A general formulation for librational dynamics of spacecraft with deploying appendages
MODI, V. J., IBRAHIM, A. M.
Journal of Guidance, Control, and Dynamics ; 7 , 5 ; 563-569
1984
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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