Digital repetitive controller design for periodic disturbance attenuation in high performance inverters

Author(s):  
Fanrong Meng ◽  
Xiaoli Duan ◽  
Jiang You ◽  
Yaohua Luo ◽  
Bin Fu
Author(s):  
J-S Yee ◽  
G-H Yang ◽  
J L Wang

This paper is concerned with the design of non-fragile H∞ output feedback control of a high-performance aircraft similar to F-16 in executing a large bank-angle tracking manoeuvre. The non-fragile H∞ flight controllers are designed to tolerate multiplicative gain variations in the controller matrices. The designs are based on three linear trim models of the high-performance aircraft. From the linear and non-linear simulations, the results show that the resulting closed-loop systems using the non-fragile H∞ flight controllers are robustly stable and have H∞ disturbance attenuation bounds with respect to some admissible controller gain variations. Corresponding performance comparisons with the standard robust design approach show that the resulting closed-loop systems using the standard H∞ flight controllers are unstable under the same controller gain variations.


Author(s):  
J. Fulna Kanaga ◽  
◽  
P. Subha Hency Jose ◽  

2011 ◽  
Vol 13 (6) ◽  
pp. 1051-1055 ◽  
Author(s):  
Wentao Chen ◽  
Yechun Lin

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