Systems and methods for status reporting for aircraft
An aircraft monitoring system includes a sensor operatively connected to at least a portion of an aircraft, a memory configured to store instructions, and a processor disposed in communication with the memory and the sensor. The processor, upon execution of the instructions, is configured to display a graphical representation of the portion of the aircraft reflecting real-time monitoring activity, and display a monitoring controller. A method of providing a graphical user interface (GUI) for an aircraft monitoring system includes displaying a graphical representation of at least a portion of an aircraft's geometry reflecting real-time monitoring activity. The method includes displaying one or more monitoring controllers. Each monitoring controller is associated with at least a portion of an aircraft monitoring system and a location on the aircraft's geometry.
1. An aircraft monitoring system comprising:
a sensor operatively connected to at least a portion of an aircraft;
a memory configured to store instructions;
a processor disposed in communication with the memory and the sensor, wherein the processor, upon execution of the instructions is configured to:
display a graphical representation of the portion of the aircraft; and
display a monitoring controller, wherein the monitoring controller is associated with the portion of the aircraft
wherein displaying the monitoring controller includes displaying the monitoring controller in a respective position more proximate to a portion of a graphical representation that corresponds to a location on the aircraft's geometry associated with the monitoring controller than to other portions of the graphical representation, wherein displaying the monitoring controller includes displaying, a plurality of passive status indicators indicative of statuses of respective sub-functions and, simultaneously, an active progress indicator indicative of which of the sub-functions is in progress.
2. The system as recited in claim 1 , wherein each monitoring controller includes an active progress indicator representative of the progress of a monitoring sub-function for the portion of the aircraft in real-time.
3. The system as recited in claim 1 , wherein each monitoring controller includes at least one status indicator representative of the real-time status of an overall monitoring function for the portion of the aircraft.
4. A non-transitory computer readable storage medium having one or more computer programs stored therein associated with an aircraft monitoring system, the computer programs comprising instructions, which when executed by a processor of a computer system, cause the processor to:
display a graphical representation of at least a portion of an aircraft's geometry; and
display one or more monitoring controllers, wherein each monitoring controller is associated with at least a portion of the aircraft monitoring system and a location on the aircraft's geometry
wherein displaying the one or more monitoring controllers includes displaying each monitoring controller in a respective position more proximate to a portion of the graphical representation that corresponds to the location on the aircraft's geometry associated with the monitoring controller than to other portions of the graphical representation, wherein displaying the one or more monitoring controllers includes displaying, for each monitoring controller, a plurality of passive status indicators indicative of statuses of respective sub-functions and, simultaneously, an active progress indicator indicative of which of the sub-functions is in progress.
5. The non-transitory computer readable storage medium as recited in claim 4 , wherein at least one of the one or more monitoring controllers is positioned in a respective position more proximate to a portion of the graphical representation that corresponds to the location on the aircraft's geometry associated with the monitoring controller than to other portions of the graphical representation.
6. A method of providing a graphical user interface (GUI) for an aircraft monitoring system, the method comprising:
displaying a graphical representation of at least a portion of an aircraft's geometry; and
displaying one or more monitoring controllers, wherein each monitoring controller is associated with at least a portion of an aircraft monitoring system and a location on the aircraft's geometry,
wherein displaying the one or more monitoring controllers includes displaying each monitoring controller in a respective position more proximate to a portion of the graphical representation that corresponds to the location on the aircraft's geometry associated with the monitoring controller than to other portions of the graphical representation, wherein displaying the one or more monitoring controllers includes displaying, for each monitoring controller, a plurality of passive status indicators indicative of statuses of respective sub-functions and, simultaneously, an active progress indicator indicative of which of the sub-functions is in progress.
7. The method as recited in claim 6 , wherein displaying the graphical representation includes displaying a first portion of the aircraft's geometry and a second portion of the aircraft's geometry, wherein displaying the one or more monitoring controllers includes displaying a first monitoring controller associated with the first portion, wherein the first monitoring controller is positioned closer to the first portion than the second portion.
8. The method as recited in claim 6 , wherein displaying the one or more monitoring controllers, includes displaying, for each monitoring controller, at least one of an active progress indicator or a passive status indicator.
9. The method as recited in claim 6 , wherein the method includes displaying both the active progress indicator and one of the plurality of passive status indicators to which the active progress indicator relates with a common graphical theme in order for a user to easily ascertain an overall status of the sub-functions.
10. The method as recited in claim 6 , wherein each monitoring controller includes a user entry area for receiving at least one of an on command, a start command or a download command.
11. The method as recited in claim 6 , further comprising providing a user entry area for receiving a start command configured and adapted to begin monitoring functions for a plurality of monitoring controllers.
12. The method as recited in claim 6 , wherein the method includes displaying an active progress indicator that corresponds to the monitoring controller and is representative of the progress of a monitoring sub-function for the portion of the aircraft monitoring system associated therewith.
13. The method as recited in claim 11 , wherein the monitoring sub-function includes least one of a acquiring data, downloading data, transferring data, converting data or uploading data.
14. The method as recited in claim 6 , wherein the method includes displaying a passive status indicator representative of the status of a monitoring function for the portion of the aircraft monitoring system associated therewith.
15. The method as recited in claim 6 , further comprising displaying a health status of at least one portion of the aircraft with a health indicator overlaid onto a portion of the graphical representation of the aircraft to which the health status pertains.
16. The method as recited in claim 6 , further comprising displaying a health status of at least one portion of the aircraft with a health indicator and providing a user entry area associated with the health indicator for receiving user commands to initiate system action.
17. The method as recited in claim 6 , wherein displaying the graphical representation includes displaying the graphical representation on a computing device having a display screen.
18. The method as recited in claim 6 , wherein displaying the one or more monitoring controllers includes displaying the one or more monitoring controllers on a computing device having a display screen.