This system comprises a drone and a remote station with virtual reality glasses rendering images transmitted from the drone, and provided with means for detecting changes of orientation of the user's head. The drone generates a “viewpoint” image (P′1) and a “bird's eye” image (P′2) whose field is wider and whose definition is lower. When the sight axis of the “viewpoint” image is modified in response to changes of position of the user's head, the station generates locally during the movement of the user's head a combination of the current “viewpoint” and “bird's eye” images, with outlines (CO′) adjusted as a function of the changes of position detected by the detection means.

The system comprises a drone and a ground station with a console adapted to be directed towards the drone, and virtual reality glasses rendering images taken by a camera of the drone. The system further comprises means for modifying the framing of the images taken by the camera as a function of framing instructions received from the ground station. It further comprises relative heading determination means (302-324) for periodically elaborating an angular difference between the orientation of the glasses and the orientation of the console, and means (316) for elaborating framing instructions for the drone as a function said angular difference. The sudden changes of framing when the user simply turns the console and his whole body, head included, towards the drone to follow it in its displacements, are hence avoided.

This disclosure is generally directed to an Unmanned Aerial Device (UAV) that uses a removable computing device for command and control. The UAV may include an airframe with rotors and an adjustable cradle to attach a computing device. The computing device, such as a smart phone, tablet, MP3 player, or the like, may provide the necessary avionics and computing equipment to control the UAV autonomously. For example, the adjustable cradle may be extended to fit a tablet or other large computing device, or retracted to fit a smart phone or other small computing device. Thus, the adjustable cradle may provide for the attachment and use of a plurality of different computing devices in conjunction with a single airframe. Additionally the UAV may comprise adjustable arms to assist in balancing the load of the different computing devices and/or additional equipment attached to the airframe.

A flying disc includes a hub composed of polymeric material, a ring composed of polymeric material and coupled to the hub. The hub and the ring may have different specific gravities by being composed of different materials or by having a weighting product embedded therein, or a weighting product may be carried between the hub and the ring.

The present invention relates to a powered, flight capable, air-filled balloon which mimics the movement of a helium-filled balloon.

A self-righting aeronautical vehicle comprising a hollowed frame and a lift mechanism. The exterior of the frame and center of gravity are adapted to self-right the vehicle. The frame can include sealed, hollowed sections for use in bodies of water. The frame can be spherical in shape enabling inspection of internal surface of partially or fully enclosed structures. Inspection equipment can be integrated into the vehicle and acquired data can be stored or wirelessly communicated to a server. A controlled or other mass can be pivotally assembled to a pivot axle spanning across the interior of the frame. The pivot axis can rotate about a vertical axis (an axis perpendicular to the elongated axis). The propulsion mechanisms can be adapted for use as a terrestrial vehicle when enclosed in a sealed spherical shell.

An automated mobile vehicle configured to autonomously provide coverage for inoperable infrastructure components at various locations. In accordance with disclosed embodiments, a plurality of automated mobile vehicles are deployed to provide emergency lighting, a wireless network, audio, video, etc., at an indoor and/or outdoor event area.

An angle detecting device includes a rotatably supported magnet, and a magnetic sensor disposed opposite to the magnet. An output of the magnetic sensor is changed based on a magnetic flux change due to a rotation of the magnet. The magnet is disposed such that a distance between the magnetic sensor and the magnet is changed by the rotation of the magnet.

A method for beautifying a balsa wood model aircraft with a thermal shrink covering film, so that the balsa wood model aircraft with a thermal shrink covering film is obtained. This method makes a model aircraft colorful, reduces labor costs, improves the beautifying and painting effect of the model aircraft, and also improves the pneumatic performance of the model aircraft.

A gyrating disc is disclosed having a circular and flat shape with an edge extending perpendicularly around its circumference. The gyrating disc has a weight on the interior or exterior of the edge, or between the center and the edge. When the gyrating disc is launched in a clockwise or counterclockwise manner, the disc achieves a gyrating flight, moving on its horizontal plane and stable at the vertical axis established in the center of the disc.