초록 ▼

The present invention provides a diagnostics methodology and embedded electronic system that allows optimized low-frequency data sampling for EMA motoring subsystems in an operating vehicle. Each of the EMA motoring subsystems includes: an EMA; at least one motor for driving the EMA; and power contr

The present invention provides a diagnostics methodology and embedded electronic system that allows optimized low-frequency data sampling for EMA motoring subsystems in an operating vehicle. Each of the EMA motoring subsystems includes: an EMA; at least one motor for driving the EMA; and power controls for operating the motor, wherein the power controls includes a DSP controller for sampling and processing data at low-frequency sampling rates. The diagnostic methodology includes a method that has the steps of: determining an operational mode of the EMA motoring subsystem; selecting a sampling rate optimized for the determined operational mode; acquiring and processing data at the selected sampling rate; and analyzing the processed data to identify and classify a fault of the EMA motoring subsystem.

대표청구항 ▼

We claim: 1. A method for identifying a pseudo-steady-state operating condition of an EMA motoring subsystem in a system, comprising: determining a mission phase of a system; assessing at least one key state variable of an EMA motoring subsystem in the system; and identifying a pseudo-steady-state

We claim: 1. A method for identifying a pseudo-steady-state operating condition of an EMA motoring subsystem in a system, comprising: determining a mission phase of a system; assessing at least one key state variable of an EMA motoring subsystem in the system; and identifying a pseudo-steady-state operating condition of the EMA motoring subsystem based on the determined mission phase combined with the assessed at least one key state variable. 2. The method of claim 1, wherein the determined mission phase is on-ground, take-off, cruise or landing phase. 3. The method of claim 1, wherein the assessed at least one key state variable is position of a ball screw ram, motor position, motor phase current, motor input current, motor bridge current, motor pulse-width-modulation amplitude, motor supply voltage or actuator position. 4. The method of claim 1, wherein the identified pseudo-steady-state operating condition is on-ground, take-off, cruise or landing condition. 5. A method for identifying a pseudo-steady-state operating condition of an electro-mechanical/electro-hydrostatic actuator (EMA) motoring subsystem in a system, comprising: assessing at least one key state variable of an EMA motoring subsystem in the system to determine if the system is in a pseudo-small signal mode; and performing a diagnostics task at an optimized low-frequency sampling rate when the system is in said pseudo-small signal mode. 6. The method of claim 5, further comprising: determining a mission phase of the system; and selecting said optimized low-frequency sampling rate based on said determined mission phase. 7. The method of claim 5, further comprising selecting an optimum sampling rate when the system is in a large signal mode. 8. The method of claim 5, wherein: said diagnostics task comprises acquiring multi-channel data at said optimized low-frequency sampling rate. 9. The method of claim 5, wherein: said diagnostics task comprises real-time sampling and processing data from the EMA motoring subsystem; and detecting a fault of the EMA motoring subsystem. 10. A method for identifying a pseudo-steady-state operating condition of an electro-mechanical/electro-hydrostatic actuator (EMA) motoring subsystem in a system, comprising: identifying a pseudo-steady-state operating condition of the EMA motoring subsystem based on a selected mission phase combined with at least one assessed key state variable; and selecting an optimal low-frequency sampling rate of data from the EMA motoring subsystem based on said identified pseudo-steady-state operating condition. 11. The method of claim 10, wherein: said optimal low-frequency sampling rate is determined based on the selected mission phase and the at least one assessed key state variable referencing an accessment data profile. 12. The method of claim 10, further comprising: sampling data from the EMA motoring subsystem at said selected optimal low-frequency sampling rate; and exploiting said sampled data to control a vehicle. 13. The method of claim 10, further comprising: sampling data from the EMA motoring subsystem at said selected optimal low-frequency sampling rate; and passing said sampled data to a vehicle management computer that analyzes said data and detects a fault of the EMA motoring subsystem. 14. The method of claim 10, further comprising: sampling data from the EMA motoring subsystem at said selected optimal low-frequency sampling rate; and passing said sampled data to a vehicle management computer connected to a graphical user interface (GUI) for testing the EMA motoring subsystem.