This invention relates generally to motor position estimation systems and in particular to motor position estimation systems for permanent magnet synchronous motors.
Permanent magnet synchronous motors (PMSMs) have become increasingly popular in high-performance variable-frequency drives due to their high efficiency, high torque-to-inertia ratio, rapid dynamic response, and relatively simple modeling and control. To achieve the proper field position orientation in motion control applications, it is necessary to obtain the actual position of the rotor magnets. Typically, this position is obtained through the use of position sensors mounted on the motor shaft. These position sensors can include a shaft encoder, resolver, Hall effect sensor, or other form of angle sensor. These sensors typically are expensive, require careful installation and alignment, and are fragile. Accordingly, the the use of these position sensors both in terms actual cost to produce the product and in the costs associated with the maintenance and repair of these systems is high.
Sensorless position estimation systems have been developed to overcome these limitations, but the present sensorless position estimation systems have their own drawbacks as well. These systems typically fall into two categories: back emf methods and signal injection methods. Back emf systems use the measured back emf voltage to estimate the position of the rotor magnets. The back emf voltage signal is roughly proportional to the rotational velocity of the motor. Although this method achieves valid results at higher rotational velocities, at low rotational velocities and high torque settings, the back emf voltage signal decreases to values that are too small to be useful, and vanish entirely at speeds close to a standstill. Thus, the back emf method is not suitable for these low rotational velocity high torque applications. The second method is the signal injection method in which an auxiliary signal is introduced into the motor electrical subsystem and measure the response of the motor electrical subsystem to estimate the rotor position. Although this method avoids the singularities of the back emf method, these methods are computationally intensive and thus are not well suited for industrial applications.
Accordingly, it would be advantageous to provide a position estimation system that avoids the singularities at low speeds and the computationally intensive methods of the prior art.
A method and system for the sensorless estimation of the states of the mechanical subsystem of a motor are disclosed. In particular, the method and system split the estimation problem into two sub-problems: the estimation of motor parameters as a function of position, and the determination of the states of the mechanical subsystem of the motor using the estimated parameters via a state observer. Motor current and PWM voltage in a polyphase system is measured or otherwise determined and converted into current and voltage in α-β coordinates. A least square estimator is constructed that uses the voltage and current in α-β coordinates and provides an estimate of the motor parameters, and in particular, the inductances of the motor, which are a function of the rotor position. These estimated inductances are used to drive a state observer whose dynamics have been selected to provide as an output the state of the mechanical subsystem of the motor, and in particular, the position, velocity, and acceleration of this subsystem.
Other features, functions, and aspects of the invention will be evident from the Detailed Description of the Invention that follows.
The invention will be more fully understood with reference to the following Detailed Description of the Invention in conjunction with the drawings of which:
where yα and yβ are the output in α-β coordinates and x1, x2, and x3 are the 3 polyphase current values. The α-β currents, yαand yβ, are then provided to the least square parameter estimator 110.
The controller 102 also provides the 3-phase PWM control signals to another 3-phase to α-β converter module 112 that converts the 3-phase voltage commands into α-β coordinates using the above transformation in which x1, x2, and x3 are the 3 polyphase voltage signals and yα and yβ are the voltages vα and vβ and are provided to the parameter estimator 110. The parameter estimator 110 uses the transformed current and voltage signals to estimate a set of parameters for the motor 106. These estimated parameters are provided as an input to the mechanical observer 114 that uses the estimated parameters to provide estimates of the position, velocity, and acceleration of the mechanical subsystem of motor 106.
The magnetic field of a motor with salient rotors changes along the circumference. In addition to this non-isotropic behavior due to rotor geometry, in permanent magnetic synchronous motor (PMSMs) additional asymmetry is introduced by the non-uniform magnetic saturation of the stator steel. Due to these phenomena, the fluxes through the stator windings produced by the phase currents are a function of the rotor position that implies a position dependence of the stator phase inductances. The resulting stator inductance matrix in a stationary α-β frame is given by:
The equations describing the electrical subsystem of the motor in the α-β frame are:
where v=[vαvβ]T and i=[iαiβ]T are the vectors of the stator phase voltages and currents, λ=[λαλβ]T and λT=[λταλτβ]T are the vector of stator phase total and partial fluxes, which are due to the rotor field and Rs=diag[Rs, Rs] is the matrix of the stator phase resistances. Combining the above equations yields the following electrical subsystem in the α-β frame:
where
is the effective resistance matrix.
The torque produced by the motor includes reluctance and mutual components and, neglecting torque ripple, is given by:
where P is the number of pole pairs. The mechanical behavior of the motor is modeled with the viscous friction and inertia as:
where J and B are the moment of inertia and the friction constant normalized with respect to P, and τ1 is the load torque.
The position estimation system utilizes the above model and uses the mechanical state variables as parameters in the inductance and resistance matrices. This method uses the electrical transients, which have a much faster time constant than the mechanical transients, to estimate the approximately constant parameters of the system. The electrical subsystem is given by:
where
are the inductance and effective resistance matrices, where
where n=1, 2, . . . N, and N is a number of subintervals within one PWM period. Assuming that the mechanical parameters do not change from one subinterval to another, the back emf term, i.e., the ω term in equation (8) can be removed by subtracting two subsequent subintervals which yields:
At the PWM frequencies that are contemplated for use in this system, the contribution of the R term in equation (9) is negligible, and accordingly the term is neglected. This reduces the problem to be solved to:
where xn is the slope of the current is determined.
