problems associated with the Load Correction Method and control problems involving partial differential equations for the large space structure models. Partial differential equations will be used to model a large space structure, base the design of an optimal controller on this model, approximate the resulting optimal control model, and compare the results with data from other methods.
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Donaldson, J. A.. 1984-03-22. Mathematical analysis. https://ntrs.nasa.gov/citations/19840016411
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