Direct comparison of Neural Network, Fuzzy Logic and Model Prediction Variable Structure vortex flow controllers /
Current fighter aircraft are required to be maneuverable and agile at high angles of attack. Limited control power available at these extreme flight conditions prompts the need to use control augmentation techniques. The method of tangential slot blowing is found to be an effective technique. This t...
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| Format: | Thesis eBook |
| Language: | English |
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[Place of publication not identified] :
[publisher not identified] ;
1999.
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| Online Access: | Link to OAKTrust copy |
Internet
Link to OAKTrust copyCushing: Theses & Dissertations Microforms (Does not check out)
| Call Number: |
1999 Thesis J68 |
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|---|---|---|
| Call Number | Status | Get It |
| 1999 Thesis J68 | Available | |
Available Online
| Call Number: |
1999 Thesis J68 |
|
|---|---|---|
| Call Number | Status | Get It |
| 1999 Thesis J68 | Available | |