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Flight Dynamics Analysis SystemFlight Dynamics Analysis System (FDAS) collection of computer programs provides environment for configuration and study of Ada software. Designed to support flight-dynamics research and analysis activities concerning software models, algorithms, and techniques used within flight Dynamics Division at Goddard Space Flight Center. Assists analysts and programmers in building, testing, and evaluating applications software by providing integrated support system for modification and reconfiguration of software. Includes capability of assembling reusable software components into applications programs, and reconfiguring assembled program after partially or fully completed. Developed in Ada for use on DEC VAX computer operating under VMS 4.3 or higher and version 1.3 or higher of VAX Ada Compilation System (ACS).
Document ID
19900000288
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Tasaki, Keiji
(Computer Sciences Corp.)
Jun, Lenda
(Computer Sciences Corp.)
Seidewitz, ED
(Computer Sciences Corp.)
Date Acquired
August 14, 2013
Publication Date
June 1, 1990
Publication Information
Publication: NASA Tech Briefs
Volume: 14
Issue: 6
ISSN: 0145-319X
Subject Category
Mathematics And Information Sciences
Report/Patent Number
GSC-13163
Report Number: GSC-13163
ISSN: 0145-319X
Accession Number
90B10288
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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