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Solar Dynamics Observatory (SDO) HGAS Induced JitterThis paper presents the results of a comprehensive assessment of High Gain Antenna System induced jitter on the Solar Dynamics Observatory. The jitter prediction is created using a coupled model of the structural dynamics, optical response, control systems, and stepper motor actuator electromechanical dynamics. The paper gives an overview of the model components, presents the verification processes used to evaluate the models, describes validation and calibration tests and model-to-measurement comparison results, and presents the jitter analysis methodology and results.
Document ID
20080045421
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Liu, Alice
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Blaurock, Carl
(Nightsky Systems Raleigh, NC, United States)
Liu, Kuo-Chia
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Mule, Peter
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 24, 2013
Publication Date
April 7, 2008
Subject Category
Aeronautics (General)
Meeting Information
Meeting: 49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Location: Schaumburg, IL
Country: United States
Start Date: April 7, 2008
End Date: April 10, 2008
Sponsors: American Society of Civil Engineers, American Society of Mechanical Engineers, American Society for Composites, American Inst. of Aeronautics and Astronautics, American Helicopter Society, Inc.
Distribution Limits
Public
Copyright
Public Use Permitted.
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