Maximized gust loads for a nonlinear airplane using matched filter theory and constrained optimization
Maximized gust loads for a nonlinear airplane using matched filter theory and constrained optimization
- New search for: Scott, Robert C.
- New search for: Pototzky, Anthony S.
- New search for: Perry, Boyd, III
- New search for: Scott, Robert C.
- New search for: Pototzky, Anthony S.
- New search for: Perry, Boyd, III
Two matched filter theory based schemes are described and illustrated for obtaining maximized and time correlated gust loads for a nonlinear aircraft. The first scheme is computationally fast because it uses a simple 1-D search procedure to obtain its answers. The second scheme is computationally slow because it uses a more complex multi-dimensional search procedure to obtain its answers, but it consistently provides slightly higher maximum loads than the first scheme. Both schemes are illustrated with numerical examples involving a nonlinear control system.
Document information
Maximized gust loads for a nonlinear airplane using matched filter theory and constrained optimization
1991 AIAA Atmospheric Flight Mechanics Conference ; 1991 ; New Orleans, LA, United States
1991-09-01
Conference paper
No indication
English
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