Various techniques employed in detecting the position of a movable element in an electrically commutated machine have been satisfactory in general but not completely without problems. More specifically, while the invention finds applicability in linear motors and other types of motors, for example where the movable element may follow a reciprocal parti-circular path, it is particularly well suited to brushless direct current (BLDC) motors. In the past, rotor position in BLDC motors has been detected using devices such as Hall sensors or encoders. If the rotor position is calculated using various motor quantities such as voltage and current, the detection scheme is called “sensorless.” Since the use of sensors adds to the cost of the device, the sensorless method is typically a more desirable implementation. Current sensorless methods utilize a six-step drive which activates two of the three legs of an inverter at any given time while the non-active leg is utilized in calculation of the rotor position. When using drive schemes such as sine wave drive, all legs of the inverter are active during the time the motor is driven. Information relevant to attempts to address these problems can be found in U.S. Pat. No. 6,252,362 B1. However, this reference suffers from the disadvantage of having discontinuities introduced into the drive waveform timed to coincide with back electromagnetic force(BEMF) zero crossings.
It is the general object of the present invention to provide an improved method of detecting the position of the movable element of an electrically commutated machine where the position can be detected with an arbitrary waveform applied to drive the machine without the introduction of discontinuities into the drive waveform.
In fulfillment of the aforementioned objects and in accordance with the present invention, the method of the invention comprises the steps of determining the applied voltage, current, resistance, and inductance of at least one phase and then calculating the position of the movable element from the applied voltage, current, resistance and inductance.
The values of the applied voltage, current, resistance, and inductance of each phase can be determined using several different methods. The applied voltage of a phase can be measured directly or inferred with the knowledge of the supplied bus voltage and the percentage of the duty cycle of the pulse width modulation (PWM) waveform applied to the phase. Similarly, the current in a phase can be determined by direct measurement or inferred by measuring the voltage across the phase and calculating the current in the phase with knowledge of the resistance of the phase. The inductance and resistance are quantities that are determined during the development and manufacture of the machine. The resistances of the phases of the machine remain substantially constant. The inductances of the phases of the machine are assumed to remain substantially constant. For brushless direct current (BLDC) motors and similar machines this is a valid assumption since the air gap between the rotor and the stator is fairly constant. In BLDC motors, the star point voltage can be measured directly or calculated using the applied voltage, the phase resistance, and phase inductance.
The motor model, 11, as shown in
Where va, is the voltage applied on the terminal of the motor ra is the resistance, La is the inductance, vemfa is the back electromagnetic force (BEMF), ia is the current. All these quantities refer to phase A of the motor. Quantities with b and c subscript refer to phases B and C of the motor respectively. vn is the star point voltage of the motor. Note that in the above equations, it is assumed that the inductance is substantially constant as a function of the rotor position. For BLDC, this is a valid assumption since the air gap between the rotor and the stator is fairly constant. In BLDC based drives, the applied voltage, the phase resistance and inductance are known, and the star point voltage vn can be calculated via these known quantities or measured directly. The above equations can be solved to compute the BEMF. The zero crossing of the BEMF will provide Hall like signals estimating the rotor position in 60 Degree resolutions. In contrast, if the complete BEMF waveform is utilized, the rotor position can be estimated similar to an encoder or a resolver sensor.
The equations can be implemented in analog or digital circuitry. Whether to implement in analog or digital, is a system level decision based upon cost and performance optimization. The preferred embodiment of the present invention is implemented using the following steps. Note these steps have to be repeated for all phases.
The preferred embodiment is an analog implementation to provide sensor-less sine wave drive. In this implementation, special consideration is given to the filtering process. Filters not only eliminate switching noise, but must also have a constant group delay. This ensures that the wave shape of the measured quantities are preserved as they are filtered. These filters are easily implemented via conventional operational amplifiers. In
In Block2 of
The measured phase current IA 42 is then fed to Block366 of
PA_Zerox 72 along with PB_Zerox and PC_Zerox are fed to the microprocessor where they are used to generate Sine Wave Drive. Note the microprocessor compensates for the time lag introduced by the Bessel Filter in the calculation of the BEMF waveforms. Additionally, it can advance or retard the sine wave based on these zero crossing to improve the efficiency of the motor drive.
The method of the invention can be implemented using digital components as shown in
Provisional application No. 60/508,412, titled “Sensorless Sinewave Drive” filed Oct. 2, 2003, inventors Haroon I. Yunus, Russel H. Marvin, Bumsuk Won, incorporated herein by reference.
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Number | Date | Country | |
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60508412 | Oct 2003 | US |