Abstract: A system comprises: a sensor configured to detect a gesture relating to a vehicle; a network; an electronic control unit (ECU) coupled to the network, a display device, and the sensor, the ECU providing media functionality for the vehicle, the ECU configured to present a surround view video on the display device, determine a gesture state and screen coordinates for the gesture, and send the gesture state and the screen coordinates over the network; cameras providing feeds; and an ECU coupled to the network and to the cameras, the ECU providing an advanced driver assistance system (ADAS) for the vehicle, the ECU configured to receive the gesture state and the screen coordinates over the network, generate the surround view video based on the feeds of the cameras and the gesture state and the screen coordinates, and send the surround view video over the network.

Abstract: A system comprises: a sensor configured to detect a gesture relating to a vehicle; a network; an electronic control unit (ECU) coupled to the network, a display device, and the sensor, the ECU providing media functionality for the vehicle, the ECU configured to present a surround view video on the display device, determine a gesture state and screen coordinates for the gesture, and send the gesture state and the screen coordinates over the network; cameras providing feeds; and an ECU coupled to the network and to the cameras, the ECU providing an advanced driver assistance system (ADAS) for the vehicle, the ECU configured to receive the gesture state and the screen coordinates over the network, generate the surround view video based on the feeds of the cameras and the gesture state and the screen coordinates, and send the surround view video over the network.

Abstract: Disrupting convergence of lytic granules produced by cytotoxic lymphocytes allows non-directional degranulation, which improves and broadens killing efficiency of the cytotoxic cells in pathogenic environments such as when used for cancer therapy. Accordingly, methods of inducing multidirectional degranulation by cytotoxic effector cells in a tumor microenvironment, methods of treating a tumor, and related therapeutic composition are described.

Abstract: A vehicle includes a plurality of loudspeakers, memory storing pre-stored sound files, encoding a sound for rendering by the loudspeakers, memory storing an attribute file containing attributes associated with the sounds and associated with audio streams, the attributes defining parameters for rendering each of the sounds and audio streams. An audio manager is configured for receiving the pre-stored sound files, audio streams, and attributes from the attribute file, the received attributes corresponding to the received pre-stored sound files and audio files. The audio manager is configured for, based on the received attributes, determining relative priorities for rendering the received pre-stored sound files and audio streams. An audio mixer is configured for, based on the determined relative priorities, outputting signals to the loudspeakers to render the received pre-stored sound files and audio streams according to the determined relative priorities.

Abstract: A winged vertical take-off and landing aircraft with compound control surfaces comprising flaps and ailerons which can be operated simultaneously with each other offers improved aerodynamic performance and maneuverability. Configuration of the compound control surfaces may be varied to optimize performance in hovering (vertical) flight modes, cruising (horizontal) flight modes, and transitional flight modes.

Abstract: A winged vertical take-off and landing aircraft with compound control surfaces comprising flaps and ailerons which can be operated simultaneously with each other offers improved aerodynamic performance and maneuverability. Configuration of the compound control surfaces may be varied to optimize performance in hovering (vertical) flight modes, cruising (horizontal) flight modes, and transitional flight modes.

Abstract: An aircraft includes a wing. The wing includes an aileron pivotally connected to a trailing edge of the wing, and a Lam aileron pivotally connected to the trailing edge of the wing. The aircraft includes a motor connected to the Lam aileron and configured to rotate the Lam aileron. The aircraft includes a controller configured to detect a deflection of the aileron from a neutral position, calculate a target deflection for the Lam aileron using the deflection of the aileron, and cause the motor to rotate the Lam aileron to the target deflection.

Abstract: A system and related method for the exchange of information, data and instructions between one or more network administrators and one or more network infrastructure devices via one or more media exchanges. Devices are managed using a social media agent including a session agent that translates media messages into network device content and vice versa while maintaining context. Particular media interfaces may be selected for messaging dependent upon the particular message to be exchanged. Shorthand may be used to facilitate messaging through media of interest.

Abstract: Disclosed are techniques for correcting the EUV crosstalk effects. Isolated mask feature component diffraction signals associated with individual layout feature components are determined based on a component-based mask diffraction modeling method such as a domain decomposition method. Mask feature component diffraction signals are then determined based on the isolated mask feature component diffraction signals, layout data and predetermined crosstalk signals. Here, the predetermined crosstalk signals are derived based on mask feature component diffraction signals computed using an electromagnetic field solver and the component-based mask diffraction modeling method, respectively. The mask feature component diffraction signals are then used to process layout designs.

Abstract: An aircraft includes a wing. The wing includes an aileron pivotally connected to a trailing edge of the wing, and a Lam aileron pivotally connected to the trailing edge of the wing. The aircraft includes a motor connected to the Lam aileron and configured to rotate the Lam aileron. The aircraft includes a controller configured to detect a deflection of the aileron from a neutral position, calculate a target deflection for the Lam aileron using the deflection of the aileron, and cause the motor to rotate the Lam aileron to the target deflection.

