| 摘要 |
An unmanned aerial vehicle (100), comprising an inertial measurement unit (20), a positioning component (30), a controller (50), a memory (40) and an early warning prompt unit (70). The inertial measurement unit (20) comprises a gyroscope (21), an angular velocity meter (22) and a processor (23). The positioning component (30) comprises a magnetic field inductor (31) and a GPS positioning unit (32). The processor (23) is used for detecting various operational data of the gyroscope (21), the angular velocity meter (22), the magnetic field inductor (31) and the GPS positioning unit (32). The controller (50) is used for extracting the various operational data detected by the processor (23) and analyzing whether there is an abnormity according to a plurality of items of extracted operational data. The memory (40) stores a plurality of segments of prompt configuration files corresponding to a plurality of cases of abnormal conditions on a one-to-one basis. When the controller (50) analyzes that there is an abnormity according to the plurality of items of extracted operational data, the controller (50) outputs a corresponding prompt configuration file from the memory (40) to the early warning prompt unit (70) so that the early warning prompt unit (70) sends a prompt corresponding to the abnormal conditions. Also provided is a flight state auxiliary prompt method. |
