DYNAMIC RESPONSE OF A FLEXIBLE SPACECRAFT STRUCTURE DUE TO ATTITUDE CONTROL GENERATED MOTION
In the dynamic structural analyses of spacecraft, the structures are typically considered multibody mechanical systems consisting of rigid and flexible parts. The dynamic attitude of the rigid body, i.e., a spacecraft body, induces structural deformation in the flexible parts. The flexible struct...
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| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/66870 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |
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