DocumentCode :
231742
Title :
Polytopic LPV system based control design for multi-propeller airship
Author :
Chen, Luo-nan ; Duan, D.P.
Author_Institution :
Inst. of Aerosp. Sci. & Technol., Shanghai Jiao Tong Univ., Shanghai, China
fYear :
2014
fDate :
28-30 July 2014
Firstpage :
4273
Lastpage :
4276
Abstract :
An airship with multi-propeller was proposed in this paper, the nonlinear dynamic model was established and the longitudinal model is transformed into a LPV form by Jacobian linearization method. The discreted LPV system within the interzone of the changing parameters is storied into a tensor, and then HOSVD is used to obtain a finite number of LTI vertex systems, then the robust state-feedback controller was designed in vertex system using linear matrix inequalities(LMIs) approach, and a robust variable gain controller is synthesized via convex decomposition techniques. The velocity tracking of time-varying references based on nonlinear model was carried out with the designed controller; simulation results illustrate the validity of the designed controller.
Keywords :
airships; control system synthesis; discrete systems; gain control; linear matrix inequalities; nonlinear dynamical systems; number theory; robust control; singular value decomposition; state feedback; tensors; time-varying systems; HOSVD; Jacobian linearization method; LMI; LTI vertex systems; convex decomposition techniques; discreted system; finite number; linear matrix inequalities approach; longitudinal model; multipropeller airship; nonlinear dynamic model; polytopic LPV system based control design; robust state-feedback controller; tensor; time-varying references; variable gain controller; velocity tracking; Aerodynamics; Atmospheric modeling; Buoyancy; Gravity; Mathematical model; Robustness; H State feedback; HOSVD; Multi-propeller airship; Polytopic LPV System; Vectored thrust;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2014 33rd Chinese
Conference_Location :
Nanjing
Type :
conf
DOI :
10.1109/ChiCC.2014.6895655
Filename :
6895655
Link To Document :
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