Nonlinear model order reduction for rapid gust loads analysis of flexible manoeuvring aircraft
This paper describes a systematic approach to the nonlinear model order reduction of free-flying flexible aircraft and the subsequent flight control system design. System nonlinearities arise due to large wing deformations and the coupling between flexible and rigid-body dynamics. The nonlinear flig...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
2015-05-08.
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| Subjects: | |
| Online Access: | Get fulltext |