Abstract: A pair of intelligent assisted vision glasses includes an eyeglass body, the left and right frames respectively having two accommodation rooms with transparent liquid, a set of left eye lenses and a set of right eye lenses respectively in the left and right frames, a microelectromechanical component, a sensor electrically connected with the microelectromechanical component for detecting the axial length of eyeball and the curvature of the cornea to generate control signal, and a pair of push units respectively arranged at upper ends of the left frame and a pair of push units respectively arranged at upper ends of the right frame and each pair of push units is electrically connected with the microelectromechanical component. The microelectromechanical component controls the push units to change the curvature of the set of left and/or right eye lenses according to the controlling signal.

Abstract: A pair of intelligent assisted vision glasses includes an eyeglass body, the left and right frames having accommodation room with transparent liquid, a set of left eye lenses and a set of right eye lenses respectively in the left and right frames, a microelectromechanical component, a sensor electrically connected with the microelectromechanical component for detecting the axial length of eyeball and the curvature of the cornea to generate control signal, and a push unit arranged on the left and right frames and electrically connected with the microelectromechanical component. The microelectromechanical component controls the push unit to change the curvature of the set of left and/or right eye lenses according to the controlling signal. The flow volume of the transparent liquid in the voids between the set of left and/or right eye lenses is changed corresponding to the curvature of the set of left and/or right eye lenses.

Abstract: An unmanned aerial vehicle (UAV) and a landing method thereof are provided. The landing method includes the following steps. Firstly, a depth image of a scene is obtained. Next, a landing position is determined in accordance with the depth image. Next, a height information of the landing position is obtained. Next, a plurality of relative distances of the landing gears relative to the landing position are adjusted in accordance with the height information to make the relative distances substantially the same. Then, the UAV lands on the landing position.

Abstract: An Unmanned Aerial Vehicle (UAV) includes a fuselage, a plurality of rotors, and a sensor, wherein the fuselage includes a control module and a signal processing module, and the control module is connected the arms, which is used to control the rotation of arms. The sensor is configured to the fuselage of the UAV, which is used to detect the rotation change value of the UAV. The signal processing module is connected with the sensor and the control module, which is used to receive and analyze the signal of the sensor, and the control module controls the following flying of the UAV.

Abstract: An unmanned aerial vehicle (UAV) and a landing method thereof are provided. The landing method includes the following steps. Firstly, a depth image of a scene is obtained. Next, a landing position is determined in accordance with the depth image. Next, a height information of the landing position is obtained. Next, a plurality of relative distances of the landing gears relative to the landing position are adjusted in accordance with the height information to make the relative distances substantially the same. Then, the UAV lands on the landing position.

Abstract: An Unmanned Aerial Vehicle (UAV) includes a fuselage, a plurality of rotors, and a sensor, wherein the fuselage includes a control module and a signal processing module, and the control module is connected the arms, which is used to control the rotation of arms. The sensor is configured to the fuselage of the UAV, which is used to detect the rotation change value of the UAV. The signal processing module is connected with the sensor and the control module, which is used to receive and analyze the signal of the sensor, and the control module controls the following flying of the UAV.