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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Bibliographic Details
Main Author: Joshi, Praveen Sudhakar
Format: Thesis eBook
Language:English
Published: [Place of publication not identified] : [publisher not identified] ; 1999.
Subjects:
Online Access:Link to OAKTrust copy

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Cushing: Theses & Dissertations Microforms (Does not check out)

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Call Number: 1999 Thesis J68
 
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1999 Thesis J68 Available

Available Online

Holdings details from Available Online
Call Number: 1999 Thesis J68
 
Call Number Status Get It
1999 Thesis J68 Available