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Optimal solar pressure attitude control of spacecraft—II: Large-angle attitude maneuvers

✍ Scribed by R. Venkatachalam; K.C. Pande


Publisher
Elsevier Science
Year
1982
Tongue
English
Weight
363 KB
Volume
9
Category
Article
ISSN
0094-5765

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A three-dimensional rest-to-rest attitude maneuver of ¯exible spacecraft equipped with on±o reaction jets is studied. Equations of motion of the spacecraft are developed by using Lagrangian formulation. The ®nite element method is used to discretize elastic deformations of a particular model of sate