Abstract: Systems and methods are provided for detecting and warning of aircraft rollover conditions. The systems include one or more sensors onboard the aircraft and a controller onboard the aircraft that is in operable communication with the one or more sensors. The controller is configured to, by one or more processors: receive input data from the one or more sensors and, optionally, one or more other sources, process the input data to dynamically determine a roll angle of the aircraft, an angular roll rate of the aircraft, and a critical rollover angle of the aircraft, determine whether current or potential static or dynamic rollover conditions of the aircraft exist based, at least in part, on the roll angle, the angular roll rate, and the critical rollover angle, and generate an alert in response to determining that the current or potential static or dynamic rollover conditions exist.

Abstract: Systems and methods are provided for detecting and warning of aircraft rollover conditions. The systems include one or more sensors onboard the aircraft and a controller onboard the aircraft that is in operable communication with the one or more sensors. The controller is configured to, by one or more processors: receive input data from the one or more sensors and, optionally, one or more other sources, process the input data to dynamically determine a roll angle of the aircraft, an angular roll rate of the aircraft, and a critical rollover angle of the aircraft, determine whether current or potential static or dynamic rollover conditions of the aircraft exist based, at least in part, on the roll angle, the angular roll rate, and the critical rollover angle, and generate an alert in response to determining that the current or potential static or dynamic rollover conditions exist.

Abstract: A Modular Reconfigurable Simulator is provided. The Modular Reconfigurable Simulator may include at least one Core Module with at least one Instrumental Module, including Computing Unit and Virtual or Mixed Reality headset. The Modular Reconfigurable Simulator may be reconfigured into multiple different aircraft by the user without needing additional technical assistance from a third party while emulating aircraft ergonomics and automatically binding controller functions with Image Generators virtual aircraft model.

Abstract: A virtual or augmented reality device is provided. The virtual or augmented reality device may include at least one visualization device and at least one computer that may be communicatively linked. The external computer may further include a central processing unit and a video adaptor. The video adaptor may supply multiple data stream to the visualization device. The virtual or augmented reality device may also include at least two displays that may be connected to the visualization device.

Abstract: A virtual or augmented reality device is provided. The virtual or augmented reality device may include at least one visualization device and at least one computer that may be communicatively linked. The external computer may further include a central processing unit and a video adaptor. The video adaptor may supply multiple data stream to the visualization device. The virtual or augmented reality device may also include at least two displays that may be connected to the visualization device.