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An onboard deorbit target line computation techniqueThe design concept and results of a target line generator software package, which was developed to provide the onboard entry interface range, were documented. This generator, which was eventually reduced to one linear equation, was developed to the point that it provides autonomous landing site relocation capability, negligible core storage, and acceptable performance for the cases tested.
Document ID
19760024154
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bedford, J. J.
(McDonnell-Douglas Technical Services Co., Inc. Houston, TX, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1976
Subject Category
Astrodynamics
Report/Patent Number
NASA-CR-150939
DN-1.4-4-21
Report Number: NASA-CR-150939
Report Number: DN-1.4-4-21
Accession Number
76N31242
Funding Number(s)
CONTRACT_GRANT: NAS9-14960
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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