Attitude dynamics of a three-axis stabilized satellite with a large flexible solar array
Guidance and Control Conference ; 1972 ; Stanford , CA , U.S.A.
1972-01-01
Conference paper
Electronic Resource
English
Optimal attitude control for three-axis stabilized flexible spacecraft
Online Contents | 2005
|A flexible attitude control system for three-axis stabilized nanosatellites
DataCite | 2018
|