초록 ▼

Methods and apparatus are provided for indicating safe or potentially hazardous operating conditions of an aircraft in a required navigational performance (RNP) environment. The apparatus comprises a course deviation display field with first and second markers defining outer boundaries of the RNP wi

Methods and apparatus are provided for indicating safe or potentially hazardous operating conditions of an aircraft in a required navigational performance (RNP) environment. The apparatus comprises a course deviation display field with first and second markers defining outer boundaries of the RNP width and a central marker indicating the desired course within the RNP width, an aircraft estimated position uncertainty (EPU) marker in the display field whose size corresponds to the EPU relative to the RNP and a current aircraft position marker coupled to the EPU marker and moving therewith as the aircraft position changes with respect to the RNP width. The display desirably changes color and/or flashes to alert a pilot to a potentially hazardous condition when an outer boundary of the EPU marker approaches to within a predetermined guard-band distance of or overlaps either of the first or second markers. An audible warning can be included.

대표청구항 ▼

1. A flight display for aircraft comprising:a course deviation indicator display field with first and second markers defining outer boundaries of a required navigational performance width and having a central marker indicating the desired course within the required navigational performance width; an

1. A flight display for aircraft comprising:a course deviation indicator display field with first and second markers defining outer boundaries of a required navigational performance width and having a central marker indicating the desired course within the required navigational performance width; an aircraft estimated position uncertainty marker in the display field whose size corresponds to the estimated position uncertainty; and a current aircraft position marker coupled to the estimated position uncertainty marker and moving therewith as the aircraft position changes with respect to the required navigational performance width. 2. The display of claim 1 further comprising an alarm means, wherein the alarm means alerts a pilot when an outer boundary of the expected performance uncertainty marker approaches to within a predetermined guard-band amount of either of the first or second markers or lies outside either of the first or second markers.3. The display of claim 2 wherein the alarm means includes changing a color of the expected performance uncertainty marker to a color suggestive of a Hazard Warning.4. The display of claim 2 wherein the alarm means includes causing the estimated position uncertainty marker or required navigation performance markers or both to flash on and off.5. The display of claim 2 wherein the alarm means includes an audible alarm.6. The display of claim 1 further comprising an alarm means, wherein the alarm means alerts a pilot when an outer boundary of the expected performance uncertainty marker impinges on or crosses over either of the first or second markers.7. The display of claim 1 wherein the estimated position uncertainty marker has a winglet shape with a wingspan corresponding to the size of the expected performance uncertainty.8. The display of claim 1 wherein a distance between the first and second markers on the display is fixed independent of the size of the required navigational performance width.9. The display of claim 8 wherein the size of the estimated position uncertainty marker is shown on the display in relation to the required navigational performance width.10. The display of claim 1 further comprising a field that indicates when illuminated, that required navigational performance operating conditions are existent.11. The display of claim 1 further comprising a field that numerically shows the required navigational performance width.12. The display of claim 1 further comprising a field that numerically shows the estimated position uncertainty.13. The display of claim 1 further comprising a second course deviation indicator display field comprising a second required navigational performance width, second aircraft estimated position uncertainty markers and second current aircraft position maker, the combination indicating vertical course deviation.14. A method for indicating when a potentially unsafe aircraft operating condition is existent, comprising:determining a required navigational performance width between first and second outer boundaries thereof, an estimated position uncertainty having third and fourth opposed outer boundaries in a first direction substantially parallel to the required navigational performance width, and a current course deviation between actual and planned position in the first direction; presenting the required navigational performance width, the estimated position uncertainty and the current course deviation on a display, wherein the required navigational performance width and the estimated position uncertainty are shown separately in the same field; and when either of the third or fourth boundaries approaches within a predetermined guard-band of or overlaps either of the first or second boundaries, announcing optically, audibly or both that a potentially hazardous condition has occurred. 15. The method of claim 14 wherein the presenting step comprises presenting the course deviation by showing a planned course marker within the first and second boundaries and showing an actual aircraft position marker within the third and fourth boundaries, and moving the actual aircraft position marker and the third and fourth boundaries in unison as the aircraft operating conditions change.16. The method of claim 14 wherein the presenting step comprises showing the required navigational width by fixed scale markers whose outermost members comprise the first and second boundaries, and showing the estimated position uncertainty in the form of a winglet whose wingtips correspond to the third and fourth boundaries.17. A display for indicating safe or potentially hazardous operation of an aircraft, comprising:scale markers distributed in a first direction, whose outermost members indicate a required navigation performance width within which it is desired that the aircraft operate and which contains an indicator showing the planned position of the aircraft with respect to the required navigational performance width; a variable size marker whose extent between outer boundaries in the first direction indicates an estimated position uncertainty of the aircraft with respect to its actual position and which contains a current position marker, wherein both move in unison in the first direction as the actual aircraft position varies with respect to it planned position; and annunciator means indicating a change from safe to potentially hazardous operating conditions when either outer boundary of the variable size marker encroaches within a predetermined guard-band distance of either outermost member of the required navigational performance scale markers or lies outside of either of the outermost members. 18. The display of claim 17 wherein the annunciator means indicates a safe operating condition when either outer boundary of the variable size marker does not so encroach or lie outside.