Abstract: In an embodiment, an electronic device includes a display and processing circuitry. The display includes a plurality of pixels arranged in a plurality of rows, wherein a first grouping of the plurality of rows displays image content during a first portion of an image frame, and wherein a second grouping of the plurality of rows displays image content during a second portion of the image frame. The processing circuitry is operatively coupled to the display and determines a velocity associated with the image content displayed by the first grouping of the plurality of rows moving across the display and adjusts a position of the image content displayed by the second grouping of the plurality of rows during the second portion of the image frame.

Abstract: A rotor-wing assembly includes a motor, a propeller, and a connection assembly connecting the propeller to the motor. The motor includes a rotating portion. The connection assembly includes a locking member and a reinforcing member arranged between the propeller and the motor. The locking member locks the propeller to the rotating portion. A first end of the reinforcing member is mounted at the rotating portion. A second end of the reinforcing member opposite to the first end is engaged with the locking member, to reinforce the locking member to lock the propeller to the rotating portion.

Abstract: A motor includes a bottom and a top opposite to the bottom. The bottom is a mounting side of the motor and the bottom is inclined relative to a rotation axis of the motor.

Abstract: A portable device for holding and carrying an unmanned aerial vehicle (“UAV”) includes a body. The body includes a first holding member configured to hold the UAV and having a shape matching a shape of the UAV. The portable device also includes a charging board disposed in the body. The portable device also includes a first charging station disposed in the first holding member and configured to electrically connect with the charging board for charging the UAV. The portable device further includes at least one second charging station disposed on the body and configured to electrically connect with the charging board for charging at least one battery.

Abstract: A charging dock is provided. The charging dock includes: a main body; a charging unit disposed with the main body; and a plurality of cover plates. The charging unit includes a plurality of battery sockets. Each cover plate corresponds to one of the plurality of battery sockets. Each cover plate is movably connected to the main body. And each cover plate is switchable between a closed configuration covering the corresponding battery socket and an open configuration exposing the corresponding battery socket. Further, a charging assembly is provided. The charging assembly includes the forgoing charging dock and a rechargeable battery configured to be mounted on one of the plurality of cover plates in the open configuration, and plugged into the corresponding battery socket.

Abstract: An antenna structure includes a base, a first radiator, and a second radiator. The base is configured to be rotatably connected to a remote controller body of a remote controller of an unmanned aerial vehicle (UAV) system. One ends of the first radiator and the second radiator are connected to the base, and other ends of the first radiator and the second radiator extend away from the base. The first radiator and the second radiator are fixedly connected to the base in a rotation direction relative to the remote controller body and are configured to rotate simultaneously with the base in the rotation direction.

Abstract: A motor includes a bottom and a top opposite to the bottom. The bottom is a mounting side of the motor and the bottom is inclined relative to a rotation axis of the motor.

Abstract: A camera assembly includes a bracket and a camera device. The bracket includes a mounting surface, which is configured to be connected to a body of an unmanned aerial vehicle (UAV). The camera device is mounted at the bracket. An optical axis of the camera device tilts downward relative to the mounting surface.

Abstract: An unmanned aerial vehicle (UAV) includes a heat dissipation device, an inertial measurement unit (IMU), and a control module. The heat dissipation device includes an air guiding cover and a heat conduction plate. The air guiding cover includes an air duct configured to guide an airflow, and the heat conduction plate directly constitutes a portion of a sidewall of the air duct. The IMU module is received within the air duct. The control module is located outside the air duct and disposed at a side of the heat conduction plate that faces away from the IMU module. Heat generated by the IMU module is taken away directly by the airflow within the air duct.

Abstract: A portable device for holding and carrying an unmanned aerial vehicle (“UAV”) includes a body. The body includes a first holding member configured to hold the UAV and having a shape matching a shape of the UAV. The portable device also includes a charging board disposed in the body. The portable device also includes a first charging station disposed in the first holding member and configured to electrically connect with the charging board for charging the UAV. The portable device further includes at least one second charging station disposed on the body and configured to electrically connect with the charging board for charging at least one battery.

Abstract: An unmanned aerial vehicle (UAV) includes a fuselage, an electrical component, and an adapter arranged at the fuselage. The fuselage includes a battery compartment for accommodating a battery. The battery compartment includes an electrical connector for electrically coupling to the battery. The adapter is electrically coupled to the electrical connector and includes an access unit electrically coupled to the electrical connector and an adapting unit detachably coupled to the access unit. The adapting unit is configured to be electrically connected to the access unit when the adapting unit is coupled to the access unit. The adapting unit is electrically coupled to the electrical component through an adapting conductive wire to conduct power from the battery to the electrical component.

Abstract: A rotor-wing assembly includes a motor, a propeller, and a connection assembly connecting the propeller to the motor. The motor includes a rotating portion. The connection assembly includes a locking member and a reinforcing member arranged between the propeller and the motor. The locking member locks the propeller to the rotating portion. A first end of the reinforcing member is mounted at the rotating portion. A second end of the reinforcing member opposite to the first end is engaged with the locking member, to reinforce the locking member to lock the propeller to the rotating portion.

Abstract: An unmanned aerial vehicle (UAV) includes a fuselage, an electrical component, and an adapter arranged at the fuselage. The fuselage includes a battery compartment for accommodating a battery. The battery compartment includes an electrical connector for electrically coupling to the battery. The adapter is electrically coupled to the electrical connector and includes an access unit electrically coupled to the electrical connector and an adapting unit detachably coupled to the access unit. The adapting unit is configured to be electrically connected to the access unit when the adapting unit is coupled to the access unit. The adapting unit is electrically coupled to the electrical component through an adapting conductive wire to conduct power from the battery to the electrical component.

Abstract: A charging dock is provided. The charging dock includes: a main body; a charging unit disposed with the main body; and a plurality of cover plates. The charging unit includes a plurality of battery sockets. Each cover plate corresponds to one of the plurality of battery sockets. Each cover plate is movably connected to the main body. And each cover plate is switchable between a closed configuration covering the corresponding battery socket and an open configuration exposing the corresponding battery socket. Further, a charging assembly is provided. The charging assembly includes the forgoing charging dock and a rechargeable battery configured to be mounted on one of the plurality of cover plates in the open configuration, and plugged into the corresponding battery socket.

Abstract: An unmanned aerial vehicle (UAV) includes a heat dissipation device, an inertial measurement unit (IMU), and a control module. The heat dissipation device includes an air guiding cover and a heat conduction plate. The air guiding cover includes an air duct configured to guide an airflow, and the heat conduction plate directly constitutes a portion of a sidewall of the air duct. The IMU module is received within the air duct. The control module is located outside the air duct and disposed at a side of the heat conduction plate that faces away from the IMU module. Heat generated by the IMU module is taken away directly by the airflow within the air duct.

Abstract: A heat dissipation device includes an air guiding cover and a heat conduction plate. The air guiding cover includes an air duct configured to guide an airflow and including a mounting window formed on a sidewall of the air duct, an air inlet formed at a first end of the air duct, and an air outlet formed at a second end of the air duct. The heat conduction plate is disposed at the mounting window and covers the mounting window.

Abstract: A heat dissipation device includes an air guiding cover and a heat conduction plate. The air guiding cover includes an air duct configured to guide an airflow and including a mounting window formed on a sidewall of the air duct, an air inlet formed at a first end of the air duct, and an air outlet formed at a second end of the air duct. The heat conduction plate is disposed at the mounting window and covers the mounting window.