DocumentCode
1597697
Title
A predictive multivariable helicopter robust design
Author
Aslan, Y. ; Beauvois, D. ; Rossiter, J.A.
Author_Institution
Ecole Superieure d´´Electricite, Gif sur Yvette, France
fYear
1992
Firstpage
812
Abstract
The characteristic decomposition methodology and its use for the multivariable characteristic GPC (CGPC) are reviewed. The approach is illustrated via a helicopter application. The characteristic decomposition results and the simulations obtained by the MIMO CGPC are given. These simulations show that the initial feedback configuration has to be slightly modified to ensure the required performance/robustness. With good eigenstructure approximations, the CGPC design offers important advantages: (i) by means of eigen projection, it decouples and simplifies the prediction equations; (ii) by the ease of use of independent prediction parameters for each subsystem, it makes it possible to shape the individual subsystems behavior and, hence, the behavior of the overall system according to the necessary and sufficient generalized Nyquist condition; and (iii) the appropriate use of a matrix polynomial filter makes it possible to achieve the desired robustness
Keywords
aircraft control; control system synthesis; helicopters; multivariable control systems; predictive control; stability; aircraft control; characteristic decomposition; eigenstructure approximations; feedback; generalised predictive control; generalized Nyquist condition; helicopter; matrix polynomial filter; multivariable characteristic GPC; robustness; stability; Cost function; Eigenvalues and eigenfunctions; Error correction; Helicopters; MIMO; Matrix decomposition; Polynomials; Predictive control; Robustness; Transfer functions;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Applications, 1992., First IEEE Conference on
Conference_Location
Dayton, OH
Print_ISBN
0-7803-0047-5
Type
conf
DOI
10.1109/CCA.1992.269743
Filename
269743
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