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The Microwave Anisotropy Probe (MAP) MissionThe Microwave Anisotropy Probe mission is designed to produce a map of the cosmic microwave background radiation over the entire celestial sphere by executing a fast spin and a slow precession of its spin axis about the Sun line to obtain a highly interconnected set of measurements. The spacecraft attitude is sensed and controlled using an inertial reference unit, two star trackers, a digital sun sensor, twelve coarse sun sensors, three reaction wheel assemblies, and a propulsion system. This paper presents an overview of the design of the attitude control system to carry out this mission and presents some early flight experience.
Document ID
20020084567
Acquisition Source
Goddard Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Markley, F. Landis
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Andrews, Stephen F.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
ODonnell, James R., Jr.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Ward, David K.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Bauer, Frank H.
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA Paper 2002-4578
Report Number: AIAA Paper 2002-4578
Meeting Information
Meeting: AIAA Guidance, Navigation and Control Conference
Location: Monterey, CA
Country: United States
Start Date: August 5, 2002
End Date: August 8, 2002
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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