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.

A system, includes a memory in communication with a processor, the memory storing instructions that when executed by the processor cause the processor to receive a first location of a real vehicle, receive an updated location of the real vehicle, compute, utilizing at least the first location and the updated location, a future location of the real vehicle at a predetermined time in the future and output data to a display device adapted to display to a user of the display device at the predetermined time a mixed reality representation of an environment surrounding the real vehicle as viewed from the future location.

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.

This invention relates inter alia to a motion generator which comprises: an end effector; a stationary support having a base; at least one first tensile member, and at least six second tensile members, wherein each of the at least one first tensile member and the at least six second tensile members comprises a elastic element and each of which tensile members being attached at one end thereof to the end effector and being attached at the other end thereof to the stationary support; in which each tensile member applies a tensile force between the end effector and the stationary support, and in which each one of the at least six tensile members is independently adjustably tensioned by an actuator fixed to the stationary support which acts on the tensile member at a point along its length between the end effector and the elastic element, wherein the actuator acts to change the tension in the part of the tensile member between the end effector and the actuator in order to affect the forces and moments applied to the end effector by the system, wherein the actuator reacts the tensile force it applies to the tensile member against the stationary support, and wherein the tensile force applied by each tensile member to the end effector reacts against the tensile forces applied by the other tensile members via the end effector such that the end effector is maintained in suspension and out of contact with the stationary support by the tensile forces in the tensile members and any other forces applied to the end effector.

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.

A system, method, and device for generating a flight training scheme oriented to an individual difference are provided to resolve a problem that a differentiated training scheme applicable to a training state of a trainee cannot be generated quickly. The system includes a first apparatus configured to obtain identity information of a user; a second apparatus configured to store training data of the user; a third apparatus configured to read the corresponding training data of the user based on the identity information of the user, obtain a mastery degree of a training item of the user as well as an emotion class and rating of the user corresponding to the training item, configure the training item based on a training scenario, and generate an initial training scheme; and a fourth apparatus configured to configure a flight training simulation environment based on the initial training scheme.

A system for facilitating provisioning of a virtual experience is disclosed. The system may include a communication device configured for receiving at least one first sensor data from at least one first sensor of a first vehicle and at least one second sensor data from at least one second sensor of a second vehicle. Further, the communication device may be configured for transmitting at least one first presentation data to at least one first presentation device and at least one second presentation data to at least one second presentation device. Further, the at least one presentation device may be configured for presenting the at least one first presentation data and the at least one second presentation data. Further, the system may include a processing device configured for generating the at least one first presentation data and the at least one second presentation data.

An aircraft cockpit training simulator includes a plurality of aircraft cockpit simulation panels and power over Ethernet (POE) cabling extending therebetween. Each panel includes a simulator user interface device, an input circuit or an output circuit, a POE interface circuit, and a distributed controller coupled to the input circuit or output circuit and POE interface device and asynchronously communicating with other controllers using a publish/subscribe protocol. A host controller is coupled to the distributed controllers via the POE cabling and operates the aircraft cockpit simulation panels using a host computer model. The distributed controllers may operate independent of the host computer model.

An aircraft cockpit training simulator includes a plurality of aircraft cockpit simulation panels and power over Ethernet (POE) cabling extending therebetween. Each panel includes a simulator user interface device, an input circuit or an output circuit, a POE interface circuit, and a distributed controller coupled to the input circuit or output circuit and POE interface device and asynchronously communicating with other controllers using a publish/subscribe protocol. A host controller is coupled to the distributed controllers via the POE cabling and operates the aircraft cockpit simulation panels using a host computer model. The distributed controllers may operate independent of the host computer model.