Attitude Determination Error Analysis System (ADEAS) mathematical specification document
By: prepared by Computer Sciences Corporation ; M. NIcholson, F. Markley, E. Seidewitz.
Contributors: Markley, F.; Seidewitz, Ed.; Computer Sciences Corporation.; Goddard Space Flight Center.
Series: NASA CR -- 189281.; NASA contractor report -- NASA CR-189281.
Publisher: Goddard Space Flight Center
Published: 1988
Place of publication: [Greenbelt, Md.]
Language: eng
Format: Microform
Subjects: Atitude (inclination); Attitude control.; Attitude indicators.; Error analysis.; Mathematical models.; Spacecraft control.; Specifications.; Spin stabilization.
Notes: Also available via Internet from the NASA Technical Report Server web site. Address as of 5/9/06: http://ntrs.nasa.gov/archive/nasa/casi/ntrs.nasa.gov/19920018967%5F1992018967.pdf ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1992]. 2 microfiches.