NASA NTRS · 19760020210
Analytic Drag Controller guidance gains evaluation. Mission planning, mission analysis and software formulation
Abstract
Results of a study to optimize the guidance gains for the analytical drag control entry guidance system are presented. The guidance gains were optimized for study points chosen in all phases of entry.
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Treybig, J. H.. 1975-02-28. Analytic Drag Controller guidance gains evaluation. Mission planning, mission analysis and software formulation. https://ntrs.nasa.gov/citations/19760020210
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