The present invention includes a device for hypoxia training comprising: one or more electrochemical cells each comprising: a cathode and an anode separated by a proton exchange membrane, each of the anode and cathode in communication with an input and an output, wherein the input of the cathode is in fluid communication with ambient air, and wherein the input of the anode is in fluid communication with a source of liquid water; a power supply connected to the one or more electrochemical cells; and a mask in fluid communication with the output from the cathode of the one or more electrochemical cells, wherein oxygen is removed from the ambient air during contact with the cathode when hydrogen ions separated from liquid water by a catalyst on the anode convert oxygen in the ambient air into water.

A water rollover simulation system includes a simulation training device. The simulation training device is connected to a track, wherein one end of the track is submerged in water. The simulation training device begins a simulation on another portion of the track not submerged in water, moves toward the end of the track, and completes the simulation by allowing one or more trainees to escape the simulation training device while the simulation training device is submerged under water. The water rollover simulation system includes various safety features. The safety features can be activated automatically after a predetermined amount of time, or manually via a remote control system.

A mobile aircraft simulation tool that includes a simulated aircraft body extending between a front end and rear end along a central axis X and having a length of between 10 and 60 feet. The simulated aircraft body includes a plurality of windows, one or more doors, an internal cavity, and a passenger cabin within the internal cavity having a plurality of seats.

In an aspect of the present disclosure is a system for simulating an electrical vertical takeoff and landing (eVTOL) aircraft, including a fuselage comprising one or more pilot inputs, each of the pilot inputs configured to detect pilot datum; a concave screen facing the fuselage; a plurality of projectors directed at the concave screen; a computing device communicatively connected to the plurality of projectors, the computing device configured to: receive the pilot datum detected by the pilot inputs; generate a simulated eVTOL flight maneuver as a function of the pilot datum; and command the plurality of projectors to display one or more images based on the simulated flight maneuver.

The present invention includes a device for hypoxia training comprising: one or more electrochemical cells each comprising: a cathode and an anode separated by a proton exchange membrane, each of the anode and cathode in communication with an input and an output, wherein the input of the cathode is in fluid communication with ambient air, and wherein the input of the anode is in fluid communication with a source of liquid water; a power supply connected to the one or more electrochemical cells; and a mask in fluid communication with the output from the cathode of the one or more electrochemical cells, wherein oxygen is removed from the ambient air during contact with the cathode when hydrogen ions separated from liquid water by a catalyst on the anode convert oxygen in the ambient air into water.

Systems and methods include providing a virtual reality (“VR”) flight emulator system that simulates control, operation, and response of a vehicle. The flight emulator includes a control interface and a head-mounted display worn by a user. Motion, orientation, and/or forces experienced by the simulated vehicle are imparted to a user through a motion-control seat. Multiple flight emulators can be connected to a communication network, and a master flight emulator may teleport into a slave flight emulator in order to observe, overtake, override, and/or assume control of the slave flight emulator. Inputs made via the control interface of the master flight emulator or during playback of a pre-recorded training exercise or flight mission are translated into the control interface, head-mounted display, and motion-control seat of the slave flight emulator to provide real-time feedback to the user of the slave flight emulator.

A system and method for a mobile flight simulator of an electric aircraft is illustrated. The first simulator housing instrument is configured to house a plurality of first flight simulator components. The second simulator housing instrument is configured to house a plurality of second flight simulator components. The pilot control is configured to receive a pilot command and transmit the pilot command to a computing device. The computing device is configured to communicatively connect each first flight simulator component of the plurality of flight simulator components and each second flight simulator component of the plurality of flight simulator components, generate a mobile flight simulation as a function of the pilot command, the mobile flight simulation including an electric aircraft model, and update the electric aircraft model as a function of the pilot command, the mobile flight simulation and a feedback datum.

In an aspect of the present disclosure is a system for simulating an electrical vertical takeoff and landing (eVTOL) aircraft, including a fuselage 104 comprising one or more pilot inputs, each of the pilot inputs configured to detect pilot datum; a concave screen facing the fuselage 104; a plurality of projectors directed at the concave screen; a computing device communicatively connected to the plurality of projectors, the computing device configured to: receive the pilot datum detected by the pilot inputs; generate a simulated eVTOL flight maneuver as a function of the pilot datum; and command the plurality of projectors to display one or more images based on the simulated flight maneuver.

A system and method for a mobile flight simulator of an electric aircraft is illustrated. The first simulator housing instrument is configured to house a plurality of first flight simulator components. The second simulator housing instrument is configured to house a plurality of second flight simulator components. The pilot control is configured to receive a pilot command and transmit the pilot command to a computing device. The computing device is configured to communicatively connect each first flight simulator component of the plurality of flight simulator components and each second flight simulator component of the plurality of flight simulator components, generate a mobile flight simulation as a function of the pilot command, the mobile flight simulation including an electric aircraft model, and update the electric aircraft model as a function of the pilot command, the mobile flight simulation and a feedback datum.

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.