A flight-capable imaging system includes a set of parallel rails, a power source mounted to the set of parallel rails, an imaging device mounted to the set of parallel rails, an aerial vehicle body mounted to the set of parallel rails, a set of aerial vehicle arms attached to the aerial vehicle body that each include a set of propellers and a motor configured to turn the set of propellers to enable flight of the flight-capable imaging system, and at least one processing module configured to control the flight of the of the flight-capable imaging system based on controlling a motor speed of the motor of each of the set of aerial vehicle arms.

A system for remote pilot control of an electric aircraft in autopilot mode including a remote computing device configured to receive a user input and generate a control datum as a function of the pilot input, a flight controller configured to receive the control datum from the remote computing device, and generate a command datum as a function of the control datum and an authority status, and the remote computing device configured to receive the command datum from the flight controller, and display the command datum.

A system for remote pilot control of an electric aircraft in autopilot mode including a remote computing device configured to receive a user input and generate a control datum as a function of the pilot input, a flight controller configured to receive the control datum from the remote computing device, and generate a command datum as a function of the control datum and an authority status, and the remote computing device configured to receive the command datum from the flight controller, and display the command datum.

An autonomous unmanned aerial vehicle for land, sea and air use. The autonomous unmanned aerial vehicle is more specifically related to an unmanned aerial vehicle, wherein the autonomous unmanned aerial vehicle is configured to vertically take off and vertically land, fly with fixed wings and stay in the air silently for a long time by means of a balloon inflated behind it.

An autonomous unmanned aerial vehicle for land, sea and air use. The autonomous unmanned aerial vehicle is more specifically related to an unmanned aerial vehicle, wherein the autonomous unmanned aerial vehicle is configured to vertically take off and vertically land, fly with fixed wings and stay in the air silently for a long time by means of a balloon inflated behind it.

A pendant assembly for a rescue hoist may comprise a pendant, an interface box discrete from the pendant, and a display screen discrete from the pendant. The pendant may include a hoist input. The interface box may be configured to receive a control input from the pendant. The display screen may be configured to receive a display command from the interface box.

A pendant assembly for a rescue hoist may comprise a pendant, an interface box discrete from the pendant, and a display screen discrete from the pendant. The pendant may include a hoist input. The interface box may be configured to receive a control input from the pendant. The display screen may be configured to receive a display command from the interface box.

A wireless aircraft cabin control panel is disclosed. In embodiments, the wireless aircraft cabin control panel includes a user interface device disposed on a first surface of a bulkhead of an aircraft cabin. In embodiments, the user interface includes a display device, a user input device, wireless communication circuitry, and a controller. The controller may be configured to: generate control signals configured to cause the wireless communication circuitry to transmit wireless control signals to wireless communication circuitry of a control unit disposed on a second surface of the bulkhead; receive power via wireless charging signals received from the wireless communication circuitry of the control unit; distribute power from the wireless charging signals to the display device; extract data signals encoded within the wireless charging signals; and cause the display device to display at least one of an indicator or an image in response to the extracted data signals.

A wireless aircraft cabin control panel is disclosed. In embodiments, the wireless aircraft cabin control panel includes a user interface device disposed on a first surface of a bulkhead of an aircraft cabin. In embodiments, the user interface includes a display device, a user input device, wireless communication circuitry, and a controller. The controller may be configured to: generate control signals configured to cause the wireless communication circuitry to transmit wireless control signals to wireless communication circuitry of a control unit disposed on a second surface of the bulkhead; receive power via wireless charging signals received from the wireless communication circuitry of the control unit; distribute power from the wireless charging signals to the display device; extract data signals encoded within the wireless charging signals; and cause the display device to display at least one of an indicator or an image in response to the extracted data signals.

An electronic control device of an avionics system for implementation of a critical avionics function, comprising: a module for receiving a voice instruction signal; a speech recognition module configured to transform the voice signal into a textual transcript; a processing module configured to associate the textual transcript with at least one action to be performed; a monitoring system comprising: a control module configured to check whether the textual transcript and/or the action to be performed is consistent if and only if: a) the textual transcript and/or the action to be performed is consistent with the expected syntax, b) the textual transcript and/or the action to be performed is consistent with the expected lexical field, and c) the textual transcript and/or the action to be performed is consistent with the current context, a module for generating an associated command only if no inconsistencies are detected.