System and method for providing flight cues for the navigation function required time of arrival (RTA)

• US 9,829,341 B1
• Filed: 06/26/2008
• Issued: 11/28/2017
• Est. Priority Date: 06/26/2008
• Status: Active Grant

• Current Assignee: Rockwell Collins, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Rockwell Collins, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Swiderski, Frank J., Krenz, Michael J.
• Primary Examiner(s): Zeender, F.
• Assistant Examiner(s): Racic, Milena
• Application Number:
  US12/215,294
• Time in Patent Office: 3,442 Days
• Field of Search: 701204, 701 14, 701120, 340973, 340978
• CPC Class Codes: G01C 23/00 Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration

Abstract

The present invention is a flight deck situational awareness system for displaying Required Time of Arrival (RTA) information for an aircraft. The system may include a memory configured for storing aircraft navigation information for the aircraft. The system may also include a processor. The processor may be configured for being communicatively coupled with the memory and may further be configured for receiving the aircraft navigation information stored in the memory. The processor may generate a depiction based upon the aircraft navigation information. The depiction may include a Required Time of Arrival (RTA) flight cue for the aircraft. The system may further include a display, which may be communicatively coupled with the processor. The display may receive the depiction from the processor and may display the depiction.

Claims

1. A flight deck situational awareness system for displaying Required Time of Arrival (RTA) information for an aircraft, comprising:

a memory configured for storing aircraft navigation information for the aircraft, the memory implemented on the aircraft, the aircraft navigation information including a position of the aircraft, a performance of the aircraft, an environment of the aircraft, an approach path of the aircraft, a landing area of the aircraft, and terrain information associated with the aircraft;

a processor implemented on the aircraft, the processor configured for being communicatively coupled with the memory and further configured for;

receiving the aircraft navigation information stored in the memory;

receiving an assigned RTA clearance time for an assigned RTA clearance location for the aircraft and an assigned RTA clearance window for the assigned RTA clearance location for the aircraft, the assigned RTA clearance window including the assigned RTA clearance time, the assigned RTA clearance time received from an air traffic control; and

based at least upon the aircraft navigation information and the assigned RTA clearance time, generating at least one graphical depiction including a plurality of predictive indicators indicative of whether the aircraft is predicted to reach the assigned RTA clearance location within the assigned RTA clearance window, a vertical RTA flight profile for the aircraft, an airspeed indicator for the aircraft, a vertical speed indicator (VSI) for the aircraft, a minimum vertical descent speed vector, and a maximum vertical descent speed vector, the plurality of predictive indicators including a first speed cue positioned on the airspeed indicator, a second speed cue positioned on the vertical speed indicator, and a time cue, the time cue depicting the assigned RTA clearance time relative to a current time status of the aircraft, the airspeed indicator for the aircraft being a speed tape graphical indicator; and

a display implemented on the aircraft, the display being communicatively coupled with the processor, the display being configured for;

receiving data associated with the at least one graphical depiction including the plurality of predictive indicators, the vertical RTA flight profile, the airspeed indicator, the vertical speed indicator, the minimum vertical descent speed vector, and the maximum vertical descent speed vector from the processor; and

displaying the at least one graphical depiction including the plurality of predictive indicators, the vertical RTA flight profile, the airspeed indicator, the vertical speed indicator, the minimum vertical descent speed vector, and the maximum vertical descent speed vector to a pilot, the time cue indicating that the aircraft is projected to arrive at the assigned RTA clearance location outside of the assigned RTA clearance window, the first speed cue indicating on the airspeed indicator a prescribed range of speed values for the aircraft to arrive at the assigned RTA clearance time and at the assigned RTA clearance location, the second speed cue indicating on the vertical speed indicator a prescribed range of vertical speed values for the aircraft to arrive at the assigned RTA clearance time and at the assigned RTA clearance location, wherein each of the minimum vertical descent speed vector and the maximum vertical descent speed vector is graphically depicted as a line.

2. A flight deck situational awareness system as claimed in claim 1, wherein the vertical RTA flight profile for the aircraft is at least one of an ascent profile and a descent profile.

3. A flight deck situational awareness system as claimed in claim 1, wherein the system is further configured for dynamically updating the plurality of predictive indicators in real time based upon updated aircraft navigation information for the aircraft.

4. A method for providing Required Time of Arrival (RTA) information for an aircraft via a flight deck situational awareness system of the aircraft, comprising:

storing, in a memory implemented on the aircraft, aircraft navigation information for the aircraft, the aircraft navigation information including a position of the aircraft, a performance of the aircraft, an environment of the aircraft, an approach path of the aircraft, a landing area of the aircraft, and terrain information associated with the aircraft;

receiving, by a processor implemented on the aircraft, the aircraft navigation information;

receiving, by the processor, an assigned RTA clearance time and an assigned RTA clearance window for an assigned RTA clearance location, the assigned RTA clearance window including the assigned RTA clearance time, the assigned RTA clearance time received from an air traffic control, the processor communicatively coupled to the memory;

based at least upon the aircraft navigation information and the assigned RTA clearance time, generating, by the processor, at least one graphical depiction including a plurality of predictive indicators indicative of whether the aircraft is predicted to reach the assigned RTA clearance location within the assigned RTA clearance window, a vertical RTA flight profile for the aircraft, an airspeed indicator for the aircraft, a vertical speed indicator (VSI) for the aircraft, a minimum vertical descent speed vector, and a maximum vertical descent speed vector, the plurality of predictive indicators including a first speed cue positioned on the airspeed indicator, a second speed cue positioned on the vertical speed indicator, and a time cue, the time cue depicting the assigned RTA clearance time relative to a current time status of the aircraft, the airspeed indicator for the aircraft being a speed tape graphical indicator;

