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Analytic Drag Controller guidance gains evaluation. Mission planning, mission analysis and software formulationResults 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.
Document ID
19760020210
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Treybig, J. H. (McDonnell-Douglas Technical Services Co., Inc. Houston, TX, United States)
Date Acquired
September 3, 2013
Publication Date
February 28, 1975
Subject Category
Astrodynamics
Report/Patent Number
REPT-1.4-4-6
NASA-CR-147813
Report Number: REPT-1.4-4-6
Report Number: NASA-CR-147813
Accession Number
76N27298
Funding Number(s)
CONTRACT_GRANT: NAS9-13970
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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