DocumentCode
1595098
Title
Improved Algorithm Simulation of Adaptive Blade Pitch Control for Electrically Controlled Rotor
Author
Dong Weisheng ; Lu Yang
Author_Institution
Nat. Key Lab. of Rotorcraft Aeromechanics, Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
fYear
2012
Firstpage
691
Lastpage
695
Abstract
Based on the former adaptive blade pitch control method of the Electrically Controlled Rotor in time domain, two improved control algorithms are proposed. One method is through adding a weight-constrained function for active control filter, which can prevent the divergent of control system caused by interference signal of error channel. The other method is through adding a desired signal of scaling factor to replace the identification process of the forward path. The algorithm can enhance the real time characteristics and the response characteristics of control system. In addition, the comparison between two improved methods and the former method is conducted, and the simulation analysis is made based on the matlab/simulink. The simulation results show that the two proposed methods have better system robustness, and the control characteristics are obviously superior to the former system.
Keywords
active filters; adaptive control; blades; helicopters; rotors; Matlab/Simulink; active control filter; adaptive blade pitch control method; electrically controlled rotor; helicopter; improved algorithm simulation; interference signal; simulation analysis; weight-constrained function; Adaptation models; Blades; Control systems; Helicopters; Noise; Rotors; Simulation; Adaptive Control; Blade Pitch Control; Electrically Controlled Rotor; Simulation;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent System Design and Engineering Application (ISDEA), 2012 Second International Conference on
Conference_Location
Sanya, Hainan
Print_ISBN
978-1-4577-2120-5
Type
conf
DOI
10.1109/ISdea.2012.594
Filename
6173300
Link To Document