Abstract: An aircraft includes a wing. The wing includes an aileron pivotally connected to a trailing edge of the wing, and a Lam aileron pivotally connected to the trailing edge of the wing. The aircraft includes a motor connected to the Lam aileron and configured to rotate the Lam aileron. The aircraft includes a controller configured to detect a deflection of the aileron from a neutral position, calculate a target deflection for the Lam aileron using the deflection of the aileron, and cause the motor to rotate the Lam aileron to the target deflection.

Abstract: Disclosed are techniques for correcting the EUV crosstalk effects. Isolated mask feature component diffraction signals associated with individual layout feature components are determined based on a component-based mask diffraction modeling method such as a domain decomposition method. Mask feature component diffraction signals are then determined based on the isolated mask feature component diffraction signals, layout data and predetermined crosstalk signals. Here, the predetermined crosstalk signals are derived based on mask feature component diffraction signals computed using an electromagnetic field solver and the component-based mask diffraction modeling method, respectively. The mask feature component diffraction signals are then used to process layout designs.

Abstract: A system and related method for the exchange of information, data and instructions between one or more network administrators and one or more network infrastructure devices via one or more media exchanges. Devices are managed using a social media agent including a session agent that translates media messages into network device content and vice versa while maintaining context. Particular media interfaces may be selected for messaging dependent upon the particular message to be exchanged. Shorthand may be used to facilitate messaging through media of interest.

Abstract: A system and related method for the exchange of information, data and instructions between one or more network administrators and one or more network infrastructure devices via one or more media exchanges. Devices are managed using a social media agent including a session agent that translates media messages into network device content and vice versa while maintaining context. Particular media interfaces may be selected for messaging dependent upon the particular message to be exchanged. Shorthand may be used to facilitate messaging through media of interest.

Abstract: An aircraft includes a wing. The wing includes an aileron pivotally connected to a trailing edge of the wing, and a Lam aileron pivotally connected to the trailing edge of the wing. The aircraft includes a motor connected to the Lam aileron and configured to rotate the Lam aileron. The aircraft includes a controller configured to detect a deflection of the aileron from a neutral position, calculate a target deflection for the Lam aileron using the deflection of the aileron, and cause the motor to rotate the Lam aileron to the target deflection.

Abstract: An aircraft control system is presented. The system includes a wing including a flap track, and a shuttle connected to the flap track and configured to slide along a length of the flap track. The system includes a flap panel pivotally attached to the shuttle at a flap pivot. The flap panel is configured to rotate about the flap pivot. When the shuttle is deployed along a length of the flap track, the shuttle is configured to prevent rotation of the flap panel about the flap pivot, and when the shuttle is withdrawn into a stowed position, the shuttle is configured to allow the flap panel to rotate about the flap pivot.

Abstract: A mechanical control mixer configured to couple to an aircraft is provided. An axle is mounted to a frame of the mechanical control mixer, and a barrel is configured to rotate about the axle. A central rod is disposed within the barrel. The central rod is configured to rotate with respect to the barrel. A roll control input is connected to the central rod. The roll control input is configured to cause the central rod to rotate within the barrel. Output control rods are connected to the central rod. The output control rods are connected to at least one control surface of the aircraft. An air brake input is connected to the barrel. The air brake input is configured to cause the barrel to rotate about the axle to move at least one of the output control rods.

Abstract: A mechanical control mixer configured to couple to an aircraft is provided. An axle is mounted to a frame of the mechanical control mixer, and a barrel is configured to rotate about the axle. A central rod is disposed within the barrel. The central rod is configured to rotate with respect to the barrel. A roll control input is connected to the central rod. The roll control input is configured to cause the central rod to rotate within the barrel. Output control rods are connected to the central rod. The output control rods are connected to at least one control surface of the aircraft. An air brake input is connected to the barrel.

Abstract: An aircraft control system is presented. The system includes a wing including a flap track, and a shuttle connected to the flap track and configured to slide along a length of the flap track. The system includes a flap panel pivotally attached to the shuttle at a flap pivot. The flap panel is configured to rotate about the flap pivot. When the shuttle is deployed along a length of the flap track, the shuttle is configured to prevent rotation of the flap panel about the flap pivot, and when the shuttle is withdrawn into a stowed position, the shuttle is configured to allow the flap panel to rotate about the flap pivot.

Abstract: Disclosed are techniques for simulating and correcting the mask shadowing effect using the domain decomposition method (DDM). According to various implementations of the invention, DDM signals for an extreme ultraviolet (EUV) lithography mask are determined for a plurality of azimuthal angles of illumination. Base on the DDM signals, one or more layout designs for making the mask may be analyzed and/or modified.