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Study of Flight/Thrust Control System Using H∞ Synthesis in Carrier Landing System(PDF)

《南京理工大学学报》(自然科学版)[ISSN:1005-9830/CN:32-1397/N]

Issue:
2003年03期
Page:
256-260
Research Field:
Publishing date:

Info

Title:
Study of Flight/Thrust Control System Using H∞ Synthesis in Carrier Landing System
Author(s):
YuYong YangYidong Dai
College of Automation Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing
Keywords:
carrier-based aircraft flight/ thrust system linear matrix inequality∞ control
PACS:
U674.7
DOI:
-
Abstract:
In this paper, the flight / thrust integ rated cont rol system ( FT ICS) with con stantα d , actual angle of at tack, using LMI-based H ∞ synthesis is developed. The FTICS de signed can improve the key performances of dynamic tracking and air wake disturbance rest rain ing and keep att itude and path angle constant even during the airplane passing through the ramp where the t racking radar doesn’ t w ork and the guidance sig nal is terminated. In view of eng ineering realization the H∞ controller order reduct ion method is also proposed. T he simula t ion result s indicate the new ly designed FTICS can satisfy the design specificat ions very w ell.

References:

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Last Update: 2013-03-17