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Orbit determination software development for microprocessor based systems: Evaluation and recommendationsA guide is presented for National Aeronautics and Space Administration management personnel who stand to benefit from the lessons learned in developing microprocessor-based flight dynamics software systems. The essential functional characteristics of microprocessors are presented. The relevant areas of system support software are examined, as are the distinguishing characteristics of flight dynamics software. Design examples are provided to illustrate the major points presented, and actual development experience obtained in this area is provided as evidence to support the conclusions reached.
Document ID
19820021152
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Shenitz, C. M. (Computer Sciences Corp. Greenbelt, MD, United States)
Mcgarry, F. E. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Tasaki, K. K. (NASA Goddard Space Flight Center)
Date Acquired
September 4, 2013
Publication Date
July 1, 1980
Subject Category
Computer Programming And Software
Report/Patent Number
NASA-TM-84794
STL-80-001
NAS 1.15:84794
Accession Number
82N29028
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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