Abstract: A new hybrid method for displaying, detecting, and selecting objects in a CAD system is disclosed. A CAD model is loaded and displayed using one of several render techniques to approximate natural visual perception (e.g. hidden-line rendering, solid rendering or 3D textured rendering). These render techniques necessarily hide parts of the model to approximate natural vision; additionally, only objects visible to the rendered presentation may be detected (as geometry “snapped to” for additional constructions) or selected for editing. The hybrid presentation method provides in any editing context an instantly available “x-ray view” that apparently de-renders the model in a region surrounding the point of interest and makes any part of the model at any depth visible within the region available for detection, selection or editing. In this mode objects are selectable not by their faces, but by their edges, which are more easily distinguished and picked in this view.

Abstract: A system and method for selecting a runway, comprises retrieving runway feature data and aircraft data including aircraft heading with respect to the bearing of first and second runways. Runway boundary envelopes are created for each of the first and second runways, each having a predetermined score. A total score for each of the first and second runways is compared to determine which of the runways is selected.

Abstract: A system and method for passively detecting aircraft wingtip strikes includes generating a digital base map represented by a plurality of aerodrome cells. A numeric value is assigned to each of the aerodrome cells that is representative of the specific wingtip strike threat associated with that aerodrome cell. An index count array is generated that has a separate entry for each numeric value. A digital aircraft structure is generated that is representative of an aircraft, and is represented by a plurality of aircraft cells. A portion of the aerodrome cells are replaced with the plurality of aircraft cells. Each numeric value of the aerodrome cells that are replaced is counted to determine a replacement count associated therewith and that is entered into the separate entry in the index count array for that numeric value. One or more potential aircraft wingtip strikes are detected based on the replacement counts.

Abstract: Systems and methods for verifying that the flight crew has not made an error in entering takeoff flight performance data into the flight management system (FMS) using the electronic flight bag (EFB). The EFB includes a user interface that receives basic flight plan information and a processor. The processor automatically receives calculated takeoff performance data based on a previously entered basic flight plan, automatically receives user-entered takeoff performance data from a flight management system (FMS) located on a host aircraft, automatically compares the calculated takeoff performance data to the received takeoff performance data, and generates an entry error indication, if the comparison indicates that at least a portion of the entered takeoff performance data does not match the calculated takeoff performance data. An output device outputs the generated entry error indication.

Abstract: A system and method are provided for alerting of remaining runway based on deceleration, following, for example, a landing or discontinued takeoff. An advisory system compares the current aircraft deceleration value to a predetermined threshold value when proceeding down the runway. If the current aircraft deceleration is less than the threshold value, the runway distance remaining callouts are triggered.

Abstract: A system and method provide an alert to a pilot of an aircraft aurally with a given volume and inflection, and/or visually with a text message which includes color, font, and pitch (size). The alert is rendered in distinct fashion for the expected and unexpected cases, e.g., an intended runway and an unintended runway. In a preferred embodiment, the alert for the intended runway is changed to a confirmation level, or one that is less likely to interfere with other information flow, while the alert for the unintended runway would be provided in a more conspicuous manner.

Abstract: In one embodiment of the present invention, a method for concurrently constructing and testing a software program is provided. The method includes interacting with a program editor that allows a user to construct the program, and testing the program during construction of the program to produce a test result.

Abstract: Systems and methods for adjusting target approach speed for use in a “Too Fast” approach to landing condition. An exemplary system stores predefined maximum wind setting and a predefined reference speed and a pilot set bug speed value. A processing device sets a target speed equal to the bug speed, if the bug speed is less than the reference speed plus a value associated with a predefined maximum wind setting, and sets the target speed equal to the reference speed plus the max wind added value, if the manual bug speed is not less than the reference speed plus the max wind added value. An output device outputs an alert if the received aircraft speed is greater than the set target speed plus a predefined error value when the received aircraft location is within a threshold value of a touchdown point.

Abstract: A system and method monitor aircraft state parameters, for example, aircraft movement and flight parameters, applies those inputs to a spatial disorientation model, and makes a prediction of when pilot may become spatially disoriented. Once the system predicts a potentially disoriented pilot, the sensitivity for alerting the pilot to conditions exceeding a threshold can be increased and allow for an earlier alert to mitigate the possibility of an incorrect control input.

Abstract: Embodiments of a flight deck display system deployed onboard an aircraft are provided, as are embodiments of a method carried-out by a flight deck display system. In one embodiment, the flight deck display system includes a cockpit display device and a controller. The controller is configured to: (i) establish the speed trend of the aircraft over a predetermined time period; (ii) generate a primary flight display on the cockpit display device including a speed trend vector graphic representative of the established speed trend; and (iii) alter the appearance of the speed trend vector graphic in a first predetermined manner if a low speed change condition is detected during at least one of aircraft takeoff and landing.

