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Linear Covariance Analysis of Closed-Loop Attitude Determination and Control System of Sub-Arcsec Pointing Three-Axes Spacecraft
By: Divya Bhatia.
Pub. 2019,
17pgs.
PDF File.
AAS 19-739.
Price: $29.00
Reprinted from Astrodynamics 1999, Advances in the Astronautical Sciences, Vol 171
This item is an
electronic document
and will be delivered by email to the address you provide within two business days.