Debriefing a session from a user in a system. During the session, while the user performs actions on one or more tangible instruments of the system, dynamic data is logged in relation to the system along a session timeline. The dynamic data covers the actions of the user on tangible instrument(s). A graphical user interface depicting a debriefing scene, related to the session, is displayed from a first point of view starting at a first time within the session timeline. The debriefing scene is generated starting at the first time from at least a first image feed. Upon detection of a predetermined event in the dynamic data at a second time along the session timeline, a second point of view different from the first point of view is defined and the debriefing scene is generated therefrom after the second time using at least a second image feed.

A method for assisting a trainee during a pilot training on a pilot training simulator, comprising receiving a vocal input message from the trainee; converting the vocal input message into a text input message; processing the text input message by a neural network configured as a large language model, LLM, to identify the content of the text input message and extract at least a request related to the pilot training simulator; accessing and searching a database based on the request to determine an educational advice using the neural network, wherein the database includes data about an aircraft on which the pilot training is performed; generating a response message containing the educational advice using the neural network; converting the response message into a vocal response message; and providing the vocal response message to the trainee.

A vestibular stimulation system, computer controls, methods, and doses are provided.

The invention relates to a method for providing predefined desired drive characteristics (38, 50) in an aircraft, characterized by the following steps: driving a thrust generation element of the aircraft by means of an electric motor that has actual drive characteristics (34) which include at least some of the desired drive characteristics (38, 50) but are also partly different therefrom; andhaving a control device adjust operating points of the electric motor exclusively according to the desired drive characteristics (38, 50).

The invention relates to a method for providing predefined desired drive characteristics (38, 50) in an aircraft, characterized by the following steps: driving a thrust generation element of the aircraft by means of an electric motor that has actual drive characteristics (34) which include at least some of the desired drive characteristics (38, 50) but are also partly different therefrom; andhaving a control device adjust operating points of the electric motor exclusively according to the desired drive characteristics (38, 50).

Disclosed is a flight simulation apparatus. According to the flight simulation apparatus of the present disclosure, first left and right rails and second left and right rails slide along a pair of first front and rear rails and a pair of second front and rear rails so that first and second seats can freely move forward and rearward, first and second auxiliary rails are formed to position the first and second seats at various locations in the front-rear direction, and the first and second seats can be stably supported by first and second sliders.

Disclosed is a flight simulation apparatus. According to the flight simulation apparatus of the present disclosure, first left and right rails and second left and right rails slide along a pair of first front and rear rails and a pair of second front and rear rails so that first and second seats can freely move forward and rearward, first and second auxiliary rails are formed to position the first and second seats at various locations in the front-rear direction, and the first and second seats can be stably supported by first and second sliders.

The present invention provides a system for training a subject to recognize the onset of hypoxia, the system including (i) a flight simulation system, and (ii) a hypoxia induction system, wherein the flight simulation system is operably linked to the hypoxia induction system. The system provides a tool for pilot training to a pilot, allowing for the delivery of standardized training programs where the tasks required for the operation of an aircraft are able to be coordinated with an induction of hypoxia in the subject. Such a system is also able to provide an assessment tool to demonstrate when a pilot has had sufficient training in recognizing the effects of hypoxia.

The present invention provides a system for training a subject to recognize the onset of hypoxia, the system including (i) a flight simulation system, and (ii) a hypoxia induction system, wherein the flight simulation system is operably linked to the hypoxia induction system. The system provides a tool for pilot training to a pilot, allowing for the delivery of standardized training programs where the tasks required for the operation of an aircraft are able to be coordinated with an induction of hypoxia in the subject. Such a system is also able to provide an assessment tool to demonstrate when a pilot has had sufficient training in recognizing the effects of hypoxia.

A device for pilot training includes a memory, an interface, and one or more processors. The memory is configured to store at least one computational model of at least one human sensory system. The interface is configured to receive sensor data and aircraft state data from a flight simulator. The sensor data includes pilot activity data and motion data. The motion data is indicative of detected motion of a simulated aircraft of the flight simulator. The processor(s) are configured to process the motion data and the pilot activity data based on the at least one computational model to predict a pilot estimated aircraft state. The processor(s) are configured to determine an estimated error based on a comparison of the pilot estimated aircraft state and a detected aircraft state. The aircraft state data indicates the detected aircraft state. The processor(s) are configured to provide the estimated error to a second device.