receiving, by a flight deck display of the aircraft, data associated with the at least one graphical depiction including the plurality of predictive indicators, the vertical RTA flight profile, the airspeed indicator, the vertical speed indicator, the minimum vertical descent speed vector, and the maximum vertical descent speed vector from the processor; and

displaying, by the flight deck display, the at least one graphical depiction including the plurality of predictive indicators, the vertical RTA flight profile, the airspeed indicator, the vertical speed indicator, the minimum vertical descent speed vector, and the maximum vertical descent speed vector to a pilot, the time cue indicating that the aircraft is projected to arrive at the assigned RTA clearance location outside of the assigned RTA clearance window, the first speed cue indicating on the airspeed indicator a prescribed range of speed values for the aircraft to arrive at the assigned RTA clearance time and at the assigned RTA clearance location, the second speed cue indicating on the vertical speed indicator a prescribed range of vertical speed values for the aircraft to arrive at the assigned RTA clearance time and at the assigned RTA clearance location, wherein each of the minimum vertical descent speed vector and the maximum vertical descent speed vector is graphically depicted as a line.

5. A method as claimed in claim 4, further comprising:

based upon the received aircraft navigation information, determining a prescribed range of speed values for the aircraft for promoting arrival of the aircraft at the assigned RTA clearance time and at the assigned RTA clearance location.

6. A method as claimed in claim 4, further comprising:

receiving updated aircraft navigation information for the aircraft.

7. A method as claimed in claim 6, further comprising:

based at least upon the received updated aircraft navigation information, determining an updated predicted time of arrival at the assigned RTA clearance location for the aircraft.

8. A method as claimed in claim 7, further comprising:

based at least upon the updated predicted time of arrival at the assigned RTA clearance location, updating the plurality of predictive indicators including the time cue, the updated time cue indicating an updated predicted arrival status of the aircraft relative to the assigned RTA clearance time for the aircraft;

based at least upon the updated received aircraft navigation information and the updated plurality of predictive indicators, generating at least one updated depiction including the updated plurality of predictive indicators; and

displaying at least one updated depiction including the updated plurality of predictive indicators.

9. A method as claimed in claim 6, further comprising:

based upon the received updated aircraft navigation information, determining updated prescribed ranges of speed values for the aircraft for promoting arrival of the aircraft at the assigned RTA clearance time and at the assigned RTA clearance location.

10. A method as claimed in claim 9, the method further comprising:

based at least upon the updated prescribed ranges of speed values, updating the first speed cue and the second speed cue, the updated first speed cue and the updated second speed cue indicating the updated prescribed ranges of speed values;

based at least upon the updated received aircraft navigation information, generating at least one updated depiction including an updated plurality of predictive indicators including the updated first speed cue and the updated second speed cue; and

displaying the at least one updated depiction including the updated plurality of predictive indicators including the updated first speed cue and the updated second speed cue.

11. A computer-readable medium having non-transitory computer readable code embodied therein, the non-transitory computer readable code comprising instructions which, when executed by a computer device processor, perform a method for providing Required Time of Arrival (RTA) information for an aircraft via a flight deck situational awareness system of the aircraft, said method comprising:

receiving, by the computer device processor implemented on the aircraft, aircraft navigation information for the aircraft, the aircraft navigation information including a position of the aircraft, a performance of the aircraft, an environment of the aircraft, an approach path of the aircraft, a landing area of the aircraft, and terrain information associated with the aircraft;

receiving, by the computer device processor, an assigned RTA clearance time for an assigned RTA clearance location for the aircraft and an assigned RTA clearance window for the assigned RTA clearance location for the aircraft, the assigned RTA clearance window including the assigned RTA clearance time, the assigned RTA clearance time received from an air traffic control;

based at least upon the aircraft navigation information and the assigned RTA clearance time, generating, by the computer device processor, at least one graphical depiction including a plurality of predictive indicators indicative of whether the aircraft is predicted to reach the assigned RTA clearance location within the assigned RTA clearance window, a vertical RTA flight profile for the aircraft, an airspeed indicator for the aircraft, a vertical speed indicator (VSI) for the aircraft, a minimum vertical descent speed vector, and a maximum vertical descent speed vector, the plurality of predictive indicators including a first speed cue positioned on the airspeed indicator, a second speed cue positioned on the vertical speed indicator, and a time cue, the time cue depicting the assigned RTA clearance time relative to a current time status of the aircraft, the airspeed indicator for the aircraft being a speed tape graphical indicator; and

outputting, by the computer device processor, data associated with the at least one graphical depiction including the plurality of predictive indicators, the vertical RTA flight profile, the airspeed indicator, the vertical speed indicator, the minimum vertical descent speed vector, and the maximum vertical descent speed vector from the processor,

wherein, based at least on a reception of the data associated with the at least one graphical depiction, the flight deck display is configured to display the at least one graphical depiction including the plurality of predictive indicators, the vertical RTA flight profile, the airspeed indicator, the vertical speed indicator, the minimum vertical descent speed vector, and the maximum vertical descent speed vector to a pilot, the time cue indicating that the aircraft is projected to arrive at the assigned RTA clearance location outside of the assigned RTA clearance window, the first speed cue indicating on the airspeed indicator a prescribed range of speed values for the aircraft to arrive at the assigned RTA clearance time and at the assigned RTA clearance location, the second speed cue indicating on the vertical speed indicator a prescribed range of vertical speed values for the aircraft to arrive at the assigned RTA clearance time and at the assigned RTA clearance location, wherein each of the minimum vertical descent speed vector and the maximum vertical descent speed vector is graphically depicted as a line.