Abstract: An interactive speed profile bar that enables crew awareness of the overall planned flight trajectory speed profile. The speed profile bar will have a graphical depiction (e.g., virtual buttons having alphanumeric symbology) of some or all of the speed segments of the speed profile. Each graphical element (e.g., virtual button) includes symbology identifying the applicable speed mode and corresponding target speed change. Each speed segment will start at the inflection point where the speed change will occur in the flight plan, and will continue until the next trajectory speed change. The speed profile bar will be interactive, allowing the flight crew to select the speed segment to change, in response to which selection the system displays graphical user interface elements showing a menu of the available speed segment options. Each individual speed segment is represented by an individual virtual button that can be selected by touching the screen or other input device.

Abstract: An interactive speed profile bar that enables crew awareness of the overall planned flight trajectory speed profile. The speed profile bar will have a graphical depiction (e.g., virtual buttons having alphanumeric symbology) of some or all of the speed segments of the speed profile. Each graphical element (e.g., virtual button) includes symbology identifying the applicable speed mode and corresponding target speed change. Each speed segment will start at the inflection point where the speed change will occur in the flight plan, and will continue until the next trajectory speed change. The speed profile bar will be interactive, allowing the flight crew to select the speed segment to change, in response to which selection the system displays graphical user interface elements showing a menu of the available speed segment options. Each individual speed segment is represented by an individual virtual button that can be selected by touching the screen or other input device.

Abstract: An interactive speed profile bar that enables crew awareness of the overall planned flight trajectory speed profile. The speed profile bar will have a graphical depiction (e.g., virtual buttons having alphanumeric symbology) of some or all of the speed segments of the speed profile. Each graphical element (e.g., virtual button) includes symbology identifying the applicable speed mode and corresponding target speed change. Each speed segment will start at the inflection point where the speed change will occur in the flight plan, and will continue until the next trajectory speed change. The speed profile bar will be interactive, allowing the flight crew to select the speed segment to change, in response to which selection the system displays graphical user interface elements showing a menu of the available speed segment options. Each individual speed segment is represented by an individual virtual button that can be selected by touching the screen or other input device.

Abstract: A flight information system may include a plan vertical situation display. The plan vertical situation display may display a vertical view of a flight path of an aircraft. The plan vertical situation display may display at least one path symbol showing at least one of a current path of the aircraft, a modified but not executed route of the aircraft, and an inactive route of the aircraft. The at least one path symbol may be adapted to display each of the current path of the aircraft, the modified but not executed route of the aircraft, and the inactive route of the aircraft. The plan vertical situation display may further display at least one terrain symbol showing a vertical terrain in the flight path along the at least one path symbol.

Abstract: Systems and methods for presenting and obtaining flight control information are disclosed. In one embodiment, information corresponding to a vertical motion of the aircraft can be displayed between information corresponding to a lateral motion of the aircraft and information corresponding to an airspeed of the aircraft. The information displayed can include a current mode for controlling the motion of the aircraft, a current target to which the aircraft is being directed and, at least proximate to both the current mode and the current target, a subsequent target to which the aircraft will be directed after attaining the current target.

Abstract: Apparatuses and methods for displaying autoflight information and controlling autoflight systems. In one embodiment, a flight deck for an aircraft having an autoflight system includes at least one pilot seat, at least one window positioned forward of the pilot seat, and a forward instrument panel positioned forward of the pilot seat. In one aspect of this embodiment, the forward window provides a forward field of view out of the aircraft for a pilot seated in the pilot seat. In another aspect of this embodiment, the flight deck further includes a display device configured to provide information related to one or more autoflight modes. The display device can be positioned at least approximately between the forward instrument panel and the forward window to provide the pilot with autoflight information at least proximate to the forward field of view. In a further aspect of this embodiment, the display device can be configured to provide information related to one or more target flight parameters.

