초록 ▼

A system for use in generating a command trajectory for an aircraft is provided. The system includes a natural frequency determining module configured to determine a closure rate of the aircraft to a selected flight path, compare the closure rate of the aircraft to a threshold closure rate, and calc

A system for use in generating a command trajectory for an aircraft is provided. The system includes a natural frequency determining module configured to determine a closure rate of the aircraft to a selected flight path, compare the closure rate of the aircraft to a threshold closure rate, and calculate a natural frequency based on whether the closure rate is below the threshold closure rate. The system further includes a command processor coupled to the natural frequency determining module and configured to receive the calculated natural frequency from the natural frequency determining module, and generate a command trajectory using the calculated natural frequency.

대표청구항 ▼

1. A system for use in capture of a selected flight path for an aircraft, said system comprising: a frequency determining module configured to: calculate a natural frequency based on a closure rate of the aircraft to the selected flight path; andcalculate an augmented frequency that is greater than

1. A system for use in capture of a selected flight path for an aircraft, said system comprising: a frequency determining module configured to: calculate a natural frequency based on a closure rate of the aircraft to the selected flight path; andcalculate an augmented frequency that is greater than the natural frequency when the closure rate of the aircraft to the selected flight path is below a threshold closure rate; anda command processor coupled to said frequency determining module and configured to: receive the natural frequency;generate a command trajectory to capture the selected flight path in a capture maneuver;receive the augmented frequency; andgenerate an augmented command trajectory to capture the selected flight path in an expedited capture maneuver as compared to the capture maneuver of the command trajectory. 2. A system in accordance with claim 1, wherein to calculate the augmented frequency, said frequency determining module is further configured to set the augmented frequency to a predetermined fixed value when the closure rate is below the threshold closure rate. 3. A system in accordance with claim 1, wherein to calculate the augmented frequency, said frequency determining module is further configured to calculate the augmented frequency as a predetermined multiple of the natural frequency. 4. A system in accordance with claim 1, said system further comprising a vertical position control system coupled to said command processor and configured to control the aircraft, using one of the command trajectory and the augmented command trajectory, such that the aircraft captures the selected flight path. 5. A system in accordance with claim 1, wherein the selected flight path is a glideslope flight path. 6. A system in accordance with claim 5, said system further comprising a vertical position control system coupled to said command processor and configured to control the aircraft, using one of the command trajectory and the augmented command trajectory, such that the aircraft captures the glideslope flight path above a decision height. 7. A processing device for use in capture of a selected flight path for an aircraft, said processing device configured to: calculate a natural frequency based on a closure rate of the aircraft to the selected flight path;calculate an augmented frequency that is greater than the natural frequency when the closure rate of the aircraft to the selected flight path is below a threshold closure rate;supply the natural frequency to a command processor; andsupply the augmented frequency to the command processor, wherein the command processor is configured to generate a command trajectory for capturing the selected flight path. 8. A processing device in accordance with claim 7, wherein the selected flight path is a glideslope flight path. 9. A processing device in accordance with claim 7, wherein to calculate the augmented frequency, said processing device is further configured to set the augmented frequency to a predetermined fixed value when the closure rate is below the threshold closure rate. 10. A processing device in accordance with claim 7, wherein to calculate a natural the augmented frequency, said processing device is further configured to calculate the augmented frequency as a predetermined multiple of the natural frequency. 11. A processing device in accordance with claim 7, wherein to calculate the augmented frequency, said processing device is further configured to calculate the augmented frequency only when the closure rate is below the threshold closure rate and the aircraft is within a predetermined vertical range from the selected flight path. 12. A method for performing a change in the flight path of an aircraft, said method comprising: calculating a natural frequency;calculating an augmented frequency that is greater than the natural frequency;comparing an initial flight path of the aircraft to a selected flight path that is to be captured by the aircraft to determine whether the initial flight path is nearly parallel to the selected flight path; andcapturing the selected flight path using a command trajectory generated using the natural frequency unless the initial flight path is nearly parallel to the selected flight path,wherein the selected flight path is captured using an augmented command trajectory generated using the augmented frequency when the initial flight path is nearly parallel to the selected flight path. 13. A method in accordance with claim 12, wherein comparing an initial flight path to a selected flight path comprises: determining a closure rate of the aircraft to the selected flight path; andcomparing the closure rate of the aircraft to a threshold closure rate. 14. A method in accordance with claim 13, wherein calculating the augmented frequency comprises setting the augmented frequency to a predetermined fixed value. 15. A method in accordance with claim 13, wherein using the command trajectory results in a slower capture of the selected flight path than using the augmented command trajectory. 16. A method in accordance with claim 13, wherein calculating the augmented frequency comprises calculating an augmented frequency that is a predetermined multiple of the natural frequency. 17. A method in accordance with claim 12, wherein comparing an initial flight path of the aircraft to a selected flight path comprises comparing the initial flight path to a glideslope flight path. 18. A method in accordance with claim 17, wherein capturing the selected flight path using an augmented command trajectory comprises capturing the glideslope flight path above a decision height.