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Dynamic attitude command and control of the TOPEX/Poseidon spacecraftThe dynamic control laws utilized by the TOPEX/Poseidon (T/P) spacecraft attitude determination and control subsystem to command and maneuver the satellite during normal mission mode (NMM) laws are described. Results show that the vehicle is able to respond to the dynamic attitude commands while at the same time providing ample disturbance rejection capability.
Document ID
19910065043
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Zimbelman, D. F. (Fairchild Space Co. Germantown, MD, United States)
Lee, B. B. (Fairchild Space Co. Germantown, MD, United States)
Welch, R. V. (Fairchild Space and Defense Corp. Germantown, MD, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1991
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 91-2703
Meeting Information
Meeting: AIAA Guidance, Navigation and Control Conference
Location: New Orleans, LA
Country: United States
Start Date: August 12, 1991
End Date: August 14, 1991
Accession Number
91A49666
Distribution Limits
Public
Copyright
Other

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