A system for displaying information relative to an aircraft flight and related method are provided. This system comprises a display device, and a module for managing the display on the display device, the management module being configured for controlling the display, on a window of the display device, of a timescale representative of a time period of the flight, and for controlling the display, facing the timescale, of pieces of information relative to a series of events intended to occur in a time window comprised in the time period. The module for managing the display is configured for determining a position in time of the time window comprised in the time period and a duration of the time window, and for controlling the display, along the timescale, of a marker representative of the position in time and of the duration of the time window.

A device receives a request for a mission that includes traversal of a flight path from one or more first locations to a second location and performance of mission operations, and determines required capabilities and constraints for the mission based on the request. The device identifies UAVs based on the required capabilities and the constraints, and calculates a cost effective mission plan, for the identified UAVs, based on the required capabilities and the constraints. The device generates mission plan instructions, for the cost effective mission plan, that include flight path instructions for the flight path and mission instructions for the mission operations. The device provides the mission plan instructions to the identified UAVs to permit the identified UAVs to travel from the one or more first locations to the second location, via the flight path, and to perform the mission operations.

A common operating environment (COE) display system for vehicle operations, such as for air transport provides coordination of logistics information with dispatch or a controller. An operational plan, such as a flight plan or other operational plan describing vehicle deployment is stored, and a map visualization system displays a map region. An in-vehicle display depicts the operational plan, providing displays of current and projected operational conditions of the vehicle within different time phases of the operational plan. Transfer of updates of the operational plan is performed without replacing substantial portions of the stored data for the operational plan, allowing synchronization of the operational plan with a remotely located facility. The system permits a controller or dispatcher to screen share the in-vehicle display based on information previously stored, as updated by the updates, and permits review of the modified operational plan.

Systems, methods and computer-storage media are provided for enhancing awareness in an aircraft using a touch-screen instrument panel. In one aspect, a warning is displayed peripherally in the panel in a way that attracts attention without interfering with the use of the panel for other purposes. In another aspect, a crew member is directed by highlighting through menus to a screen that enables the problem causing the warning to be corrected. In another aspect, parameters (e.g., temperatures, pressures) are displayed along with oriented graphical representations of system components. In yet another aspect, aircraft parameters are displayed in a historical context so that the user has a time-line context for a value at issue.

A method for the three-dimensional representation of the trajectory of an aircraft in flight implemented in a navigation system of an aircraft is provided. The flight plan of the aircraft comprises imposed georeferenced trajectories and predicted non-georeferenced trajectories. When the trajectory of the aircraft is dependent on a non-georeferenced flight setpoint, the three-dimensional representation method is an iterative process comprising the following steps: computing a predicted trajectory arising from at least one computed trajectory extending over a determined distance or duration; computing a smoothed trajectory from the predicted trajectory in order to obtain a resulting trajectory; computing a displayed trajectory, the trajectory being equal to the resulting trajectory corrected for constant deviations or deviations depending on the application of setpoints from the flight director; and displaying the displayed trajectory.

Systems and methods are provided for displaying roll rate on a vertical take-off and landing (VTOL) aircraft display. Aircraft roll data is received from at least one geospatial sensor of the VTOL aircraft. A roll rate scale associated with a desirable roll rate range of the VTOL aircraft is generated. An aircraft roll rate of the VTOL aircraft is determined based on the aircraft roll data. The VTOL aircraft display, including a graphical representation of the roll rate scale and the aircraft roll rate with respect to the roll rate scale, is generated for display on the display device.

A method (20) for calculating lateral avoidance trajectories for an aircraft (11). The method includes: obtaining data indicative of current aircraft position, current track, current roll, current airspeed, current vertical speed, current altitude, and maximum achievable roll of the aircraft; calculating a current trajectory of the aircraft; and calculating a left trajectory and right trajectory of the aircraft corresponding to the aircraft turning left/right at the maximum achievable roll from the current aircraft position. The method also includes obtaining local terrain elevation grid data; determining intersections between the local terrain elevation grid, and each of the current trajectory, left trajectory, and right trajectory; and providing an indication, of any intersections between the local terrain elevation grid, and each of the trajectories.

A system includes one or more control units configured to determine one or more fuel consumption models for an aircraft. A method includes determining, by one or more control units, one or more fuel consumption models for an aircraft. A non-transitory computer-readable storage medium comprising executable instructions that, in response to execution, cause one or more control units comprising a processor, to perform operations including determining one or more fuel consumption models for an aircraft.

A method for processing data generated by an event management device determining mission adaptation suggestions from current or future mission data sources, the method comprising the following steps of: receiving at least one suggestion comprising an item of information and a datum related to its construction; generating a notification for each received suggestion; storing the notification in a notifications memory. The method further comprises at least one iteration of the following steps: applying a classification operation to the notification; applying processing to the notification as a function of the classification operation, the processing comprising a step of rendering the notification on a Human-Machine interface in response to a display condition, the rendering using a display form and display dynamics.

A system and corresponding method are presented. The system comprising a primary radar system comprising one or more phased array antenna systems, a sensor arrangement, and a control system. The sensor arrangement comprises one or more sensors configured for collecting sensing data indicative of presence and location of one or more unmanned aerial vehicles (UAV's) within a predetermined region, and to provide said sensing data to the control system. The control system comprises at least one processor configured for processing the sensing data, determining a need to deactivate score for the one or more UAV's, and generating operational instructions to the primary radar system for generating deactivation beam directed toward location of said one or more UAV's, thereby deactivating said one or more UAV's.