To solve the parameter estimation problem, a least squares problem is constructed, but to simplify the process of solving the least squares problem, equation (10) is rewritten such that unknown matrix containing the parameters to be estimated multiplied by the already known voltage values as:
A parameterization to be used in the estimation problem is given by:
Accordingly, equation (11) can be rewritten as:
for n=1,2,3, . . . N−1.
Thus, equation (14) can be written
x=Wq (16)
where W is the matrix of the n−1 voltage differences between adjacent PWM subintervals for the α-β coordinates from equation (11).
Stacking the N−1 equations to form the least squares problem ensures that the system in equation (15) is over-determined, the solution for the estimate of q is given by:
{circumflex over (q)}=(WTW)−1WTx=Wpix (17)
In order to further simplify this problem, a particular PWM pattern is used. As is known, the PWM signal is a three-bit binary signal provided by the controller 102 to the voltage inverter 104 and where a “1” indicates that the corresponding phase is connected to the voltage rail and a “0” indicates that the corresponding phase is connected to ground. As discussed above, the basic unit of time is referred to as a PWM period that is subdivided into N subintervals during which a particular input switch combination is held constant. The duration of each subinterval, referred to as the “duty cycle” can vary, as can the switch combination of each subinterval. In general, the vectors and duty cycles are selected to produce the desired PWM output vector. In the embodiment described herein the PWM pattern has six subintervals and the switching combination is always each of the six non-zero PWM vectors (V1 . . . V6), see
where the duty ratios are defined as
is the duty ratio of the subinterval corresponding to the lag vector, i.e., one of the vectors adjacent to the desired vector, ζ2 is the duty ratio of the subinterval corresponding to the lead vector, i.e., the other one of the vectors adjacent to the desired vector, and ζ3,4,5,6 correspond to the other vectors.
This choice of PWM pattern that is consistent in the order in which the PWM vectors are processed and in which the value of each is consistent allows W in equation (17) to be constant over time since the voltage levels in each subinterval are the same. Thus, Wpi can be computed off-line and {circumflex over (q)}, the estimate of the parameters, will be reduced to a multiplication of a constant matrix by a vector that depends on the measured current values and the duration of the subintervals.
Once {circumflex over (q)} has been estimated, in one embodiment the rotor position could be computed using inverse trigonometric functions and solving equation (13) for θ. However, this has at least two disadvantages. First, the inverse trigonometric functions can be computationally intensive to calculate, and second, the parameter estimate is noisy and would not be filtered. Accordingly, to avoid these problems, in the preferred embodiment, a state estimator is provided that will provide an estimate for all the mechanical states of the system. The state estimator provides for filtering of the parameters and is not computationally intensive. The dynamics of the state observer are designed to be much faster than the dynamics of the mechanical loop controller, so that it is neglected during control loop design.
The observer has the following dynamic form:
{circumflex over({dot over (α)})}=γ3ε
{circumflex over({dot over (ω)})}=γ2ε+{circumflex over (α)}
{circumflex over({dot over (θ)})}=γ1ε+{circumflex over (ω)} (19)
where {circumflex over (θ)},{circumflex over (ω)}, and{circumflex over (α)} are the estimates of the position, speed, and acceleration respectively, γI are design parameters and ε is a non-linear observation error that drives the variable estimates to their true value. The non-linear observation error is derived from the inductance parameters as:
={circumflex over (p)}3 cos(2{tilde over (θ)})−{circumflex over (p)}2 sin(2{tilde over (θ)})=L1 sin(2θ) (20)
where {tilde over (θ)}=θ−{circumflex over (θ)}. It can be shown that the error dynamics of the state observer are non-linear with stable equilibria at {tilde over (θ)}=nπ and if linearized around 0 the error dynamics are stable and the values provided by the state observer will be driven toward the correct values. The speed of the response of the state observer is determined by the placement of the poles of the system which are set by the values selected for γi.
The selection of the poles presents a tradeoff between the response time of the state observer and noise filtering since the bandwidth increases for a faster response time but with less filtering and vice-versa. Another consideration of the pole placement is to keep the original state observer system in equation (19) in the neighborhood of {tilde over (θ)}=0 under all operating conditions.
Accordingly, for each update of the estimated parameters, the estimated parameters are provided to the state observer in equation (19). Equation (19) is then solved and provides an estimate vector of the position, speed, and acceleration of the mechanical subsystem of the motor for the previous PWM subinterval.
It should be appreciated that other variations to and modifications of the above-described sensorless position estimation system may be made without departing from the inventive concepts described herein. Accordingly, the invention should not be viewed as limited except by the scope and spirit of the appended claims.
This application claims the priority of U.S. Provisional Patent Application No. 60/366,047 filed, Mar. 20, 2002 entitled SALIENCY-BASED POSITION ESTIMATION IN PM SYNCHRONOUS MOTORS, the whole of which is hereby incorporated by reference herein.
Part of the work leading to this invention was carried out with United States Government support provided under a grant from the Office of Naval Research, Grant No. N00014-97-1-0704 and under a grant from the National Science Foundation, Grant No. EC9502636 Therefore, the. U.S. Government has certain rights in this invention.
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