Title : ( Design Controller H∞H2, LQG and predictive and for a jet transport aircraft )
Authors: Amir Torabi , seyed kamaleddin mousavi mashhadi , Ali Karsaz ,
Full TextAbstract
he objective of this paper is to compare the time specification performance among four state feedback tracking controller design methods and determine which control method delivers better performance for linear MIMO systems. The four controller design methods are Pole Placement method, Linear Quadratic Regulator (LQR), an Eigenvalue Assignment method for shaping the output response and a method based on Moore‟s Eigenstructure Assignment for controlling the linearized model of MIMO systems.. LQR assures stability robustness with full state feedback but does not provide the flexibility of assigning eigenvalues and eigenvectors in placing closed loop structure.
Keywords
, LQR, missile, H∞controller, predictive controller
@article{paperid:1105486,
author = {امیر ترابی and سید کمال الدین موسوی مشهدی and Ali Karsaz, },
title = {Design Controller H∞H2, LQG and predictive and for a jet transport aircraft},
journal = {Technical Journal of Engineering and Applied Sciences},
year = {2013},
volume = {3},
number = {21},
month = {June},
issn = {2051-0853},
pages = {1--10},
numpages = {9},
keywords = {LQR;missile; H∞controller; predictive controller},
}
%0 Journal Article
%T Design Controller H∞H2, LQG and predictive and for a jet transport aircraft
%A امیر ترابی
%A سید کمال الدین موسوی مشهدی
%A Ali Karsaz,
%J Technical Journal of Engineering and Applied Sciences
%@ 2051-0853
%D 2013
