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Flight Dynamics Analysis Branch End of Fiscal Year 2004 ReportThis report summarizes the major activities and accomplishments carried out by the Flight Dynamics Analysis Branch (FDAB), Code 595, in support of flight projects and technology development initiatives in Fiscal Year (FY) 2004. 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 including spacecraft navigation (autonomous and ground based); spacecraft trajectory design and maneuver planning; attitude analysis; attitude determination and sensor calibration; and attitude control subsystem (ACS) analysis and design. The FDAB currently provides support for missions and technology development projects involving NASA, other government agencies, academia, and private industry.
Document ID
20050175692
Acquisition Source
Goddard Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
DeLion, Anne
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Stengle, Thomas
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 7, 2013
Publication Date
February 28, 2005
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA/TM-2005?212777
Rept-2005-00908-0
Report Number: NASA/TM-2005?212777
Report Number: Rept-2005-00908-0
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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