Abstract

An aircraft, comprising a fuselage module (100) and an empennage module (200), and further comprising an adjustment structure, wherein the adjustment structure comprises: at least two first adjustment parts provided on one of the fuselage module and the empennage module, and at least one second adjustment part provided on the other one of the fuselage module and the empennage module, wherein the second adjustment part is suitable for working in conjunction to different first adjustment parts, so that the position of the empennage module is adjustably mounted on the fuselage module, and the height of the empennage module is different when the second adjustment part works in conjunction to the different first adjustment parts. The aircraft can adjust the flight attitude of the aircraft by adjusting the mounting position of the empennage module, and is strong in flight attitude control capacity.

IPC Classes  ?

• A63H 27/18 - Constructional features of fuselages, wings or the like, e.g. for model aircraft
• B64C 33/02 - WingsActuating mechanisms therefor

Abstract

An ornithopter, comprising: an aircraft main body (1), which is provided with a head; at least two infrared transmitters (2), which are used for transmitting infrared rays outwards, and are arranged on the aircraft main body; and an infrared receiver (3), which is used for receiving the infrared rays reflected back by external objects, and is arranged at the front end of the aircraft main body, a receiving direction of the infrared receiver facing the front of the aircraft main body. Any two of the infrared transmitters are symmetrically distributed on two sides of the infrared receiver, transmitting directions of the infrared transmitters deviate towards two sides of the aircraft main body respectively, and a first preset included angle is formed horizontally between the transmitting directions of the infrared transmitters and the receiving direction of the infrared receiver. Accordingly, the ornithopter can identify obstacles in a large wide-angle range in front and obliquely in front of same to give feedback, and the flight safety of the ornithopter is improved.

IPC Classes  ?

• B64C 33/00 - Ornithopters
• G01S 17/93 - Lidar systems, specially adapted for specific applications for anti-collision purposes

Abstract

The present application relates to an aircraft, an aircraft control method and apparatus, and a computer-readable storage medium. The aircraft is provided with at least one sensor. The method comprises: detecting the state of an electric motor of an aircraft; acquiring at least one piece of sensing data of at least one sensor; and controlling, according to the state of the electric motor and the at least one piece of sensing data, the aircraft to execute a power-on operation or power-off operation, so that the aircraft can be automatically controlled to execute a power-on operation or power-off operation, thereby improving the user experience.

IPC Classes  ?

• B64C 33/02 - WingsActuating mechanisms therefor
• G05D 1/08 - Control of attitude, i.e. control of roll, pitch, or yaw

Abstract

An electromagnetic steering engine and an aircraft. The electromagnetic steering engine comprises a driving coil (10), a permanent magnet (11), a coil fixing holder (12), and a permanent magnet fixing holder (13); the permanent magnet (11) is mounted in a through hole of the permanent magnet fixing holder; the driving coil is mounted in a through hole of the coil fixing holder (12); the permanent magnet (11) is located outside of the driving coil; the permanent magnet fixing holder (13) is rotatably connected to the coil fixing holder (12) by means of a rotating shaft; and when the permanent magnet (11) rotates, the permanent magnet fixing holder (13) is driven to synchronously rotate. After the driving coil is electrified, an electromagnetic force generated acts on the permanent magnet, so that the permanent magnet rotates at a large angle, thereby implementing that the permanent magnet fixing holder synchronously rotates along with the permanent magnet.

IPC Classes  ?

• B64C 13/50 - Transmitting means with power amplification using electrical energy
• H02K 21/14 - Synchronous motors having permanent magnetsSynchronous generators having permanent magnets with stationary armatures and rotating magnets with magnets rotating within the armatures