초록
A method for managing a premature descent envelope during descent of an aircraft is provided. The method receives glideslope deviation data by an instrument landing system (ILS) onboard the aircraft; compares, by the ILS, the glideslope deviation data to an acceptable band of glideslope deviation values; and when the glideslope deviation data is within the acceptable band, expands, by a terrain awareness and warning system (TAWS), the premature descent envelope to produce an increased premature descent envelope for the aircraft.
A method for managing a premature descent envelope during descent of an aircraft is provided. The method receives glideslope deviation data by an instrument landing system (ILS) onboard the aircraft; compares, by the ILS, the glideslope deviation data to an acceptable band of glideslope deviation values; and when the glideslope deviation data is within the acceptable band, expands, by a terrain awareness and warning system (TAWS), the premature descent envelope to produce an increased premature descent envelope for the aircraft.
대표
청구항
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1. A method for managing a premature descent envelope during descent of an aircraft, the method comprising: receiving glideslope deviation data by an instrument landing system (ILS) onboard the aircraft;comparing, by the ILS, the glideslope deviation data to an acceptable band of glideslope deviation values; andwhen the glideslope deviation data is within the acceptable band, determining that the aircraft is flying according to horizontal guidance and vertical guidance provided by the ILS; andaccommodating a potentially false glideslope signal, by: expan...
1. A method for managing a premature descent envelope during descent of an aircraft, the method comprising: receiving glideslope deviation data by an instrument landing system (ILS) onboard the aircraft;comparing, by the ILS, the glideslope deviation data to an acceptable band of glideslope deviation values; andwhen the glideslope deviation data is within the acceptable band, determining that the aircraft is flying according to horizontal guidance and vertical guidance provided by the ILS; andaccommodating a potentially false glideslope signal, by: expanding, by a terrain awareness and warning system (TAWS), the premature descent envelope to produce an increased premature descent envelope for the aircraft,wherein the premature descent envelope comprises a set of minimum clearance altitudes for the aircraft at particular distances from the runway, wherein the increased premature descent envelope comprises a second set of increased minimum clearance altitudes at the particular distances from the runway, and wherein the increased minimum clearance altitudes comprise higher altitude values than the minimum clearance altitudes; andwhen the aircraft flies below one of the increased minimum clearance values, generating an alert. 2. The method of claim 1, further comprising: receiving localizer deviation data by the ILS;comparing, by the ILS, the localizer deviation data to a second acceptable band of localizer deviation values; andwherein the increased premature descent envelope is produced by the TAWS when the glideslope deviation data is within the acceptable band and the localizer deviation data is within the second acceptable band. 3. The method of claim 2, further comprising: when the localizer deviation data is outside of the second acceptable band and the glideslope deviation data is outside of the acceptable band, determining, by the ILS, that the aircraft is not flying according to horizontal guidance provided by a localizer signal and vertical guidance provided by a glideslope signal; andmaintaining, by the TAWS, the premature descent envelope. 4. The method of claim 1, further comprising: when the glideslope deviation data is within the acceptable band, determining, by the ILS, that the aircraft is flying according to vertical guidance provided by a glideslope signal;wherein the increased premature descent envelope is produced by the TAWS to decrease allowable deviation from a defined glide path without producing an alert. 5. The method of claim 4, further comprising: when the glideslope deviation data is outside of the acceptable band, determining, by the ILS, that the aircraft is not flying according to the vertical guidance provided by the glideslope signal; andmaintaining, by the TAWS, the premature descent envelope. 6. The method of claim 1, further comprising: determining, by the ILS, whether the aircraft is flying below increased altitude values defined by the increased premature descent envelope; andwhen the aircraft is flying below the increased altitude values, generating an alert. 7. A system for managing a premature descent envelope during descent of an aircraft, the system comprising: a glideslope system, configured to detect a glideslope deviation of the aircraft from a designated glide path onto the approaching runway;system memory; andat least one processor, communicatively coupled to the system memory, the at least one processor configured to: compare the glideslope deviation to acceptable glideslope deviation values;determine that the aircraft is flying according to horizontal guidance and vertical guidance provided by the ILS, andaccommodate a potentially false glideslope signal, by: when the glideslope deviation is within predefined glideslope deviation values, increasing altitude values of the premature descent envelope:wherein the premature descent envelope comprises a set of minimum clearance altitudes for the aircraft at particular distances from the runway, wherein the increased premature descent envelope comprises a second set of increased minimum clearance altitudes at the particular distances from the runway, and wherein the increased minimum clearance altitudes comprise higher altitude values than the minimum clearance altitudes; andwhen the aircraft flies below one of the increased minimum clearance values, generating an alert. 