A remote controlled aircraft includes an aircraft that may be flown. A plurality of light emitters is coupled to the aircraft. A plurality of fans is coupled to the aircraft. Each of the fans may move air thereby facilitating each of the fans to urge the aircraft to fly. A control unit is coupled to the aircraft and the control unit is electrically coupled to each of the fans. The control unit includes a global positioning system. Thus, the control unit may identify a position of the aircraft with respect to Earth. A remote control is provided and the remote control may be manipulated. The remote control is in electrical communication with the control unit such that the remote control controls directional flight of the aircraft.

An aerial vehicle capable of convertible flight from hover to linear flight includes a body having a longitudinal body axis, a plurality of forward wings, a plurality of aft wings, at least one motor, and at least three aerodynamic propulsors driven by the at least one motor. Each forward wing extends a forward wing plane. Each aft wing extends from an aft wing plane. The aerodynamic propulsors are mounted longitudinally between the plurality of forward wings and plurality of aft wings.

Methods and systems for utilizing a mobile computing device (e.g., such as a mobile phone) for use in controlling a model vehicle are described. Consistent with some embodiments, a mobile computing device provides various user controls for generating signals that are communicated to a radio transmitter device coupled with the mobile computing device, and ultimately broadcast to a receiver residing at a model vehicle. With some embodiments, the mobile computing device may be integrated with a controller housing which provides separate user controls, such that a combination of user controls present on the mobile computing device and the controller housing can be used to control a model vehicle.

The present disclosure provides a collision judgment method and apparatus. The method includes: determining, by a moving device, according to acceleration data collected by an acceleration sensor, that the moving device collides; sending collision information to the corresponding control device, including at least a moving device identifier and a collision time; sending, by the corresponding control device, the collision information to a collision judgment device; detecting, by the collision judgement device, whether at least two collision information sent by the at least two control devices is received within a predetermined time interval; when the at least two collision information is received within the predetermined time interval, and a difference between collision times carried in the at least two collision information is less than a preset threshold, determining that moving devices corresponding to moving device identifiers carried in the at least two collision information collided with one other.

An unmanned aerial vehicle (UAV) includes a first communication module, a second communication module, and one or more processors. The first communication module is configured to directly receive control data from a controlling terminal via a first communication link and the control data is used to control operations of the UAV. The second communication module is configured to transmit feedback data to a monitoring terminal via a second communication link. The monitoring terminal is located remotely from the UAV. The one or more processors are, individually or collectively, configured to terminate and reactivate the first wireless communication link based on one or more predetermined criteria.

Methods and systems for utilizing a mobile computing device (e.g., such as a mobile phone) for use in controlling a model vehicle are described. Consistent with some embodiments, a mobile computing device provides various user controls for generating signals that are communicated to a radio transmitter device coupled with the mobile computing device, and ultimately broadcast to a receiver residing at a model vehicle. With some embodiments, the mobile computing device may be integrated with a controller housing which provides separate user controls, such that a combination of user controls present on the mobile computing device and the controller housing can be used to control a model vehicle.

A self-propelled toy glider includes a flexible frame and a flight surface. The flexible frame may deformed and held within the user's hand. When deformed, the flexible frame stores spring energy. This spring energy is subsequently used to propel the self-propelled toy glider forward as it returns to original shape. Related to glider durability and overall safety, the flexible frame can elastically deform when the toy glider impacts objects during flight.

A wireless transmitter includes a pair of control sticks, circuitry coupled to control sticks, and an antenna coupled to the circuitry. The circuitry is configured to process signals produced by the control sticks to provide control inputs for the speed, direction, and other flight characteristics of the model aircraft being controlled by the transmitter. The transmitter is configured for multiple operational modes in which the pair of control sticks engage or disengage functionality, such as return-to-center functionality, vertical or horizontal position limiting functionality, or position select functionality.

A motor assembly that includes a motor having a motor casing, a rotatable shaft extending from said motor casing to a shaft length and a hub coupled to said rotatable shaft, the hub having a circumferential skid surface disposed immediately proximal to the motor casing and having a channel configured to seat a propeller, when a propeller is present, wherein a bending moment applied to the shaft through the hub results in the circumferential skid surface contacting said motor casing.

A remote control device for an aircraft and an aircraft system are provided. The aircraft system includes the aircraft (3) and the remote control device. The remote control device includes a first global positioning system (GPS) chip (4), a magnetometer (5), a gyroscope chip (6), a main control chip (8) and a first signal transceiver (9). The first GPS chip (4), the magnetometer (5) and the gyroscope chip (6) are respectively connected with the main control chip (8), and the first signal transceiver (9) is connected with the main control chip (8). The first GPS chip (4), the magnetometer (5) and the gyroscope chip (6) transmit three different position signals of the remote control device to the main control chip (8) respectively; the main control chip (8) transmits a control signal through the first signal transceiver (9), and the first signal transceiver (9) receives a condition signal of the aircraft and then transmits to the main control chip (8). The remote control device adopts a command remote control technology, so as to operate a flight direction and a flight distance of the aircraft (3) conveniently, have a high operation precision on the aircraft (3) and increase interest during an operation process.