Young, Technical Monitor, who made numerous Finally, the authors wish to acknowledge the encouragement andĮfforts of Mr. Sible for running all of the eleven demonstration problems on the 360/95Ĭomputer.
Tractor a self authored subroutine to read NASTRAN output, and was respon. In addition, he supplied theĬontractor with a 360 system compatible plot package, furnished the con. With the GSFC IBM 360/95 computer system. Ted invaluable advice on requirements for making the program compatible Internal forces at the interconnect points. James Mason offered significant advice on the need to compute During the very early program development WilliamĬase provided valuable advice on the interfacing with NASTRAN output andĪlso he generated the demonstration problem utilized to validate the in. The subroutine used in the generation of root locus plots. To verify both the nonlinear time response and linear transfer functionĪnd stability analysis portions of the program. They provided the associated data which was used Tion and stability analysis portion of the program and defined 8 of the 11ĭemonstration problems. In particular, they layed out the basic approach which was to be used forĭata input, defined exactly what should be included in the transfer func. Ted many valuable technical comments and suggestions throughout the program The authors wish to acknowledge the assistance provided by Goddard Spaceįlight Center personnel. Istration, Goddard Space Flight Center, Greenbelt, Maryland, under the The study was performed from May 1973 to Aprilġ975 and was administered by the National Aeronautics and Space Admin.
Sults of a study whose purpose was to develop a computer program systemįor dynamic simulation and stability analysis of passive and activelyĬontrolled spacecraft. This report, prepared by the Dynamics and Loads Section, Martin MariettaĬorporation, Denver Division, under Contract NAS5-11996, presents the re. Volume 3: Demonstration problems"ĭEMONSTRATION PROBLEMS COMPUTER PROGRAM SYSTEM
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Full text of " NASA Technical Reports Server (NTRS) 19760018233: Computer program system for dynamic simulation and stability analysis of passive and actively controlled spacecraft.
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