Abrégé

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.

Classes IPC  ?

• A63H 27/18 - Caractéristiques structurelles des fuselages, des ailes ou analogues, p. ex. pour avions modèles réduits
• B64C 33/02 - AilesMécanismes d'actionnement des ailes

Abrégé

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.

Classes IPC  ?

• B64C 33/00 - Ornithoptères
• G01S 17/93 - Systèmes lidar, spécialement adaptés pour des applications spécifiques pour prévenir les collisions

Abrégé

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.

Classes IPC  ?

• B64C 33/02 - AilesMécanismes d'actionnement des ailes
• G05D 1/08 - Commande de l'attitude, c. à d. élimination ou réduction des effets du roulis, du tangage ou des embardées

Abrégé

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.

Classes IPC  ?

• B64C 13/50 - Dispositifs de transmission avec amplification de puissance utilisant l'énergie électrique
• H02K 21/14 - Moteurs synchrones à aimants permanentsGénératrices synchrones à aimants permanents avec des induits fixes et des aimants tournants avec des aimants tournant à l'intérieur des induits