Bending modes analysis in atmospheric flight for heavy launcher
This report presents the bending modes study conducted on a heavy launcher. The controller of the launcher takes as inputs the attitude and attitude rate measurements given by the Inertial Measurement Unit (IMU). Since the bending modes generate measurement errors at the IMU location, the study of d...
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| Format: | Others |
| Language: | English |
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KTH, Flygdynamik
2019
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-265615 |