DocumentCode :
1657162
Title :
A MIMO backstepping control with acceleration feedback for torpedo
Author :
Vuilmet, Cyrille
Author_Institution :
Departement ING, DCN Armes sous-marines, Saint-Tropez
fYear :
2006
Firstpage :
157
Lastpage :
162
Abstract :
In this paper we are interested in the MIMO backstepping control technique with acceleration feedback in order to track a trajectory generated by a way-point guidance system. The control objective is to reach the desired waypoints, with a desired surge. Here, the surge controller is designed with an integrator backstepping control that takes the propeller model and the motor model into account. In order to generate a realistic trajectory between two consecutive waypoints, the guidance system takes into consideration the torpedo´s dynamics and kinematics. The numerical simulations in the presence of marine current and of torpedo´s parameters uncertainties show the robustness of the MIMO backstepping control loop associated with the acceleration feedback loop. In the same time, the generation of a realist trajectory, generated from the torpedo´s hydrodynamic model, assures a feasible trajectory tracking. The implementation of a MIMO backstepping control with acceleration feedback, and of an integrator backstepping control in a heavyweight torpedo of type F17 mod2, designed by DCN Armes sous-marines, is the main contribution of this work
Keywords :
MIMO systems; control system synthesis; feedback; military systems; missile guidance; position control; MIMO backstepping control technique; acceleration feedback; hydrodynamic model; integrator backstepping control; surge controller; torpedo; way-point guidance system; Acceleration; Backstepping; Control systems; Feedback; Kinematics; MIMO; Numerical simulation; Propellers; Surges; Trajectory;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
System Theory, 2006. SSST '06. Proceeding of the Thirty-Eighth Southeastern Symposium on
Conference_Location :
Cookeville, TN
Print_ISBN :
0-7803-9457-7
Type :
conf
DOI :
10.1109/SSST.2006.1619111
Filename :
1619111
Link To Document :
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