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NASA NTRS · 19680056598

Application of C-minimax optimal control theory to flight control problems.

Abstract

Spacecraft and large launch vehicle nonoptimal /suboptimal/ controllers evaluated with Chebyshev minimax optimal control theory

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BibTeXRIS

Johnson, C. D., Redus, J. R.. 1968-08-01. Application of C-minimax optimal control theory to flight control problems.. https://ntrs.nasa.gov/citations/19680056598

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