Storage media, unmanned aerial vehicle and shock detection, tracking control method and system
A technology for unmanned aerial vehicles and detection methods, which is applied in the field of unmanned aerial vehicles and their vibration detection and tracking control, can solve problems such as fuselage vibration, unmanned aerial vehicle crashes, and influence on the normal operation and flight of unmanned aerial vehicles. The effect of safety and reliability
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0066] This embodiment provides a vibration detection method for an unmanned aerial vehicle, figure 1 A schematic flow chart of the vibration detection method for an unmanned aerial vehicle provided in Embodiment 1 of the present invention, as shown in figure 1 As shown, the vibration detection method of the unmanned aerial vehicle includes:
[0067] S11: Obtain flight data of the unmanned aerial vehicle;
[0068]Among them, there is no limit to the type and means of obtaining the flight data of the unmanned aerial vehicle. Those skilled in the art can set according to the specific design requirements. For example, the flight data can be set to include flight direction, flight track, flight speed, flight Acceleration, flight geographic location and flight environment, any one or any combination of several items; and based on the above-mentioned different flight data, those skilled in the art can use different means of obtaining data, such as obtaining flight direction informa...
Embodiment 2
[0077] On the basis of the first embodiment above, continue to refer to the appended figure 1 It can be seen that, in order to be more clear about the meaning of the different flight directions in the number of times the unmanned aerial vehicle switches between different flight directions according to the flight data in the above-mentioned embodiment, this embodiment sets the different flight directions to include: the first flight direction and the second flying direction, and an angle is formed between the first flying direction and the second flying direction.
[0078] Among them, for the specific direction characteristics of the first flight direction and the second flight direction, those skilled in the art can set according to specific design requirements, such as east, west, south, north and southeast, northeast, southwest in the map can be set and a combination of any two items in Northwest; or the first flight direction or the second flight direction can be set as any...
Embodiment 3
[0081] figure 2 The schematic flow chart of the vibration detection method of the unmanned aerial vehicle provided by the second embodiment of the present invention, on the basis of the second embodiment above, continue to refer to the attached figure 2 It can be seen that when the angle formed by the first flight direction and the second flight direction is set to 180°, it means that the first flight direction and the second flight direction are opposite to each other; at this time, in order to better understand the technical solution, The first flight direction at this time is defined as the forward flight direction, and the second flight direction is defined as the reverse flight direction, therefore,
[0082] S12: Within the preset time, determine the number of times the unmanned aerial vehicle switches between different flight directions according to the flight data, specifically including:
[0083] S121: Within a preset time, determine the number of times the unmanned...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More