Abstract: A semiconductor device includes a first region and a second region, and the second region surrounds the first region. The semiconductor device includes at least one electronic unit, a redistribution structure, a plurality of first pads, and a plurality of second pads. The redistribution structure may be electrically connected to at least one electronic unit. A plurality of first pads are arranged on the redistribution structure and correspondingly to the first region. There is a first pitch between two adjacent first pads. A plurality of second pads are arranged on the redistribution structure and correspondingly to the second region. There is a second pitch between two adjacent second pads, so that the first pitch is smaller than the second pitch.

Abstract: The present disclosure relates to a method for fabricating a semiconductor structure. The method includes providing a substrate with a gate structure, an insulating structure over the gate structure, and a S/D region; depositing a titanium silicide layer over the S/D region with a first chemical vapor deposition (CVD) process. The first CVD process includes a first hydrogen gas flow. The method also includes depositing a titanium nitride layer over the insulating structure with a second CVD process. The second CVD process includes a second hydrogen gas flow. The first and second CVD processes are performed in a single reaction chamber and a flow rate of the first hydrogen gas flow is higher than a flow rate of the second hydrogen gas flow.

Abstract: Context information of a handshake between a source entity and a target entity is obtained at a security proxy. The context information is transmitted from the security proxy to a key manager. The key manager maintains a first private key of the security proxy. A first handshake message is received from the key manager. The first handshake message is generated at least based on the context information and signed with the first private key. The first handshake message is then transmitted to the target entity.

Abstract: An automatic nucleic acid detection system and a method thereof are disclosed. The automatic nucleic acid detection method includes: performing, by an automatic control subsystem, on a nucleic acid extraction machine platform, a nucleic acid extraction on one or more specimens in a sample tray to generate one or more corresponding nucleic acids in the sample tray; distributing, by the automatic control subsystem, on a nucleic acid distribution machine platform, the nucleic acid in each hole of the sample tray and a first reagent into a plurality of holes of a detection tray, wherein the number of holes of the detection tray is greater than that of the sample tray; and performing, by the automatic control subsystem, on a nucleic acid detection machine platform, a nucleic acid detection on the detection tray.

Abstract: The present invention discloses a processor control method including: controlling a processor to execute a first operating system in a first state; when the processor executing the first operating system satisfies a predetermined condition, controlling the processor to switch from the first state to a second state; and controlling the processor to execute a second operating system in the second state, wherein an authority of the first state is higher than an authority of the second state.

Abstract: The disclosure provides an electronic device and a manufacturing method thereof. The electronic device includes a package structure, a circuit structure, a bonding structure and an external element. The circuit structure is disposed on the package structure and is electrically connected to the package structure. The circuit structure has a recess. The bonding structure includes a first bonding pad and a second bonding pad. The second bonding pad is disposed in the recess, and the second bonding pad is disposed on the first bonding pad. The bonding structure is disposed between the circuit structure and the external element. The external element is electrically connected to the circuit structure through the bonding structure. A width of the first bonding pad is smaller than a width of the second bonding pad.

Abstract: A package structure including a photonic, an electronic die, an encapsulant and a waveguide is provided. The photonic die includes an optical coupler. The electronic die is electrically coupled to the photonic die. The encapsulant laterally encapsulates the photonic die and the electronic die. The waveguide is disposed over the encapsulant and includes an upper surface facing away from the encapsulant. The waveguide includes a first end portion and a second end portion, the first end portion is optically coupled to the optical coupler, and the second end portion has a groove on the upper surface.

Abstract: A package includes a photonic layer on a substrate, the photonic layer including a silicon waveguide coupled to a grating coupler; an interconnect structure over the photonic layer; an electronic die and a first dielectric layer over the interconnect structure, where the electronic die is connected to the interconnect structure; a first substrate bonded to the electronic die and the first dielectric layer; a socket attached to a top surface of the first substrate; and a fiber holder coupled to the first substrate through the socket, where the fiber holder includes a prism that re-orients an optical path of an optical signal.

Abstract: A method, a computer program product, and a system for implementing a dynamic virtual database honeypot. The method includes relaying a query request received from a database client to a database and receiving, from the database, a response relating to the query request. The method also includes determining the query request is an attack on the database based on session information relating to the database and the database client, generating a honey token based on information contained within the response, generating an alternate response formatted in a same format as the response and containing artificial information that masks the information contained within the response. The method further includes inserting the honey token into the alternate response and transmitting the alternate response to the database client.

