Abstract: A method carried out in a user equipment, UE, (1) for generating location information to a location server (130) in a wireless network (100), the method comprising: receiving (404), from the location server, a location request message identifying a request for location information based on a UE-determined positioning method; obtaining (410) location information using a positioning method selected by the UE out of a plurality of available positioning methods, based on the location request message; transmitting (412) the location information to the location server.

Abstract: A method of operating a wireless communication device (90) includes monitoring for signals from a communications network (100, 101, 109) in a connected mode (301) of the wireless communication device (90) with a receive beam configuration (401). The method also includes storing the receive beam configuration (401) and monitoring for further signals (4003-4005) from the communications network (100, 101, 109) in a disconnected mode (302, 303) of the wireless communication device (90) with the stored receive beam configuration (401).

Abstract: Configuring a random access channel (RACH) procedure in a wireless communication network may include selecting one of plural RACH procedure configurations for a radio communication device to employ to initiate access with the wireless communication network and communicating the selected RACH procedure configuration to the radio communication device.

Abstract: Multi-rotor aerial vehicle (1, 1?, 1?, 1??, 1??, 1???, 1???) comprising, at least a first, second and third rotor 10, 20, 30, each rotatable by a dedicated first second and third hydraulic motor 11, 21, 31, a power unit 2, at least a first, second and third hydraulic pump 12, 22, 32 dedicated to the respective first, second and third hydraulic motor 11, 21, 31, wherein each hydraulic pump 12, 22, 32 is arranged to provide pressurized fluid to each hydraulic motor 11, 21, 31 for powering the hydraulic motor 11, 21, 31 and thereby rotating the respective rotor 10, 20, 30, a control unit 6 for controlling the operation of the multi-rotor aerial vehicle (1, 1?, 1?, 1??, 1??, 1???, 1???), wherein the control of the multi-rotor aerial vehicle (1, 1?, 1?, 1??, 1??, 1???, 1???) is arranged to be performed by altering the flow of pressurized fluid distributed to each respective hydraulic motor 11, 21, 31, wherein, wherein the flow of pressurized fluid provided to each hydraulic motor 11, 21, 31 is individually control

Abstract: Systems and methods are disclosed for rendering a surface in a synthetic scene using gutter space padding for texture atlases. Gutter space adjacent to UV shells may be padded with texels from the UV shells used for neighboring surfaces, rather than merely extending the interior texels. The result is that distracting artifacts, caused by mesh downsampling that produces sub-optimal polygon shapes and vertex placement may be mitigated. The resulting rendering, manifesting lessened artifacts, may appear to be less impacted by downsampling, and thus improve the experience for the viewer or other synthetics data consumer. The improvement may be used in rendering for human users and also training neural networks in computer vision tasks, such as object detection and recognition.

Abstract: Rotor flight vehicle includes a first rotor, a power unit, a transmission from the power unit to the first rotor, wherein said transmission comprises at least one belt, a group of rotational axes, at least one power output axle connected to the power unit and at least one rotor axle connected to said first rotor, the belt is applied to the power output axle, the power output axle is concentric with a rotational axis, the belt transmits power to the rotor axle, the rotor axle is concentric with a rotational axis, wherein consecutive rotational axes of the group of rotational axes extend in a relation to each other such that the angle between them is in the range of 80-100 degrees, wherein the belt has a maximal torsion of 80-100 degrees, in the belt's transition between two respective consecutive rotational axes of the group of rotational axes.

Abstract: Systems and methods are disclosed for rendering a surface in a synthetic scene using gutter space padding for texture atlases. Gutter space adjacent to UV shells may be padded with texels from the UV shells used for neighboring surfaces, rather than merely extending the interior texels. The result is that distracting artifacts, caused by mesh downsampling that produces sub-optimal polygon shapes and vertex placement may be mitigated. The resulting rendering, manifesting lessened artifacts, may appear to be less impacted by downsampling, and thus improve the experience for the viewer or other synthetics data consumer. The improvement may be used in rendering for human users and also training neural networks in computer vision tasks, such as object detection and recognition.

Abstract: A system for training a neural network generates a plurality of training meshes based on an input mesh. The plurality of training meshes include at least one mesh perceptually similar to the input mesh and one arbitrarily selected mesh perceptually dissimilar to the input mesh. The neural network is trained using the input mesh and the plurality of training meshes by tuning output of the neural network to identify similar non-identical meshes. The trained neural network is robust in identifying meshes similar to an unknown mesh input to the trained neural network.

Abstract: Multi-rotor aerial vehicle (1, 1?, 1?, 1??, 1??, 1???, 1???) comprising, at least a first, second and third rotor 10, 20, 30, each rotatable by a dedicated first second and third hydraulic motor 11, 21, 31, a power unit 2, at least a first, second and third hydraulic pump 12, 22, 32 dedicated to the respective first, second and third hydraulic motor 11, 21, 31, wherein each hydraulic pump 12, 22, 32 is arranged to provide pressurized fluid to each hydraulic motor 11, 21, 31 for powering the hydraulic motor 11, 21, 31 and thereby rotating the respective rotor 10, 20, 30, a control unit 6 for controlling the operation of the multi-rotor aerial vehicle (1, 1?, 1?, 1??, 1??, 1???, 1???), wherein the control of the multi-rotor aerial vehicle (1, 1?, 1?, 1??, 1??, 1???, 1???) is arranged to be performed by altering the flow of pressurized fluid distributed to each respective hydraulic motor 11, 21, 31, wherein, wherein the flow of pressurized fluid provided to each hydraulic motor 11, 21, 31 is individually control