A Tailless Fighter Aircraft Model for Control-Related Research and Development

2017 ◽  
Author(s):  
Michael A. Niestroy ◽  
Kenneth M. Dorsett ◽  
Katherine Markstein
Keyword(s):  
Research And Development ◽  
Fighter Aircraft ◽  
Related Research ◽  
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

Research and Implementation of Public Transport Query System Based on PHP

2014 ◽  
Vol 687-691 ◽  
pp. 1856-1859
Author(s):  
Lin Zhu
Keyword(s):  
Information System ◽  
Research And Development ◽  
Data Management ◽  
Public Transport ◽  
Economic Activities ◽  
Technology Design ◽  
Related Research ◽  
The Public ◽  
Query System

Public transport query system is the information system is dedicated to serving the public travel, it is an important part of city social and economic activities. In Hubei province, Lard city as a case study and implementation of transit oriented users query system, mainly the use of YHY technology, design and development of Apache +MySQL in +YHY environment. The system can realize the line inquiry, site query, transfer query and data management and other functions, is feasible and good expansibility, and provides the beneficial reference for the related research and development information system.

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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