Title:
FLIGHT CONTROLLER AND UNMANNED AERIAL VEHICLE
Document Type and Number:
WIPO Patent Application WO/2020/093861
Kind Code:
A1
Abstract:
A flight controller (10) and an unmanned aerial vehicle (1). The flight controller (10) comprises an inertial measurement unit (IMU) (100) and a microcontroller unit (MCU) (200). The inertial measurement unit (IMU) (100) comprises a sensor circuit (110). The sensor circuit (110) comprises at least two sensors (111) and at least two regulated power supplies (112). Each sensor (111) is electrically connected one-to-one to each regulated power supply (112). The microcontroller unit (MCU) (200) is electrically connected to the at least two sensors (111) separately, and is configured to acquire inertial data collected by the sensors (111), and to control, according to the inertial data, the unmanned aerial vehicle (1) to fly. The flight controller (10) has a simple structure and high reliability, and can save costs.
Inventors:
WU BIN (CN)
Application Number:
PCT/CN2019/112343
Publication Date:
May 14, 2020
Filing Date:
October 21, 2019
Export Citation:
Assignee:
GUANGZHOU XAIRCRAFT TECH CO LTD (CN)
International Classes:
G05D1/08; G05D1/10
Foreign References:
| CN109144091A | 2019-01-04 | |||
| CN105867414A | 2016-08-17 | |||
| CN105258953A | 2016-01-20 | |||
| CN108225313A | 2018-06-29 | |||
| CN205246884U | 2016-05-18 | |||
| CN207407893U | 2018-05-25 | |||
| CN106201022A | 2016-12-07 | |||
| US20160221663A1 | 2016-08-04 | |||
| US20050150289A1 | 2005-07-14 |
Attorney, Agent or Firm:
CHOFN INTELLECTUAL PROPERTY (CN)
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