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On the attitude stabilization of rigid spacecraft

โœ Scribed by Christopher I. Byrnes; Alberto Isidori

Publisher
Elsevier Science
Year
1991
Tongue
English
Weight
725 KB
Volume
27
Category
Article
ISSN
0005-1098

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The attitude stabilization problem of a rigid spacecraft using control torques supplied by gas jet actuators about only two of its principal axes is considered. If the uncontrolled principal axis of the spacecraft is not an axis of symmetry, then the complete spacecraft dynamics are small time local

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A three-dimensional rest-to-rest attitude maneuver of ยฏexible spacecraft equipped with onยฑo reaction jets is studied. Equations of motion of the spacecraft are developed by using Lagrangian formulation. The ยฎnite element method is used to discretize elastic deformations of a particular model of sate