A flying training support system includes: a flight condition generator that generates a simulated flight condition of a virtual another aircraft; a relative position derivation unit that derives a relative position of the virtual other aircraft based on the simulated flight condition and a real flight condition of the own aircraft; a display controller that displays an indicator indicating the virtual other aircraft at the relative position of the virtual other aircraft on a transmission display; a variation amount derivation unit that derives a simulated variation amount by which the own aircraft would vary due to flight of the virtual other aircraft, based on the simulated flight condition and the relative position of the virtual other aircraft; and a flight controller that actually varies the own aircraft so as to make the own aircraft in a state where the own aircraft varies by the simulated variation amount.

A method for creating a modified flight simulation program for a flight simulation system includes: obtaining a demonstration flight record associated with a preset track route of a virtual airplane; generating an add-on content pack for the flight simulation program based on the demonstration flight record; and merging the add-on content pack to the flight simulation program to create a modified flight simulation program. The generation of the add-on content pack includes: mapping the preset track route to geographical coordinate data in the real world, creating a first program module associated with a demonstration mode enabling a demonstration virtual flight along the preset track route, creating a second program module associated with an assisted flight mode enabling user control for a virtual flight within a free-flight space, and creating the add-on content pack that includes the first and the second program modules.

An interactive computer simulation system includes one or more processors for performing an interactive computer simulation in an interactive simulated environment based on user input and for generating images related to the interactive computer simulation. The system includes a dome for displaying the images, the dome being cut by a base below an equatorial plane of the dome, the images being displayed on the dome at a general-projection distance. The system further includes an adjusted-projection panel having an adjusted-projection surface defining an adjusted-projection distance smaller than the general-projection distance for addressing a vergence-accommodation conflict when simulated ground images are displayed.

Method and system for visualizing dynamic virtual sub-systems of a virtual simulated element in an interactive computer simulation system comprising a computer generated environment. One or more tangible instruments control the virtual simulated element in the computer generated environment. A graphical user interface comprising an interactive display portion depicting a rendered view of the virtual simulated element. While an interactive computer simulation of the virtual simulated element is performed in the interactive computer simulation system, a storage system logs dynamic data in relation to the dynamic virtual sub-systems. At least one of the dynamic virtual sub-systems of the virtual simulated element is selected and a subset of dynamic data related to the selected virtual sub-system is loaded from the storage system. The selected virtual sub-system is displayed together with the related dynamic data on the graphical user interface.

A system for flight simulation of an electric aircraft. The system includes a pilot control. The pilot control is configured to receive an input from a user. The system includes a pilot command that is generated by the pilot control. The system includes a computing device configured to generate a simulation. The simulation includes an electric aircraft model. The electric aircraft model is configured to simulate a performance of an electric aircraft. The performance is determined by at least the pilot command. The simulation is configured to provide feedback to the user based on the performance of the electric aircraft. The simulation is further configured to updated the electric aircraft model as a function of the pilot command.

An interactive computer simulation system includes one or more processors for performing an interactive computer simulation in an interactive simulated environment based on user input and for generating images related to the interactive computer simulation. The system includes a dome for displaying the images, the dome being cut by a base below an equatorial plane of the dome, the images being displayed on the dome at a general-projection distance. The system further includes an adjusted-projection panel having an adjusted-projection surface defining an adjusted-projection distance smaller than the general-projection distance for addressing a vergence-accommodation conflict when simulated ground images are displayed.

An avionics lower level device (LLD) simulator may include at least one touchscreen display device. The at least one touchscreen display device may include a display stack assembly including at least one touchscreen sensor and a display and at least one advanced haptic feedback component positioned proximate to the display stack assembly. The at least one touchscreen display device may be configured to display at least one GUI or GUI icon, the at least one GUI or GUI icon related to an operation of an aircraft, may be configured to provide at least one advanced haptic feedback response following an interaction with the at least one GUI or GUI icon displayed on the at least one touchscreen display device, and may be configured to mimic a physical response observed following an operation of a mechanical component installed within a cockpit of the aircraft.

An avionics lower level device (LLD) simulator may include at least one touchscreen display device. The at least one touchscreen display device may include a display stack assembly including at least one touchscreen sensor and a display and at least one advanced haptic feedback component positioned proximate to the display stack assembly. The at least one touchscreen display device may be configured to display at least one GUI or GUI icon, the at least one GUI or GUI icon related to an operation of an aircraft, may be configured to provide at least one advanced haptic feedback response following an interaction with the at least one GUI or GUI icon displayed on the at least one touchscreen display device, and may be configured to mimic a physical response observed following an operation of a mechanical component installed within a cockpit of the aircraft.

The present disclosure relates to a method (300) for displaying a perspective view of the surrounding of an aircraft (100) in an aircraft. The method comprises accessing (310) surrounding information from a database. The surrounding information is photo-based and three-dimensional. The method further comprises processing (320) the accessed surrounding information so that a perspective view of the surrounding of the aircraft is provided. The perspective view of the surrounding correlates to the position of the aircraft and is photo-based with spatially correlated photo-based textures. The method further comprises transmitting (360) the provided perspective view of the surrounding of the aircraft to a displaying unit so that it can be displayed in the aircraft. The present disclosure also relates to a system, an aircraft, a use, a computer program, and a computer program product.

A method for providing remote visibility into a simulation environment, comprising: establishing over a secure public network a connection between a first videoconferencing client running on a first computer and a second videoconferencing client running on a second computer; receiving at the first computer a first live camera feed encompassing a first portion of the simulation environment over a secure private network, the second computer being located outside of the secure private network; displaying within a viewer the first live camera feed and a simulation control interface, a representation of a second portion of the simulation environment and/or a second live camera feed encompassing a third portion of the simulation environment; and granting the second videoconferencing client visual access to the viewer application through the first videoconferencing client.