초록 ▼

A control stick system for simulating a detent mechanism in an aircraft is provided. The detent mechanism is simulated by a motor operably coupled to a lever and configured to bias the lever such that the user experiences the feel of a traditional detent mechanism. A controller operates the motor th

A control stick system for simulating a detent mechanism in an aircraft is provided. The detent mechanism is simulated by a motor operably coupled to a lever and configured to bias the lever such that the user experiences the feel of a traditional detent mechanism. A controller operates the motor that provides the simulated detent by receiving data from multiple sensors regarding the position and the speed of the lever and the position and the speed of a rotor assembly of the motor. Using the position and the speed measurements, the controller is able to detect when the lever is entering a specific zone of a simulated detent range. Depending on what zone the lever is in, within the simulated detent range, the controller is configured to provide a different drive current to the motor.

대표청구항 ▼

1. A control stick system for an aircraft comprising: a lever;a motor operably coupled to the lever and configured to operably bias the lever; anda controller operably controlling the motor such that the motor biases the lever in such a manner to simulate a detent mechanism, based on a position meas

1. A control stick system for an aircraft comprising: a lever;a motor operably coupled to the lever and configured to operably bias the lever; anda controller operably controlling the motor such that the motor biases the lever in such a manner to simulate a detent mechanism, based on a position measurement and a speed measurement from the motor and a position measurement and a speed measurement from the lever. 2. The control stick system of claim 1, wherein the position and speed measurement from the motor is provided by a resolver configured to monitor a rotor of the motor. 3. The control stick system of claim 1, wherein the position and speed measurement from the lever is provided by a resolver. 4. The control stick system of claim 3, wherein the position and speed measurement from the lever is provided by a second resolver. 5. The control stick system of claim 1, wherein the controller regulates a current supplied to the motor. 6. The control stick system of claim 5, wherein the current supplied to the motor changes based on the position measurement and the speed measurement from the motor and the position measurement and the speed measurement from the lever in order to create a simulated detent. 7. The control stick system of claim 6, wherein the simulated detent defines zones of operation for the motor. 8. The control stick system of claim 1, further comprising a slip clutch configured between the lever and the motor. 9. The control stick system of claim 8, further comprising a reversible gear train configured between the slip clutch and the motor. 10. The control stick system of claim 1, wherein the motor is a brushless DC motor. 11. The control stick system of claim 10, wherein the controller operably controls the motor by setting a drive current for the motor. 12. The control stick system of claim 11, wherein the controller comprises a first proportional/integrator loop for tracking the position of the control stick, a second proportional/integrator loop for tracking the speed of the control stick, and a third proportional integrator loop for setting the drive current for the motor. 13. A method of simulating a detent mechanism comprising: sensing a position and speed of a lever;sensing a position and speed of a motor operably coupled to the lever and configured to operably bias the lever; andcontrolling the motor such that the motor biases the lever in such a manner to simulate a detent mechanism, based on the position and speed of the motor and the position and speed of the lever. 14. The method of claim 13, wherein sensing the position and speed of the lever is done by a resolver. 15. The method of claim 14, wherein sensing the position and speed of the lever is done by a second resolver. 16. The method of claim 13, wherein sensing the position and speed of the motor is done by a resolver. 17. The method of claim 13, wherein the motor is a brushless DC motor powered by a drive current. 18. The method system of claim 17, wherein the drive current supplied to the motor changes based on the position and speed of the motor and the position and speed of the lever in order to create a simulated detent. 19. The method of claim 18, wherein controlling the motor comprises setting the drive current for the motor by providing a position of a simulated detent and the position of the control stick to a first proportional/integrator loop to track a position of the control stick relative to the simulated detent position to obtain a relative position of the control stick, providing the relative position of the control stick and the speed of the control stick to a second proportional/integrator loop to track the speed of the control stick relative to the control sticks position within the simulated detent to obtain a relative speed of the control stick, and providing the relative speed of the control stick and a saturation limit to a third proportional/integrator loop to determine the drive current. 20. A control stick system for an aircraft comprising: a lever;a slip clutch operably coupled to the lever;a reversible gear train operably coupled to the slip clutch;a motor operably coupled to the reversible gear train and configured to operably bias the lever by providing a torque to the reversible gear train;a first resolver configured to measure a speed and a position of the lever;a second resolver configured to measure a speed and a position of the motor; anda controller operably controlling the motor such that the motor biases the lever in such a manner to simulate a detent mechanism, based on measurements from the first resolver and the second resolver.