Abstract: A crew alerting system for a mobile platform includes a display device defining a display area, a processor operatively coupled to the display device, and a memory storing instructions that cause the processor to: upon receiving notification of an occurrence of a manual system configuration associated with the mobile platform, generate a first output for causing the display device to display a first indication in the display area, the first indication comprising a first textual message. The processor is further configured to, upon receiving notification of an occurrence of an automated system configuration associated with the mobile platform, generate a second output for causing the display device to display a second indication in the display area, the second indication comprising a second textual message accompanied by a supplemental indication such as a graphical indication.

Abstract: Systems, devices and methods for alerting a crew of an aircraft or other mobile platform of a relevant condition associated with the aircraft are disclosed. One exemplary method comprises receiving data indicative of an existence of the relevant condition associated with the aircraft; receiving data indicative of a substantially real-time value of a dynamic parameter associated with the relevant condition; and displaying an awareness-enhancing indication associated with the relevant condition in a display area of the crew alerting system of the aircraft. The awareness-enhancing indication comprises a textual message and a supplemental indication indicative of the substantially real-time value of the dynamic parameter associated with the relevant condition. In various embodiments, the supplemental indication may be textual or graphical. The supplemental indication may also be indicative of a target value of the dynamic parameter.

Abstract: Systems, devices and methods for alerting a crew of an aircraft or other mobile platform of a relevant condition associated with the aircraft are disclosed. One exemplary method comprises receiving data indicative of an existence of the relevant condition associated with the aircraft; receiving data indicative of a substantially real-time value of a dynamic parameter associated with the relevant condition; and displaying an awareness-enhancing indication associated with the relevant condition in a display area of the crew alerting system of the aircraft. The awareness-enhancing indication comprises a textual message and a supplemental indication indicative of the substantially real-time value of the dynamic parameter associated with the relevant condition. In various embodiments, the supplemental indication may be textual or graphical. The supplemental indication may also be indicative of a target value of the dynamic parameter.

Abstract: Controllers and methods for enabling an operator to interface with an aircraft system are provided. A method includes receiving a first input to the aircraft system via angular displacement of a rotatable knob in a first direction away from a neutral angular position of the rotatable knob, causing the rotatable knob to automatically return to the neutral angular position, and annunciating, via the rotatable knob, a first state of the aircraft system associated with the first input. The method also includes receiving a second input to the aircraft system from a source different from the rotatable knob, and annunciating, via the rotatable knob, a second state of the aircraft system associated with the second input.

Abstract: The present disclosure describes displaying on a flight deck (12) graphical presentations indicative of performance limitations of an aircraft (10) resulting from an in-flight aircraft reconfiguration. The graphical presentations are co-located on the flight deck (12) with the graphical presentations of the aircraft (10) and/or system (34) parameters to which the performance limitations apply.

Abstract: Methods and systems for assisting a pilot during flight of an aircraft are disclosed. The method includes receiving data indicative of a current location of the aircraft during flight and data indicative of a flight boundary, and determining that the flight boundary is relevant to the aircraft. The method also includes causing a display device to display a surface representing the flight boundary relative to the current location of the aircraft.

Abstract: Systems, devices and methods for alerting a crew of an aircraft or other mobile platform of a relevant condition associated with the aircraft are disclosed. One exemplary method comprises receiving data indicative of an existence of the relevant condition associated with the aircraft; receiving data indicative of a substantially real-time value of a dynamic parameter associated with the relevant condition; and displaying an awareness-enhancing indication associated with the relevant condition in a display area of the crew alerting system of the aircraft. The awareness-enhancing indication comprises a textual message and a supplemental indication indicative of the substantially real-time value of the dynamic parameter associated with the relevant condition. In various embodiments, the supplemental indication may be textual or graphical. The supplemental indication may also be indicative of a target value of the dynamic parameter.

Abstract: Systems and methods for assisting a flight crew of an aircraft with controller-pilot data link communication (CPDLC) are provided. A display device defines a display area on a flight deck of the aircraft. A controller is operatively coupled to the display device and configured to control a presence of a CPDLC window containing a CPDLC message in the display area. A plurality of tactile buttons are disposed proximally to each other on a glare shield panel of the flight deck. The plurality of tactile buttons comprises a first tactile button operatively coupled to the controller for selectively instructing the controller to cause the presence of the CPDLC window in the display area by actuation of the first tactile button, and a second tactile button configured to permit the flight crew to respond to the CPDLC message by actuation of the second tactile button.

Abstract: Systems, devices and methods for alerting a crew of an aircraft or other mobile platform of a relevant condition associated with the aircraft are disclosed. One exemplary method comprises receiving data indicative of an existence of the relevant condition associated with the aircraft; receiving data indicative of a substantially real-time value of a dynamic parameter associated with the relevant condition; and displaying an awareness-enhancing indication associated with the relevant condition in a display area of the crew alerting system of the aircraft. The awareness-enhancing indication comprises a textual message and a supplemental indication indicative of the substantially real-time value of the dynamic parameter associated with the relevant condition. In various embodiments, the supplemental indication may be textual or graphical. The supplemental indication may also be indicative of a target value of the dynamic parameter.

