Abstract: An aircraft includes one or more processors individually or collectively configured to determine a current location of the aircraft, determine whether the aircraft is at a first region or a second region based on the current location of the aircraft, and control the aircraft to follow a first flight rule in response to the aircraft being at the first region and follow a second flight rule in response to the aircraft being at the second region, the first flight rule being different from the second flight rule. The first region and the second region are within different jurisdictions.

Abstract: The composite diaphragm for a zinc secondary battery, including: a base diaphragm and a conductive film for the zinc secondary battery, the conductive film being connected to one end of the base diaphragm. The conductive film includes a porous polymer film, and pores of the porous polymer film are filled with conductive compositions, the conductive compositions including 1-10 parts by weight of a conductive agent and 0.1-1 part by weight of an additive. The conductive agent includes at least one of graphite, conductive carbon black, acetylene black, or a graphene carbon nanotube; and the additive includes at least one of a tin powder, a tin dioxide powder, a bismuth powder, a bismuth oxide powder, an indium powder, an indium oxide powder, a lead powder, a lead oxide powder, a cadmium powder, or a cadmium oxide powder.

Abstract: The present disclosure discloses mounting seat (12) and drying apparatus (10), the drying apparatus (10) having an airflow channel (13) and one or more one or more radiation sources (15). The mounting seat (12) comprises a mounting portion (121) and a hollow portion (122), the mounting portion (121) being available for mounting of the one or more radiation sources (15); and in any of the perpendiculars of the mounting seat (12) to the first axis (m) in section, the hollow portion (122) extends from a first edge (123) of the mounting seat (12) to a second edge (124).

Abstract: A flight control apparatus includes one or more memories individually or collectively storing computer program instructions, and one or more processors individually or collectively configured to execute the computer program instructions to: obtain a location of a movable object, obtain a location of a flight restriction zone, and control the movable object to take one or more flight response measures based on the location of the movable object and the location of the flight restriction zone. The flight restriction zone includes a flight restriction strip defined by an area encompassed by a first circle, a second circle, and one or more lines connected to the first circle and the second circle.

Abstract: The disclosure discloses a fusion albumin nanoparticle and application thereof, and belongs to the technical field of biomedicine. In the disclosure, fusion albumin is expressed by using a genetic engineering technology, and the fusion albumin nanoparticle is formed by performing self-assembly and drug loading on the fusion albumin in a neutral aqueous solution. The fusion albumin studied in the disclosure has targetability, pH and enzyme-sensitive functional groups, the nanoparticle prepared by using the fusion albumin has the functions of targetability and controlled drug release, and a method for preparing the fusion albumin nanoparticle is simple and easy to implement and has great application potential.

Abstract: Techniques are disclosed for collaborative map construction using multiple vehicles. Such a system may include a ground vehicle including a first computing device and a first scanning sensor, and an aerial vehicle including a second computing device and a second scanning sensor. The ground vehicle can obtain a first real-time map based on first scanning data using the first scanning sensor, and transmit a first real-time map and position information to the aerial vehicle. The aerial vehicle can receive the first real-time map and the position information from the first computing device, obtain a second real-time map based on second scanning data collected using the second scanning sensor, and obtain a third real-time map based on the first real-time map and the second real-time map.

Abstract: Functional component, forming method thereof and electronic device are provided. The functional component includes a packaging substrate and a connecting wire. The packaging substrate includes a through-hole wire-bonding area including a first insulating layer and a wire-bonding electrode sequentially formed on the substrate. The first insulating layer includes a first through hole, and the wire-bonding electrode covers the first through hole. In an area corresponding to the first through hole, the packaging substrate has wire-bonding bump electrodes on a side of the wire-bonding electrode away from the first insulating layer. The connecting wire includes a wire-bonding connection portion and a wire-bonding extension portion connected to the wire-bonding connection portion. The wire-bonding connection portion is fixedly connected to the wire-bonding electrode. The wire-bonding connection portion extends to cover at least a partial area of a side of at least one of the wire-bonding bump electrodes.

Abstract: An aerial vehicle landing method includes controlling to decelerate, with aid of one or more processors and in response to at least two of a plurality of conditions being satisfied, the aerial vehicle to cause the aerial vehicle to land autonomously. The plurality of conditions includes determining that an external signal related to a human is detected via one or more sensors; determining that a location/orientation change of the aerial vehicle is detected while the aerial vehicle is airborne; and determining that an external contact from an external object is exerted upon the aerial vehicle, the external object being an object that is not part of the aerial vehicle.

Abstract: A movable object includes one or more processors individually or collectively configured to assess a location of the movable object, calculate a distance between the movable object and a restricted region using the location of the movable object, assess whether the distance falls within a first distance threshold, and instruct the movable object to take a movement response measure selected from (1) a first movement response measure when the distance falls within the first distance threshold, and (2) a second movement response measure different from the first movement response measure when the distance falls outside the first distance threshold. The first movement response measure is related to a current movement status of the movable object.

Abstract: A method for controlling an unmanned aerial vehicle (UAV) includes determining whether the UAV is within a first flight restriction zone or a second flight restriction zone and effecting a restriction on the UAV in accordance with a result of the determination, including prohibiting the UAV from flying in response to determining that the UAV is within the first flight restriction zone, or controlling the UAV to fly below a flight ceiling in response to determining that the UAV is within the second flight restriction zone.

