NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Galileo dual-spin attitude and articulation control systemGalileo, the first outer planet explorer to be configured as a dual spinner, will conduct intensive investigation of Jupiter's atmosphere, satellites, and magnetosphere. The exacting mission, coupled with the inherently complex spin and flexible body dynamics of the vehicle, demands careful design of the Galileo Attitude and Articulation Control System (AACS). A brief overview of the Galileo mission and spacecraft is presented, followed by a detailed discussion on the mechanization of the AACS and the many factors that influence its design. Included are discussions on attitude determination and control, high-gain antenna pointing, science scan platform pointing, nutation damping, wobble compensation, spin and despin control, and propellant migration and boom flexibility effects.
Document ID
19780066311
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Ward, R. S.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 78-1268
Meeting Information
Meeting: Guidance and Control Conference
Location: Palo Alto, CA
Start Date: August 7, 1978
End Date: August 9, 1978
Accession Number
78A50220
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available