High Performance Controller Design Using Linear Matrix Inequalities for Pitch Angle Regulation of Aircraft

Author(s):  
Mizanur Rahman ◽  
Maniza Armin ◽  
Sajal K. Das ◽  
M. F. Ali
2011 ◽  
Vol 317-319 ◽  
pp. 2204-2207
Author(s):  
Dong Mei Yang ◽  
Qing Sun

This paper is concerned with the non-fragile decentralized controller design problem for uncertain singular large-scale system with time-delay. Sufficient condition for the controller is expressed in terms of linear matrix inequalities(LMIs). When this condition is feasible, the desired controller can be obtained with additive gain perturbations and multiplicative gain perturbations. Finally, a numerical example is also given to illustrate the effectiveness.


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