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Flight Dynamics Analysis BranchThis report summarizes the major activities and accomplishments carried out by the Flight Dynamics Analysis Branch (FDAB), Code 572, in support of flight projects and technology development initiatives in fiscal year 2000. The report is intended to serve as a summary of the type of support carried out by the FDAB, as well as a concise reference of key accomplishments and mission experience derived from the various mission support roles. The primary focus of the FDAB is to provide expertise in the disciplines of flight dynamics, spacecraft trajectory, attitude analysis, and attitude determination and control. The FDAB currently provides support for missions and technology development projects involving NASA, government, university, and private industry.
Document ID
20020013326
Acquisition Source
Goddard Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Stengle, Tom
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Flores-Amaya, Felipe
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Date Acquired
September 7, 2013
Publication Date
December 1, 2000
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:209971
Rept-2001-00785-0
NASA/TM-2000-209971
Funding Number(s)
PROJECT: RTOP 572-00-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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