Abstract: Methods and apparatuses for displaying and receiving tactical and strategic flight guidance information are disclosed. A method in accordance with one aspect of the invention includes displaying at least one first indicator to an operator of the aircraft, with a first indicator corresponding to a first instruction input by the operator for directing a first aircraft behavior and implemented upon receiving an activation instruction from the operator. At least one second indicator corresponding to a second instruction for directing a second aircraft behavior at least proximately the same as the first aircraft behavior is displayed, with the at least one second instruction to be automatically implemented at a future time. The at least one second indicator is at least approximately the same as the at least one first indicator. Indicators can be hierarchically organized to simplify presentation and reduce pilot training time.

Abstract: Methods and systems for handling aircraft control information are disclosed. A system in accordance with one embodiment of the invention includes a display medium coupleable to a flight manager, with the flight manager configured to receive and direct instructions for automatically controlling aircraft functions at a future time during flight of the aircraft. The system can further include a display controller coupled to the display medium to present at least one operator activatable element at the display medium and update information presented at the display medium when the operator activates the operator activatable element. For example, the operator activatable element can include an icon presented at a computer display screen, and can be activated by a keystroke.

Abstract: A system may generate a modified flight plan for an aircraft based on an original flight plan. The system may provide an automatic strategic offset function that includes an autoflight system; a sensor system including at least one of a global positioning system, an inertial reference unit, or an air data computer; and a flight management computer. The flight management computer may be operably coupled with the autoflight system and/or the sensor system. The flight management computer may process a flight plan of the vehicle and generate a non-uniform offset value in the vertical and/or lateral orientation between the flight plan and a boundary. The offset value may be used to create an offset flight plan for navigating an aircraft.

Abstract: Methods and apparatuses for displaying and receiving tactical and strategic flight guidance information are disclosed. A method in accordance with one aspect of the invention includes displaying at least one first indicator to an operator of the aircraft, with a first indicator corresponding to a first instruction input by the operator for directing a first aircraft behavior and implemented upon receiving an activation instruction from the operator. At least one second indicator corresponding to a second instruction for directing a second aircraft behavior at least proximately the same as the first aircraft behavior is displayed, with the at least one second instruction to be automatically implemented at a future time. The at least one second indicator is at least approximately the same as the at least one first indicator. Indicators can be hierarchically organized to simplify presentation and reduce pilot training time.

Abstract: Methods and apparatuses for displaying and receiving tactical and strategic flight guidance information are disclosed. A method in accordance with one aspect of the invention includes displaying at least one first indicator to an operator of the aircraft, with a first indicator corresponding to a first instruction input by the operator for directing a first aircraft behavior and implemented upon receiving an activation instruction from the operator. At least one second indicator corresponding to a second instruction for directing a second aircraft behavior at least proximately the same as the first aircraft behavior is displayed, with the at least one second instruction to be automatically implemented at a future time. The at least one second indicator is at least approximately the same as the at least one first indicator. Indicators can be hierarchically organized to simplify presentation and reduce pilot training time.

Abstract: Methods and systems for handling aircraft control information are disclosed. A system in accordance with one embodiment of the invention includes a display medium coupleable to a flight manager, with the flight manager configured to receive and direct instructions for automatically controlling aircraft functions at a future time during flight of the aircraft. The system can further include a display controller coupled to the display medium to present at least one operator activatable element at the display medium and update information presented at the display medium when the operator activates the operator activatable element. For example, the operator activatable element can include an icon presented at a computer display screen, and can be activated by a keystroke.

Abstract: Methods and systems for displaying assistance messages to aircraft operators are disclosed. A method in accordance with one embodiment includes receiving an input from an aircraft operator at an aircraft flight deck, comparing a characteristic of the input to at least one target value for the characteristic, and, if the characteristic of the input differs from the at least one target value for the characteristic by at least a threshold amount, displaying an assistance message to the aircraft operator. The assistance message can include a complying input and/or an instruction for creating a complying input. The input and the assistance message can be displayed simultaneously.

