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The Application of Eigenstructure Assignment to the Design of Flight Control Systems

Faleiro, L. F. (1999) The Application of Eigenstructure Assignment to the Design of Flight Control Systems. In: The Application of Eigenstructure Assignment to the Design of Flight Control Systems

Full text not available from this repository.

Abstract

Modern control methods have often been advocated by academics as able to solve fairly complex control engineering design problems in the aircraft industry. However, evidence suggests that practice is still geared towards using classical techniques, even on the most modern fighter aircraft which are open-loop unstable. This thesis stems from a need to understand the reasons for this. Modern methods are examine din order to determine their strengths and weaknesses when applied to industrial problems.

Document Type:Book Section
Additional Information: LIDO-Berichtsjahr=2000, thesis_type=thesis,
Title:The Application of Eigenstructure Assignment to the Design of Flight Control Systems
Authors:
AuthorsInstitution or Email of Authors
Faleiro, L. F.UNSPECIFIED
Date:1999
Journal or Publication Title:The Application of Eigenstructure Assignment to the Design of Flight Control Systems
Refereed publication:Yes
In ISI Web of Science:No
Editors:
EditorsEmail
Faleiro, L.F.UNSPECIFIED
Status:Published
Keywords:Eigenstructure assignment, flight control, modern control
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):UNSPECIFIED
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of Robotics and Mechatronics
Deposited By: elib DLR-Beauftragter
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 17:35

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