Automated procedure for gain scheduled flight control law design

Author(s):  
M. Oosterom ◽  
G. Schram ◽  
R. Babuska ◽  
H. Verbruggen
Author(s):  
Laleh Ravanbod ◽  
Dominikus Noll

We present a new method to compute output gain-scheduled controllers for nonlinear systems. We use structured H∞-control to precompute an optimal controller parametrization as a reference. We then propose three practical methods to implement a control law which has only an acceptable loss of performance with regard to the optimal reference law. Our method is demonstrated in longitudinal flight control, where the dynamics of the aircraft depend on the operational conditions velocity and altitude. We design a structured controller consisting of a PI-block to control vertical acceleration, and another I-block to control the pitch rate.


2000 ◽  
Vol 48 (561) ◽  
pp. 322-328 ◽  
Author(s):  
Yasuhiro YAMAGUCHI ◽  
Masahiro OHNO ◽  
Takashi HATA ◽  
Atsumi OHARA ◽  
Masakazu IDE

1999 ◽  
Vol 3 (3) ◽  
pp. 111-113
Author(s):  
Georg Grübel ◽  
Jean-François Magni

2006 ◽  
Vol 12 (11) ◽  
pp. 1130-1137 ◽  
Author(s):  
Chong-Sup Kim ◽  
In-Je Cho ◽  
Jong-Min Ahn ◽  
Ji-Hwan Shin ◽  
Sang-Seon Park

Sign in / Sign up

Export Citation Format

Share Document