scholarly journals Design of Flight Control System Using MIMO H^|^infin; Control Design Method Combined with Exact Model Matching Method

1994 ◽  
Vol 30 (7) ◽  
pp. 767-775
Author(s):  
Takashi KIMURA ◽  
Morio TAKAHAMA ◽  
Ei TOKUDA ◽  
Masahiro OHNO
Keyword(s):  
Control System ◽  
Flight Control ◽  
Design Method ◽  
Control Design ◽  
Model Matching ◽  
Flight Control System ◽  
Matching Method ◽  
Exact Model

scholarly journals H^|^infin; Control Design Method Combined with Exact Model Matching Method

1993 ◽  
Vol 29 (9) ◽  
pp. 1104-1113
Author(s):  
Takashi KIMURA ◽  
Morio TAKAHAMA ◽  
Ei TOKUDA ◽  
Masahiro OHNO
Keyword(s):  
Design Method ◽  
Control Design ◽  
Model Matching ◽  
Matching Method ◽  
Exact Model

A Rapid and Reliable System Design Method for Flight Control System

2021 ◽  
pp. 4917-4931
Author(s):  
Liu Changxiu ◽  
Wang Kaiqiang ◽  
Zhang Minjie ◽  
Chen Runfeng ◽  
Hou Yanze
Keyword(s):  
Control System ◽  
System Design ◽  
Flight Control ◽  
Design Method ◽  
Flight Control System ◽  
Reliable System

Modeling, control design, and influence analysis of catapult-assisted take-off process for carrier-based aircrafts

2017 ◽  
Vol 232 (13) ◽  
pp. 2527-2540 ◽  
Author(s):  
Ziyang Zhen ◽  
Ju Jiang ◽  
Xinhua Wang ◽  
Kangwei Li
Keyword(s):  
Control System ◽  
Flight Control ◽  
Control Design ◽  
Control Surface ◽  
Flight Control System ◽  
Influence Analysis ◽  
Surface Ship ◽  
Lateral Channel ◽  
And Performance ◽  
Longitudinal Channel

This paper addresses the problems of modeling, control design, and influence analysis of the steam catapult-assisted take-off process of the carrier-based aircrafts. The mathematical models of the carrier-based aircraft, steam catapult, landing gears, and the environmental factors including deck motion and bow airflow have been established to express the aircraft dynamics in the take-off process. An engineering method based automatic flight control system has been designed, which is divided into the longitudinal channel and lateral channel. The influences of the preset control surface, ship deck motion, ship bow airflow, and automatic flight control system system are tested by a series of simulations. The simulation results show that the elevator angle preset is necessary in the stage of accelerated running on the ship deck and the deck motion is the most important factor for safe take-off, while the ship bow airflow is beneficial for climbing up of the aircraft. The automatic flight control system gives the guarantee of safety and performance in the take-off process of the carrier-based aircraft.

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