A system for modular mobile flight simulator for an electric aircraft is presented. The system includes a simulator module include a concave display, a plurality of projection devices, a pilot interface, wherein the pilot includes a primary flight display and at least a pilot control communicatively connected to a sensor configured to detect a plurality of measure pilot data and generate a pilot datum. The system further includes a computing device configured to receive the pilot datum from the sensor, simulate an aircraft model of the electric aircraft as a function of the pilot datum, blend a plurality of images to be projected by the plurality of projection devices into a distinct image, display the distinct image onto the concave display, generate a feedback, and perform a physical feedback on the simulator module.

Aspects relate to augmented reality (AR) methods and systems for simulated operation of an electric vertical take-off and landing (eVTOL) aircraft. An exemplary AR system includes at least an aircraft component of an eVTOL aircraft, a computing device configured to operate a flight simulator to simulate flight in an environment and simulate at least a virtual representation interactive with the flight simulator, where the at least a virtual representation includes an aircraft digital twin of the at least an aircraft component, and a mesh network configured to communicatively connect the at least an aircraft component and the computing device and communicate encrypted data.

Aspects relate to augmented reality (AR) methods and systems for simulated operation of an electric vertical take-off and landing (eVTOL) aircraft. An exemplary AR system includes at least an aircraft component of an eVTOL aircraft, a computing device configured to operate a flight simulator to simulate flight in an environment and simulate at least a virtual representation interactive with the flight simulator, where the at least a virtual representation includes an aircraft digital twin of the at least an aircraft component, and a mesh network configured to communicatively connect the at least an aircraft component and the computing device and communicate encrypted data.

The instant application pertains to a mobile aircraft training system comprising a user interface and a virtual flight deck display operably configured to the user interface. A processor is operably linked to the user interface and the virtual flight deck display. The virtual flight deck display is configured to display a three dimensional representation of an aircraft's controls and indicators from a perspective of an aircraft crew member position. The use interface is configured to identify an interaction between a user and the aircraft's controls and indicators in the three dimensional representation and configured to communicate said interaction to the processor. The three dimensional representation is altered based upon said interaction. The processor is configured to provide audio and video feedback to the user via the virtual flight deck display based upon the identified interaction between the user and the aircraft's controls and indicators in the three dimensional representation.

Systems and methods for providing immersive avionics training include controlling a virtual or augmented reality device to present, to a user, a virtual or augmented reality simulation of a user interface of an avionics system including a simulation of a display of the avionics system. The method further includes detecting a user action based on a point of gaze and touch inputs of the user indicative of a user command to use a functionality of the avionics system. The user action is a physical interaction with a control panel apparatus representing an input device of the user interface of the avionics system. The method also includes simulating the use of the functionality in accordance with the user command to generate output data and controlling the virtual or augmented reality device to simulate display of the output data in the simulation of the display of the avionics system.

A crane, a construction machine or an industrial truck, with a control station including at least one input means for inputting control commands, a graphical simulation module for calculating a virtual representation of the machine surroundings and/or machine components visible from the control station, such as a boom or a load hook, and a display device for displaying the calculated virtual representation, wherein a movement simulation module is provided for determining movements and/or deformations of the machine components according to the inputted control commands, depending on which the graphical simulation module calculates the virtual representation. Proposed is a data emulation using hardware components, which carry out actual actuating movements and thus simulate “actual” actuating movements of the machine to be simulated, in order to provide corresponding movement data more rapidly and with less computing performance, whereby a more realistic simulation can be achieved in real-time or almost real-time.

A method and system for simulating pilot controls in a cockpit simulator by controlling one or more arms on which is/are mounted a control grip, pedal or the like, to locate the grip at different positions and allow movement of the grip in a plurality of movement directions and trajectories while allowing varying force feedback.

A method is present for presenting a flight deck. A model of the flight deck is identified having a number of locations for a number of displays. Aircraft data is obtained. A number of panels is generated from the aircraft data. A display of the flight deck is generated containing the number of panels in the number of locations to form a presentation of the flight deck.

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 jet aircraft maneuvering characteristic simulation system for a single propeller aircraft includes a power lever, speed brakes, and a controller. The power lever is configured to change a thrust of the single propeller aircraft. The speed brakes are provided on respective right and left sides of the single propeller aircraft. The controller is configured to, in response to an operation of the power lever to raise the thrust of the single propeller aircraft, deploy both the right and the left speed brakes to cause an increase in speed of the single propeller aircraft to be moderate, and control the speed brakes to cause a force in a yaw direction and a force in a roll direction to be generated that act against a turning tendency of the single propeller aircraft by making amounts of the deployment of the right and the left speed brakes different from each other.