Claims
- 1. In a control system for a permanent-magnet motor driven by a multiphase line-commutated inverter, said control system having means for integrating the back EMF of each phase of said motor for use in generating system control signals for said inverter, an improvement comprising
- means for generating a signal proportional to motor speed, and
- adaptive means responsive to said motor speed signal for increasing the attenuation of low frequencies in the back EMF of each phase of said motor by said integrating means as said motor speed increases.
- 2. An improvement as defined in claim 1 wherein said adaptive means is comprised of electronic switches and filter circuits at the input of said integrating means for selectively altering connections of said filter circuits to so alter filter configurations as to shift the corner frequency of said integrating means away from the j.omega. axis thereof as the speed of the motor increases.
- 3. An improvement as defined in claim 2 wherein said filter circuits for each EMF signal are comprised of an operational amplifier with an integrating capacitor for each EMF signal and at least two high-pass filters, a first one permanently connected to couple said EMF signal to said operational amplifier for integration and a second one connected in parallel with said first one by one of said electronic switches.
- 4. In a control system for a permanent-magnet motor driven by a line-commutated inverter, a separate integrator having an adaptive high-pass filter for use in generating system control signals for said inverter from back EMF of said motor, and means for generating a signal proportional to motor speed, and means responsive to said signal for shifting the corner frequency of the high-pass filter of each integrator away from the j.omega. axis as the speed of the motor increases, whereby the attenuation of low-frequency components in said back EMF by the integrators is increased as the motor speed increases to offset the gain of the integrators to spurious low frequencies, thereby assuring a desired minimum power factor at all speeds.
ORIGIN OF INVENTION
The invention described herein was made in the performance of work under a NASA contract and is subject to the provisions of Section 305 of the National Aeronautics and Space Act of 1958, Public Law 85-568 (72 Stat. 435; 42 USC 2457).
US Referenced Citations (5)