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  4. Modal matching for LPV model reduction of aeroservoelastic vehicles
 
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Modal matching for LPV model reduction of aeroservoelastic vehicles

Publikationstyp
Conference Paper
Date Issued
2015
Sprache
English
Author(s)
Theis, Julian  orcid-logo
Werner, Herbert  
Takarics, Béla  
Pfifer, Harald  
Balas, Gary  
Institut
Flugzeug-Systemtechnik M-7  
Regelungstechnik E-14  
TORE-URI
http://hdl.handle.net/11420/11404
Citation
AIAA Atmospheric Flight Mechanics Conference, 2015 (): - (2015)
Contribution to Conference
AIAA Atmospheric Flight Mechanics Conference, 2015  
Publisher DOI
10.2514/6.2015-1686
Scopus ID
2-s2.0-84958566637
Publisher
Aerospace Research Central
A model order reduction method is proposed for models of aeroservoelastic vehicles in the linear parameter-varying (LPV) systems framework, based on state space interpolation of modal forms. The dynamic order of such models is usually too large for control synthesis and implementation since they combine rigid body dynamics, structural dynamics and unsteady aerodynamics. Thus, model order reduction is necessary. For linear time-invariant (LTI) models, order reduction is often based on balanced realizations. For LPV models, this requires the solution of a large set of linear matrix inequalities (LMIs), leading to numerical issues and high computational cost. The proposed approach is to use well developed and numerically stable LTI techniques for reducing the LPV model locally and then to transform the resulting collection of systems into a consistent modal representation suitable for interpolation. The method is demonstrated on an LPV model of the body freedom flutter vehicle, reducing the number of states from 148 to 15. The accuracy of the reduced order model (ROM) is confirmed by evaluating the v-gap metric with respect to the full order model and by comparison to another ROM obtained by state-of-the-art LPV balanced truncation techniques.
DDC Class
600: Technik
620: Ingenieurwissenschaften
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