DocumentCode :
313109
Title :
Optimal control of a magnetic bearing without bias flux
Author :
Yang, C. ; Knospe, C.
Author_Institution :
Dept. of Mech., Aerosp. & Nucl. Eng., Virginia Univ., Charlottesville, VA, USA
Volume :
3
fYear :
1997
fDate :
4-6 Jun 1997
Firstpage :
1534
Abstract :
Conventional active magnetic bearings are operated using a bias current (or flux) to achieve greater linearity and dynamic capability. Bias results in undesirable rotating losses and consequent rotor heating. In this paper, optimal control of a magnetic bearing without bias is investigated. A single degree-of-freedom system consisting of a mass and two opposing electromagnets is considered. The optimal control problem is examined for a cost function that penalizes both poor regulation and rotational energy lost. Although a standard optimization procedure does not directly yield an analytical solution, it does show that the optimal control is always bang-bang with possibly a singular arc. First, the minimum time problem is solved for a simple switching law in three dimensional state space. A non-standard, physics-based approach is then employed to obtain an optimal solution for the general problem. The final result is an optimal variable structure feedback controller
Keywords :
bang-bang control; electromagnets; feedback; machine bearings; magnetic levitation; nonlinear control systems; optimal control; rotors; state-space methods; variable structure systems; active magnetic bearings; bang-bang; bias current; electromagnets; feedback; optimal control; rotor heating; state space; variable structure control; Cost function; Equations; Magnetic flux; Magnetic levitation; Optimal control; Power system modeling; Proportional control; Strain control; Velocity control; Voltage control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1997. Proceedings of the 1997
Conference_Location :
Albuquerque, NM
ISSN :
0743-1619
Print_ISBN :
0-7803-3832-4
Type :
conf
DOI :
10.1109/ACC.1997.610800
Filename :
610800
Link To Document :
بازگشت