Title:
AIRCRAFT ATTITUDE CONTROL METHOD AND APPARATUS, ELECTRONIC DEVICE, AND STORAGE MEDIUM
Document Type and Number:
WIPO Patent Application WO/2024/061150
Kind Code:
A1
Abstract:
An aircraft attitude control method. An aircraft comprises several supporting legs (100) and several rotor wings (200), wherein a bottom portion of each supporting leg (100) is provided with a pressure sensor (300) to measure the pressure on the bottom portion of the supporting leg, and the rotor wings (200) and the supporting legs (100) are correspondingly arranged on two sides of the aircraft. The aircraft attitude control method comprises: by means of a pressure sensor on each supporting leg, acquiring the pressure on a bottom portion of the supporting leg at each side (S1); and according to the pressure on the bottom portion of the supporting leg at each side, controlling the power output of a corresponding rotor wing at each side, so as to adjust the attitude of an aircraft (S2). The aircraft attitude control method can prevent an aircraft from bouncing back which is caused by the fact that a rotor wing still generates a lift force after the aircraft lands, thereby realizing a stable landing attitude.
More Like This:
Inventors:
TIAN YU (CN)
CUI YONGQIANG (CN)
CUI YONGQIANG (CN)
Application Number:
PCT/CN2023/119326
Publication Date:
March 28, 2024
Filing Date:
September 18, 2023
Export Citation:
Assignee:
AUTOFLIGHT KUNSHAN CO LTD (CN)
International Classes:
G05D1/00
Foreign References:
| CN113401336A | 2021-09-17 | |||
| CN107117330A | 2017-09-01 | |||
| CN108750141A | 2018-11-06 | |||
| KR102249308B1 | 2021-05-07 | |||
| US20170217323A1 | 2017-08-03 |
Download PDF:
Previous Patent: BATTERY MODULE ASSEMBLING METHOD
Next Patent: CLUTCH WINCH STRUCTURE FOR PROTECTING DRIVING DEVICE
Next Patent: CLUTCH WINCH STRUCTURE FOR PROTECTING DRIVING DEVICE