This device (10) for assisting in the piloting of a vehicle, in particular an aircraft, comprises a display surface (16) for displaying images and a display management assembly for images intended to be displayed on the display surface (16) in superposition with a vision of an external landscape…
The system (1) has an inertial navigation center (3) for providing aircraft positional information partially from accelerometric and gyrometric measurements, and a satellite positioning module (5) to determine another aircraft positional information from satellite positioning data received by a…
The method involves defining a set of points i.e. beacon points, for a fall back route such that edges of Voronoi diagram associated with the set of beacon points separate polygons described by convex zones (ZN1-ZN6) of three-dimensional (3D) displacement zone (ZNd) in the plane. An identifier of…
The system (10) has a management unit (42) maintaining a zone (202) representative of the position of a runway contiguous to a centered zone. The unit is centered on the runway and a front zone (204). A peripheral zone extends partially around the centered zone and/or from the front zone. The…
The system (10) has a synthetic environment generating assembly (38) including a database (45B) with topographical information relative to a terrain. A display management assembly (42) controls display of relief lines (304) representative of the terrain on a region of a display (36), without…
The system (10) has an assembly (38) for dynamic generation of synthetic images. A management assembly (42) manages a graphical interface of a display (36), so as to control the display of the synthetic images on a region (60) of the display in certain configuration changes of an aircraft, and on…
The system (17) has an electrical network (20) to electrically power functional equipment (14A-14F) of an aircraft (10). A regulating assembly (24) includes a secondary electrical power source (58) formed by a fuel cell (70), and a conversion assembly (60) for additional electrical power injected…
The system (10) has an additional display unit (38) including additional display screens (40A, 40B), and an additional management unit (42) for managing graphical user interface (GUI) of the additional display screens for displaying a synthesis window on the additional screens depending on the…
The emergency electric power generation assembly (24) has an emergency electricity generator (60) connectible to the electric network (20) of an aircraft (10). The assembly is controllable between an inactive rest configuration in which the generator is inactive and an active configuration in which…