Abstract: The present invention provides an encryption/decryption approach to protect valuable information from being represented in a clear-text form when an application processes the valuable information. The present invention processes a structured input file to create internal data structures and generates an encrypted output file from the extracted internal data structures. The encrypted file of internal data structures can be decrypted to enable further processing of the valuable information without representing the valuable information as clear-text in memory. Further, the decrypted internal data structures are stored at different locations in memory.

Abstract: Systems and methods for verifying that the flight crew has not made an error in entering takeoff flight performance data into the flight management system (FMS) using the electronic flight bag (EFB). The EFB includes a user interface that receives basic flight plan information and a processor. The processor automatically receives calculated takeoff performance data based on a previously entered basic flight plan, automatically receives user-entered takeoff performance data from a flight management system (FMS) located on a host aircraft, automatically compares the calculated takeoff performance data to the received takeoff performance data, and generates an entry error indication, if the comparison indicates that at least a portion of the entered takeoff performance data does not match the calculated takeoff performance data. An output device outputs the generated entry error indication.

Abstract: Exemplary embodiments may provide one or more computer readable storage media storing executable instructions that when executed on processing logic output a source code listing and external content to an editor. The media may hold instructions for creating a source code listing in an editor, the source code listing being executable when the source code listing is compiled or interpreted. The media may further hold instructions for inserting a non-executable statement into the source code listing, the non-executable statement including metadata identifying external content. The media may hold instructions for interpreting the metadata. The media may further hold instructions for communicating with external content. The media may also hold instructions for outputting the source code listing and the external content to the editor. The media may further hold instructions for interacting with the external content from the source code listing.

Abstract: An automatic graphics delivery system that operates in parallel with an existing Web site infrastructure is provided. The system streamlines the post-production process by automating the production of media through content generation procedures controlled by proprietary tags placed by an author within URLs embedded within Web documents.

Abstract: In an embodiment, code may be acquired that calls a first function defined to return a plurality of output arguments. The code may designate, with a designator, one or more output arguments, in the plurality of output argument, that are not present. Processing logic may generate a second function based at least on the designated one or more output arguments being designated as not present.

Abstract: An improved stable approach monitor (SAM) system provides an audible advisory to a pilot when an aircraft is on a final landing approach. More specifically, the SAM system compares a measured airspeed of the aircraft to a predetermined flap placard speed. If the measured airspeed exceeds the predetermined flap placard speed then the improved SAM system provides an audible advisory indicating the airspeed of the aircraft is too fast. Advantageously, this audible advisory should prevent the pilot from attempting to deploy the flaps at an excessive airspeed and in turn focuses the pilot's attention on the problem at hand, which would be to reduce the airspeed of the aircraft. Once the airspeed is equal to or below the predetermined flap placard speed, the improved SAM system may provide another audible advisory informing the pilot to commence deployment of the flaps.

Abstract: A user interface, such as a graphical user interface or other electronic displayable interface, is contemplated. The user interface may include a reading lens portion configured to facilitate providing expanded viewing of content from other portions of the display. The reading lens portion may be displayed according to a non-linear timeline as to facilitate identifying upcoming contents without being constrained by a linear timeline used in other portions of the user interface.

Abstract: Exemplary embodiments may provide methods, systems and devices for providing non-literal representations of programming language code. The non-literal representation of a portion of code may provide a representation of the semantics of the portion of code that is different from the source code representation. The non-literal representation may change the way the code is output to a user in order to improve readability of the source code, and may not modify the underlying structure or semantics of the code. While improving readability of the code, the non-literal representation may also retain important information about the underlying code associated with the non-literal representation.

Abstract: Systems and methods for alerting for potential tailstrike during landing. A processing device located onboard an aircraft determines whether the aircraft is in a landing operational mode. If the aircraft is determined within the landing operational mode, the processing device determines whether aircraft speed is less than a previously defined threshold speed and generates an alert signal if it is determined that the aircraft's speed is less than the previously defined threshold speed. An output device located onboard the aircraft, outputs an alert based on the generated alert signal.

Abstract: A user interface, such as a graphical user interface or other electronic displayable interface, is contemplated. The user interface may include a reading lens portion configured to facilitate providing expanded viewing of content from other portions of the display. The reading lens portion may be displayed according to a non-linear timeline as to facilitate identifying upcoming contents without being constrained by a linear timeline used in other portions of the user interface.