Three-Dimensional Response Characteristics for Spacecraft with Deploying Flexible Appendages
K.W. Lips and V.J. Modi
Journal of Guidance, Control, and Dynamics ; 4 , 5 ; 650-656
1981
Article (Journal)
Electronic Resource
English
Approximate Solutions for Attitude Dynamics of a Spacecraft with Deploying Flexible Appendages
British Library Conference Proceedings | 1997
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