Application of Single- and Multi-Objective Evolutionary Algorithms for Optimal Nonlinear Controller Design in Boiler–Turbine System

2017 ◽  
Vol 20 (3) ◽  
pp. 803-816 ◽  
Author(s):  
T. Piraisoodi ◽  
M. Willjuice Iruthayarajan ◽  
K. Mohaideen Abdul Kadhar
2017 ◽  
Vol 64 (4) ◽  
pp. 451-462 ◽  
Author(s):  
T. Piraisoodi ◽  
M. Willjuice Iruthayarajan ◽  
K. Mohaideen Abdul Kadhar

2020 ◽  
Vol 67 (4) ◽  
pp. 1500-1520
Author(s):  
Jose Luis Redondo Gutiérrez ◽  
Ansgar Heidecker

AbstractThis paper combines the nonlinear Udwadia-Kalaba control approach with the Assumed Mode Method to model flexible structures and derives an attitude controller for a spacecraft. The study case of this paper is a satellite with four flexible cantilever beams attached to a rigid central hub. Two main topics are covered in this paper. The first one is the formulation of the equation of motion and the second one is the nonlinear controller design. The combination of these two techniques is able to provide a controller that damps the vibration of a flexible structure while achieving the desired rigid-motion state.


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