Abstract: Apparatus and methods for assisting a flight crew with (e.g., pre-flight) functional testing of aircraft systems are disclosed. An aircraft condition can be used to select one or more functional tests that are applicable based on the aircraft condition. The aircraft condition can be used to initiate the execution of the one or more applicable selected functional tests. The aircraft condition can also be used to identify the one or more functional tests that are applicable on a display device so as to guide the flight crew during the execution of the functional tests.

Abstract: Systems and methods for controlling a display device of an aircraft are disclosed. The method includes using operational data associated with the aircraft, causing a primary flight display representation to be displayed on the display device where the primary flight display representation includes a first textual object having a first font size. The method also includes causing the display device to display a second textual object having a second font size. The second font size is 2.5 or more times larger than the first font size.

Abstract: Systems and methods for assisting a flight crew of an aircraft with controller-pilot data link communication (CPDLC) are provided. A display device defines a display area on a flight deck of the aircraft. A controller is operatively coupled to the display device and configured to control a presence of a CPDLC window containing a CPDLC message in the display area. A plurality of tactile buttons are disposed proximally to each other on a glare shield panel of the flight deck. The plurality of tactile buttons comprises a first tactile button operatively coupled to the controller for selectively instructing the controller to cause the presence of the CPDLC window in the display area by actuation of the first tactile button, and a second tactile button configured to permit the flight crew to respond to the CPDLC message by actuation of the second tactile button.

Abstract: Methods and systems for assisting a pilot during flight of an aircraft are disclosed. The method includes receiving data indicative of a current location of the aircraft during flight and data indicative of a flight boundary, and determining that the flight boundary is relevant to the aircraft. The method also includes causing a display device to display a surface representing the flight boundary relative to the current location of the aircraft.

Abstract: The present disclosure describes displaying on a flight deck (12) graphical presentations indicative of performance limitations of an aircraft (10) resulting from an in-flight aircraft reconfiguration. The graphical presentations are co-located on the flight deck (12) with the graphical presentations of the aircraft (10) and/or system (34) parameters to which the performance limitations apply.

Abstract: A crew alerting system for a mobile platform includes a display device defining a display area, a processor operatively coupled to the display device, and a memory storing instructions that cause the processor to: upon receiving notification of an occurrence of a manual system configuration associated with the mobile platform, generate a first output for causing the display device to display a first indication in the display area, the first indication comprising a first textual message. The processor is further configured to, upon receiving notification of an occurrence of an automated system configuration associated with the mobile platform, generate a second output for causing the display device to display a second indication in the display area, the second indication comprising a second textual message accompanied by a supplemental indication such as a graphical indication.

Abstract: Systems, methods and computer program products for controlling the movement of a cursor on a display device in an aircraft are disclosed. An exemplary method disclosed comprises the use of a digital representation of a grid defining a plurality of cells overlaying at least a portion of a display area of the display device to control the movement of the cursor over the display area. The grid may be invisible to the user during operation.

Abstract: Systems, devices and methods a for assisting a pilot with aircraft landing are disclosed. One exemplary method comprises receiving data representative of a current approach/landing capability of the aircraft and data representative of an approach/landing intent of the pilot; and showing a combined indicator graphically and simultaneously indicating the current approach/landing capability of the aircraft and the approach/landing intent of the pilot on a display device of the aircraft. The approach/landing intent of the pilot may be graphically indicated via cooperation between a first graphical object of the indicator and a second graphical object of the indicator. The method may graphically indicate a system degradation affecting the current approach/landing capability of the aircraft with the same indicator.

Abstract: Systems, devices and methods a for use with one or more high-lift flight control surfaces (24) of aircraft are disclosed. One exemplary method comprises receiving data representative of a commanded configuration (48) for a high-lift flight control surface (24); and on a display device (14) of the aircraft, showing an indicator (30) indicating the commanded configuration and a corresponding commanded position (50) for the high-lift flight control surface (24). The indicator (30) graphically indicates a correlation between the commanded configuration (48) and the corresponding commanded position (50) for the high-lift flight control surface (24).

Abstract: The present disclosure relates to a check-list display system (100), a method, a graphical interface (120) and a computer program product. The checklist display system, method, graphical interface and computer program product display in a first segment (202) of one page of the checklist display (200) at least one normal checklist identifier (210). The checklist display system, method, graphical interface and computer program further display in a second segment (206) of the one page of the checklist display at least one non-normal checklist identifier (220) and at least one limitation information (230) relating to one of the non-normal checklist.

Abstract: Systems, devices and methods for alerting a crew of an aircraft or other mobile platform of a relevant condition associated with the aircraft are disclosed. One exemplary method comprises receiving data indicative of an existence of the relevant condition associated with the aircraft; receiving data indicative of a substantially real-time value of a dynamic parameter associated with the relevant condition; and displaying an awareness-enhancing indication associated with the relevant condition in a display area of the crew alerting system of the aircraft. The awareness-enhancing indication comprises a textual message and a supplemental indication indicative of the substantially real-time value of the dynamic parameter associated with the relevant condition. In various embodiments, the supplemental indication may be textual or graphical. The supplemental indication may also be indicative of a target value of the dynamic parameter.