A water tunnel investigation of the effects of pitch rate and yaw onLEX generated vortices of an F/A-18 fighter aircraft model

1991 ◽  
Author(s):  
SHESHAGIRI HEBBAR ◽  
MAX PLATZER ◽  
ODILON CAVAZOS
Keyword(s):  
Water Tunnel ◽  
Fighter Aircraft ◽  
Aircraft Model

Vortex breakdown studies of a canard-configured X-31A-like fighter aircraft model

1993 ◽  
Vol 30 (3) ◽  
pp. 405-408 ◽  
Author(s):  
Sheshagiri K. Hebbar ◽  
Max F. Platzer ◽  
Hui Man Kwon
Keyword(s):  
Vortex Breakdown ◽  
Fighter Aircraft ◽  
Aircraft Model

scholarly journals Delayed Antiwindup Control Using a Decoupling Structure

2013 ◽  
Vol 2013 ◽  
pp. 1-7 ◽  
Author(s):  
Huawei Zhu ◽  
Guozheng Qin ◽  
Yingxin Yan ◽  
Zhichao Jiang ◽  
Zhisheng Duan
Keyword(s):  
Control Problem ◽  
Linear Matrix Inequalities ◽  
Input Saturation ◽  
Linear Matrix ◽  
Matrix Inequalities ◽  
Fighter Aircraft ◽  
Aircraft Model

This paper investigates the antiwindup (AW) control problem for plants with input saturation. The AW compensator is not activated as soon as input saturation occurs as usual. A delayed decoupling structure is first proposed. Then, appropriate linear matrix inequalities (LMIs) are developed to determine a plant-order AW compensator. Effectiveness of the presented AW technique is illustrated by a fighter aircraft model.

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