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Design and Stability of an On-Orbit Attitude Control System Using Reaction Control ThrustersNASA is providing preliminary design and requirements for the Space Launch System Exploration Upper Stage (EUS). The EUS will provide upper stage capability for vehicle ascent as well as on-orbit control capability. Requirements include performance of on-orbit burn to provide Orion vehicle with escape velocity. On-orbit attitude control is accommodated by a on-off Reaction Control System (RCS). Paper provides overview of approaches for design and stability of an attitude control system using a RCS.
Document ID
20160001818
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Hall, Robert A. (Jacobs Engineering and Science Services and Skills Augmentation Group (ESSSA) Huntsville, AL, United States)
Hough, Steven (Jacobs Engineering and Science Services and Skills Augmentation Group (ESSSA) Huntsville, AL, United States)
Orphee, Carolina (NASA Marshall Space Flight Center Huntsville, AL, United States)
Clements, Keith (Jacobs Engineering and Science Services and Skills Augmentation Group (ESSSA) Huntsville, AL, United States)
Date Acquired
February 16, 2016
Publication Date
January 4, 2016
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
M16-5024
Report Number: M16-5024
Meeting Information
Meeting: AIAA SciTech 2016
Location: San Diego, CA
Country: United States
Start Date: January 4, 2016
End Date: January 8, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNM12AA41C
Distribution Limits
Public
Copyright
Public Use Permitted.

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