NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Numerical approach for solving rigid spacecraft minimum time attitude maneuvers
Document ID
19900032502
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Li, Feiyue
(Howard Univ. Washington, DC, United States)
Bainum, Peter M.
(Howard University Washington, DC, United States)
Date Acquired
August 14, 2013
Publication Date
February 1, 1990
Publication Information
Publication: Journal of Guidance, Control, and Dynamics
Volume: 13
ISSN: 0731-5090
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
90A19557
Funding Number(s)
CONTRACT_GRANT: NSG-1414
Distribution Limits
Public
Copyright
Other

Available Downloads

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