8. The system of claim 7, further comprising: a localizer system, configured to detect a localizer deviation of the aircraft from a centerline of an approaching runway;wherein the at least one processor is further configured to increase the altitude values of the premature descent envelope when: the localizer deviation is within predefined localizer deviation values; andthe glideslope deviation is within predefined glideslope deviation values. 9. The system of claim 8, wherein the localizer deviation is within the predefined localizer deviation values when the localizer deviation is less than 0.2 dots. 10. The system of claim 8, wherein, when the localizer deviation is not within predefined localizer deviation values, the at least one processor is further configured to: determine that the aircraft is not being flown to minimize the localizer deviation and the glideslope deviation; andmaintain the premature descent envelope. 11. The system of claim 7, wherein, when the glideslope deviation is within predefined glideslope deviation values, the at least one processor is further configured to: determine that the aircraft is being flown to minimize the glideslope deviation;wherein the altitude values of the premature descent envelope are increased to decrease allowable deviation from the designated glide path without producing an alert. 12. The system of claim 7, wherein, when the glideslope deviation is not within predefined glideslope deviation values, the at least one processor is further configured to: determine that the aircraft is not being flown to minimize glideslope deviation; andmaintain the premature descent envelope. 13. The system of claim 7, wherein the glideslope deviation is within the predefined glideslope deviation values when the glideslope deviation is less than 0.2 dots. 14. The system of claim 7, wherein, after increasing altitude values of the premature descent envelope, the at least one processor is further configured to: determine whether the aircraft is flying below the increased altitude values; andwhen the aircraft is flying below the increased altitude values, generate an alert. 15. A non-transitory, computer-readable medium containing instructions thereon, which, when executed by a processor, perform a method comprising: determining whether an aircraft is adhering to vertical guidance provided by a detected glideslope signal during descent; andwhen the aircraft is adhering to the vertical guidance, determining that the aircraft is flying according to horizontal guidance and vertical guidance provided by the ILS; andaccommodating a potentially false glideslope signal, by: expanding a premature descent envelope for the aircraft:wherein the premature descent envelope comprises a set of minimum clearance altitudes for the aircraft at particular distances from the runway, wherein the increased premature descent envelope comprises a second set of increased minimum clearance altitudes at the particular distances from the runway, and wherein the increased minimum clearance altitudes comprise higher altitude values than the minimum clearance altitudes; andwhen the aircraft flies below one of the increased minimum clearance values, generating an alert. 16. The non-transitory, computer-readable medium of claim 15, wherein the method further comprises: determining a glideslope deviation, based on the detected glideslope signal and current operation of the aircraft;comparing the glideslope deviation to a predefined set of acceptable glideslope deviation values; andwhen the glideslope deviation is in the predefined set, determining that the aircraft is adhering to the vertical guidance. 17. The non-transitory, computer-readable medium of claim 15, wherein the method further comprises: determining whether the aircraft is adhering to horizontal guidance provided by a localizer signal; andexpanding the premature descent envelope when the aircraft is adhering to the vertical guidance and the horizontal guidance. 18. The non-transitory, computer-readable medium of claim 17, wherein the method further comprises: determining a localizer deviation, based on the localizer signal and current operation of the aircraft;comparing the localizer deviation to a second predefined set of acceptable localizer deviation values; andwhen the localizer deviation is in the second set, determining that the aircraft is adhering to the horizontal guidance. 19. The non-transitory, computer-readable medium of claim 15, wherein the method further comprises: when the aircraft is not adhering to the vertical guidance, maintaining the premature descent envelope for the aircraft. 20. The non-transitory, computer-readable medium of claim 15, further comprising: determining whether the aircraft is flying below increased altitude values that are indicated by the increased premature descent envelope; andwhen the aircraft is flying below the increased altitude values, generating an alert.
