Analysis of aircraft pitch axis stability augmentation system using sum of squares optimization
The aircraft pitch axis stability augmentation system was analyzed using sum of squares optimization. The nonlinear dynamics of the pitch axis of a fictitious Aircraft - the Robust Civil Aircraft Model (RCAM) was considered. A LTI dynamic inversion based control law for the short period dynamics of...
| Main Authors: | , , , |
|---|---|
| 格式: | Journal article |
| 語言: | English |
| 出版: |
2005
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Analysis of aircraft pitch axis stability augmentation system using sum of squares optimization
出版 2005
Conference item
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Analysis of aircraft pitch axis stability augmentation system using sum of squares optimization
出版 2005
Conference item