Electricity: motive power systems – Switched reluctance motor commutation control
Reexamination Certificate
2001-08-17
2003-10-28
Nappi, Robert E. (Department: 2837)
Electricity: motive power systems
Switched reluctance motor commutation control
C318S430000, C318S434000, C318S132000, C290S04000F, C290S051000
Reexamination Certificate
active
06639371
ABSTRACT:
BACKGROUND OF THE INVENTION
The present invention is generally related to control of electromechanical machines, and, more particularly, the present invention is related to method and system for controlling a permanent magnet (PM) machine without using high resolution absolute rotor position information.
In the starting and control of permanent magnet machines using sinusoidal current control, the absolute position of the rotor of the machine is generally required to appropriately position the stator's current vector relative to the rotor's magnet flux vector in order for the machine to develop a desired level of torque.
It is known that various techniques have been proposed to determine absolute rotor position. Some of the proposed techniques require the use of resolver devices. Although resolver devices can accurately determine the absolute position of the rotor, such devices generally require tight positional tolerances and associated driving circuitry, and thus their relatively high cost incrementally adds to the overall cost of a propulsion system that uses permanent magnet machines.
Other techniques have attempted to determine the absolute position of the rotor without the use of sensors. Unfortunately, sensorless techniques may require computationally intensive algorithms and may not be suitable to applications, such as those using flywheel alternator starter systems, where a relatively high initial torque is desired so that, for example, an internal combustion engine coupled to the starter system can be started as quickly as possible under extreme environmental conditions.
Unfortunately, absolute position sensors based on standard position-pulse techniques have limitations since such sensors may not be effectively utilized for applications that require high initial starting torque since the absolute position is not determined until a pulse indicative of relative position of the rotor is received by a controller. For example, the rotor position determination may not occur for up to about one mechanical revolution of the rotor, during which the controller would be unable to appropriately position the current vector relative to the flux vector. This condition could lead either to reduced torque generation or even to negative torque generation.
In view of the foregoing issues, it is desirable to provide techniques capable of producing high initial starting torque without having to use a high resolution absolute position sensor. It would be further desirable to use a low-cost and reliable sensing scheme that allows a standard vector controller that normally operates in a sinusoidal alternating current (AC) mode of operation to run during start up of the machine in a brushless direct current (BLDC) mode of operation to take advantage of the relatively higher torque characteristics that are achievable during the BLDC mode of operation. It is also desirable to be able to seamlessly transition from the BLDC mode of operation to the sinusoidal mode of operation once the startup of the machine is achieved. As will be readily understood by those skilled in the art, the use of the expression brushless direct current mode of operation is a bit of a misnomer since the mode is not truly a DC mode, if by DC one means a mode whose machine voltages and currents are unidirectional for a given condition of speed and torque. In fact, the voltages and currents of the machine generally vary trapezoidally in the BLDC mode of operation, however, the expression BLDC as used herein is consistent with traditional and well-understood usage in the field of electrical motors. For readers desiring further background regarding the operation of brushless DC motors, see 4
th
Ed. of textbook titled “Electric motors” by Cyril G. Veinott and Joseph E. Martin at pp. 261-263, published by McGraw-Hill Book Company.
BRIEF SUMMARY OF THE INVENTION
Generally, the present invention fulfills the foregoing needs by providing in one aspect thereof a method for controlling a permanent magnet machine. The method provides a sensor assembly for sensing rotor sector position relative to a plurality of angular sectors. The method further provides a sensor for sensing angular increments in rotor position. The method allows starting the machine in a brushless direct current mode of operation using a calculated initial rotor position based on an initial angular sector position information from the sensor assembly. Upon determining a transition from the initial angular sector to the next angular sector, the method allows switching to a sinusoidal mode of operation using rotor position information from the incremental sensor.
The present invention further fulfills the foregoing needs by providing in another aspect thereof, a system for controlling a permanent magnet machine. The system includes a sensor assembly for sensing rotor sector position relative to a plurality of angular sectors. The system further includes a sensor for sensing angular increments in rotor position. A module is configured to calculate initial rotor position based on an initial angular sector position information from the sensor assembly, wherein the initial rotor position is used for starting the machine in a brushless direct current mode of operation. A sector-transition module is configured to determine transitions between any two adjacent angular sectors as the rotor of the machine rotates. A switching module is responsive to a switching signal from the sector-transition module to pass rotor position information based on the incremental sensor, the rotor position information being used to provide a sinusoidal mode of operation, in lieu of the brushless direct current mode of operation, upon the sector-transition module determining a transition from the initial angular sector to the next angular sector.
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Krefta Ronald John
Walters James E.
Dobrowitsky Margaret A.
Martin Edgardo San
Nappi Robert E.
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