Abstract: Methods and apparatuses for displaying and receiving tactical and strategic flight guidance information are disclosed. A method in accordance with one aspect of the invention includes displaying at least one first indicator to an operator of the aircraft, with a first indicator corresponding to a first instruction input by the operator for directing a first aircraft behavior and implemented upon receiving an activation instruction from the operator. At least one second indicator corresponding to a second instruction for directing a second aircraft behavior at least proximately the same as the first aircraft behavior is displayed, with the at least one second instruction to be automatically implemented at a future time. The at least one second indicator is at least approximately the same as the at least one first indicator. Indicators can be hierarchically organized to simplify presentation and reduce pilot training time.

Abstract: Methods and systems for handling aircraft control information are disclosed. A system in accordance with one embodiment of the invention includes a display medium coupleable to a flight manager, with the flight manager configured to receive and direct instructions for automatically controlling aircraft functions at a future time during flight of the aircraft. The system can further include a display controller coupled to the display medium to present at least one operator activatable element at the display medium and update information presented at the display medium when the operator activates the operator activatable element. For example, the operator activatable element can include an icon presented at a computer display screen, and can be activated by a keystroke.

Abstract: Methods and apparatuses for displaying and receiving tactical and strategic flight guidance information are disclosed. A method in accordance with one aspect of the invention includes displaying at least one first indicator to an operator of the aircraft, with a first indicator corresponding to a first instruction input by the operator for directing a first aircraft behavior and implemented upon receiving an activation instruction from the operator. At least one second indicator corresponding to a second instruction for directing a second aircraft behavior at least proximately the same as the first aircraft behavior is displayed, with the at least one second instruction to be automatically implemented at a future time. The at least one second indicator is at least approximately the same as the at least one first indicator. Indicators can be hierarchically organized to simplify presentation and reduce pilot training time.

Abstract: Methods and apparatuses for displaying and receiving tactical and strategic flight guidance information are disclosed. A method in accordance with one aspect of the invention includes displaying at least one first indicator to an operator of the aircraft, with a first indicator corresponding to a first instruction input by the operator for directing a first aircraft behavior and implemented upon receiving an activation instruction from the operator. At least one second indicator corresponding to a second instruction for directing a second aircraft behavior at least proximately the same as the first aircraft behavior is displayed, with the at least one second instruction to be automatically implemented at a future time. The at least one second indicator is at least approximately the same as the at least one first indicator. Indicators can be hierarchically organized to simplify presentation and reduce pilot training time.

Abstract: Apparatuses and methods for controlling autoflight systems are disclosed herein. An apparatus for use with an aircraft having an autoflight system can include an autoflight performance selector configured to limit the response of the autoflight system to flight guidance instructions in at least two of the pitch, roll and yaw axes. The autoflight performance selector has at least a first selection and a second selection different than the first selection. Selecting the first selection causes the response of the autoflight system to flight guidance instructions to not exceed a first level in the at least two axes, and selecting the second selection causes the response of the autoflight system to the flight guidance instructions to not exceed a second level in the at least two axes different than the first level.

Abstract: Apparatuses and methods for displaying autoflight information and controlling autoflight systems. In one embodiment, a flight deck for an aircraft having an autoflight system includes at least one pilot seat, at least one window positioned forward of the pilot seat, and a forward instrument panel positioned forward of the pilot seat. In one aspect of this embodiment, the forward window provides a forward field of view out of the aircraft for a pilot seated in the pilot seat. In another aspect of this embodiment, the flight deck further includes a display device configured to provide information related to one or more autoflight modes. The display device can be positioned at least approximately between the forward instrument panel and the forward window to provide the pilot with autoflight information at least proximate to the forward field of view. In a further aspect of this embodiment, the display device can be configured to provide information related to one or more target flight parameters.

Abstract: Methods and systems for airplane speed profile management are disclosed. A method and system in accordance to one embodiment of the disclosure includes a graphical display of speed segments and constraints as well as controls for managing the speeds and associated constraints. Speed Profile Management System (SPMS) provides an integrated and interactive speed profile management tool where pilots can view, update, or change the speed profile of their airplane's current or subsequent phases of flight.