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.
Unmanned aerial vehicle and flying method thereof
2017-11-07
Patent
Electronic Resource
English
IPC: | G01D MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE , Anzeigen oder Aufzeichnen in Verbindung mit Messen allgemein / B64C AEROPLANES , Flugzeuge / G01W METEOROLOGY , Meteorologie / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen |
UNMANNED AERIAL VEHICLE FLYING METHOD AND UNMANNED AERIAL VEHICLE FLYING SYSTEM
European Patent Office | 2017
|UNMANNED AERIAL VEHICLE AND FLYING CONTROL METHOD THEREOF
European Patent Office | 2020
|Unmanned aerial vehicle and flying control method thereof
European Patent Office | 2021
|