Abstract: A semiconductor structure, comprising a redistribution layer (RDL) including a dielectric layer and a conductive trace within the dielectric layer; a first conductive member disposed over the RDL and electrically connected with the conductive trace; a second conductive member disposed over the RDL and electrically connected with the conductive trace; a first die disposed over the RDL; a second die disposed over the first die, the first conductive member and the second conductive member; and a connector disposed between the second die and the second conductive member to electrically connect the second die with the conductive trace, wherein the first conductive member is electrically isolated from the second die.

Abstract: Duplicated packet transmission methods are provided. The duplicated packet transmission method may include the following steps. A sender may determine whether to pad at least one duplicated packet into a multi-user physical-protocol-data-unit (MU-PPDU) based on at least one condition. Then, the sender may transmit the MU-PPDU with the duplicated packet to at least one receiver when the condition is met.

Abstract: A laser cutting method of the present invention comprises the steps below: a feeding mechanism generating movement information by driving the workpiece to move, and transmitting the movement information to a computing mechanism; transmitting a cutting path to the computing mechanism, making the computing mechanism calculate the cutting path and the movement information to generate a compensation cutting path, and transmitting the compensation cutting path to a fixed laser cutting mechanism; by a laser cutting mechanism, projecting a laser beam onto a moving workpiece, and continuously changing the projection direction of the laser beam onto the workpiece according to the compensation cutting path, so that the workpiece is cut by the laser beam to form a target pattern. Whereby, when the laser cutting mechanism performs laser cutting on the workpiece, the workpiece still moves without stopping, thereby shortening the processing time and relatively improving production efficiency.

Abstract: A plastic injection security label and manufacturing method of the same may comprise a mold having a pair of die sets, and at least one of the two die sets has a molding cavity formed on an inner surface thereof. The surface of the molding cavity has a plurality of nicks formed by the laser engraving machine at partial positions thereof, and the engraved nicks are arranged into a designed image or code to form a label generating area on the surface of the molding cavity. In the manufacturing process, after the die sets are coupled together, the plastic material is injected into the mold and filled with the molding cavity and the nicks of the label generating area, and a plastic product with the security label is integrally formed after the plastic material is cooled and solidified.

Abstract: A monitoring system for an aircraft guiding process is used to monitor a docking process of an aircraft guided by a guiding information display of a VDGS (Visual Docking Guidance System) along a J-line at an apron, and includes an image capturing module, an image integrating unit, a monitoring display and a video recorder. The image capturing module has a first camera for filming a docking process of an aircraft to obtain a docking video, and a second camera for filming the guiding information display to obtain a guiding information video. The image integrating unit integrates the docking video and the guiding information video into an integrated video in a synchronously-displayed and adjoining manner. The monitoring display receives and displays the integrated video. The video recorder records the integrated video. Accordingly, the present disclosure also provides a guiding method for a guiding process of an aircraft.

Abstract: An aircraft guidance system includes a reviewing and video synchronization device connected to a display panel. The display panel receives and displays guidance status of an aircraft. The reviewing and video synchronization device includes an operator panel, a video recording unit and a built-in recording unit. The operator panel includes a display screen and a plurality of keys. The display screen and the display panel synchronizedly display information. The video recording unit records the information displayed on the display screen. The built-in recording unit records the scanning signals and time stamps received by the display panel.

Abstract: A guiding method for aircraft docking process, which is used to detect an aircraft when docking to a stop line along a J-line on apron, includes steps as followed. According to response distances of different positions from a laser scanner, a distance between the aircraft and the stop line and offset angle during the docking process are detected. To show the distance and offset angle on a data display panel as guiding reference when a pilot of the aircraft operates the aircraft. The guiding method further has a waiting stage, a positioning stage, and a distinguishing stage and a guiding stage.

Abstract: An aircraft guidance system includes a reviewing and video synchronization device connected to a display panel. The display panel receives and displays guidance status of an aircraft. The reviewing and video synchronization device includes an operator panel, a video recording unit and a built-in recording unit. The operator panel includes a display screen and a plurality of keys. The display screen and the display panel synchronizedly display information. The video recording unit records the information displayed on the display screen. The built-in recording unit records the scanning signals and time stamps received by the display panel.

Abstract: A guiding method for aircraft docking process, which is used to detect an aircraft when docking to a stop line along a J-line on apron, includes steps as followed. According to response distances of different positions from a laser scanner, a distance between the aircraft and the stop line and offset angle during the docking process are detected. To show the distance and offset angle on a data display panel as guiding reference when a pilot of the aircraft operates the aircraft. The guiding method further has a waiting stage, a positioning stage, and a distinguishing stage and a guiding stage.