Robust Stability Clearance of Flight Control Law Based on Global Sensitivity Analysis
To validate the robust stability of the flight control system of hypersonic flight vehicle, which suffers from a large number of parametrical uncertainties, a new clearance framework based on structural singular value (μ) theory and global uncertainty sensitivity analysis (SA) is proposed. In this f...
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| Main Authors: | Liuli Ou, Lei Liu, Shuai Dong, Yongji Wang |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2014-01-01
|
| Series: | Journal of Applied Mathematics |
| Online Access: | http://dx.doi.org/10.1155/2014/153602 |
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