Abstract: The present disclosure provides a preparation method of a composite current collector for a zinc secondary battery, a negative electrode plate, and a zinc secondary battery. The preparation method of the composite current collector for the zinc secondary battery comprises: 1) disposing a layer of carbon cloth between two layers of zinc mesh, thermally pressing the two layers of zinc mesh with the carbon cloth, and rolling the two layers of zinc mesh with the carbon cloth to obtain a pressed zinc mesh; 2) soaking the pressed zinc mesh in a graphene dispersion, then taking out and drying the pressed zinc mesh after soaking; and 3) coating two surfaces of the dried pressed zinc mesh with a conductive paste and drying to obtain the composite current collector for the zinc secondary battery.

Abstract: A method includes obtaining, by a vehicle, data from a movable object, generating information for display at the vehicle based at least in part on the data, and causing movement of the vehicle based at least in part on the displayed information. The data is collected by one or more sensors of the movable object. The vehicle is configured to provide one or more services to the movable object.

Abstract: A method for controlling operation of an unmanned aerial vehicle (UAV), includes receiving one or more commands selected by a user via a remote controller of the UAV, and in response to a received landing command: identifying the vehicle from a plurality of vehicles for landing, navigating the UAV to travel in a substantially same direction as the vehicle, and controlling the UAV to land on the vehicle when the UAV approaches the vehicle. The one or more commands includes at least the landing command to land the UAV on a vehicle while the vehicle is in operation.

Abstract: Techniques are disclosed for collaborative map construction using multiple vehicles. Such a system may include a ground vehicle including a first computing device and a first scanning sensor, and an aerial vehicle including a second computing device and a second scanning sensor. The ground vehicle can obtain a first real-time map based on first scanning data using the first scanning sensor, and transmit a first real-time map and position information to the aerial vehicle. The aerial vehicle can receive the first real-time map and the position information from the first computing device, obtain a second real-time map based on second scanning data collected using the second scanning sensor, and obtain a third real-time map based on the first real-time map and the second real-time map.

Abstract: An aerial vehicle includes a vehicle body coupled to one or more blades configured to provide lift to the aerial vehicle, an image device including a first housing containing an optical unit and a second housing containing a non-optical unit and not the optical unit, an apparatus connected to the vehicle body and configured to stabilize at least a portion of the imaging device. The optical unit includes a lens and a photosensor. The apparatus includes a frame assembly, an inertial measurement unit, and a motor assembly coupled to the frame assembly. The frame assembly is configured to support the optical unit without supporting the non-optical unit, and to permit rotation of the optical unit about a first rotational axis or a second rotational axis. The frame assembly includes a first frame member supporting the optical unit, and a second frame member bearing weight of the first frame member.

Abstract: A method includes in response to receiving an instruction for starting a panoramic mode, controlling an unmanned aerial vehicle (UAV) to hover at or near a predetermined location; while the UAV is hovering at or near the predetermined location, causing an image capturing device to capture a plurality of images by controlling a carrier that couples the image capturing device to the UAV to rotate the image capturing device about a first axis of the carrier; and stabilizing the image capturing device against motions with respect to a second axis or a third axis of the carrier while the image capturing device is rotating about the first axis of the carrier.

Abstract: A movable object includes one or more processors individually or collectively configured to assess a location of the movable object, calculate a distance between the movable object and a restricted region using the location of the movable object, assess whether the distance falls within a first distance threshold, and instruct the movable object to take a movement response measure selected from (1) a first movement response measure when the distance falls within the first distance threshold, and (2) a second movement response measure different from the first movement response measure when the distance falls outside the first distance threshold. The first movement response measure is related to a current movement status of the movable object.

Abstract: A chip package structure, manufacturing method thereof, and module are described. In an embodiment, the chip package structure includes: a substrate, a wiring layer, a chip, and a second conductive bump, wherein, in an embodiment, the substrate includes a first region and a second region surrounding the first region, and the wiring layer is located on side of the substrate and includes metal wire, wherein at least part of a metal wire is in contact with the substrate in direction perpendicular to the substrate, and the metal wire overlaps with the second region, wherein the chip is located on side of the wiring layer facing away from the substrate, and the chip corresponds to the first region. In an embodiment, a first conductive bump is provided on side of the chip facing away from the substrate and is electrically connected to the metal wire.

Abstract: The present disclosure provides a laser diode package module. The laser diode package module includes a substrate including a first surface; a cover disposed on the first surface of the substrate; an accommodation space formed between the substrate and the cover; a laser diode die disposed in the accommodation space; and a reflective surface disposed in the accommodation space for outputting light of the laser diode die reflected by the reflective surface and transmitted through a light-transmitting area. The light-transmitting area is at least partially disposed on a surface of the cover opposite the substrate.

Abstract: An aerial vehicle landing method includes controlling to decelerate, with aid of one or more processors and in response to at least two of a plurality of conditions being satisfied, the aerial vehicle to cause the aerial vehicle to land autonomously. The plurality of conditions includes determining that an external signal related to a human is detected via one or more sensors; determining that a location/orientation change of the aerial vehicle is detected while the aerial vehicle is airborne; and determining that an external contact from an external object is exerted upon the aerial vehicle, the external object being an object that is not part of the aerial vehicle.