CN-224203601-U - Multi-element control system suitable for unmanned aerial vehicle

CN224203601UCN 224203601 UCN224203601 UCN 224203601UCN-224203601-U

Abstract

The utility model discloses a multi-element control system suitable for an unmanned aerial vehicle, which belongs to the technical field of unmanned aerial vehicles and comprises a power supply unit, a signal transmission unit, a notification unit, a battery, a signal processor, a first communication module, a second communication module, at least two sets of power supply controllers and a light source controller, wherein the battery is arranged in a battery shell, the power supply controller is used for controlling the battery, the signal processor modulates an electric signal, the electromagnetic signal converter converts the modulated electric signal into an electromagnetic wave signal, the first communication module outputs the electromagnetic wave signal, the second communication module is respectively connected with the signal processor, the power supply controllers and the light source controller, the power supply unit, the signal transmission unit and the notification unit are arranged on the unmanned aerial vehicle, at least one set of the second communication modules is in communication connection, and when one set of the second communication modules is disconnected, at least one of the power supply controllers, the signal processor and the light source controller in the other set is started to correspond to the functions according to a preset program, so that instant power supply switching and communication switching can be realized, and subsequent unmanned aerial vehicle searching can be conveniently achieved.

Inventors

MA LONGMIN
Wen Binxin
WEI KAIJING

Assignees

广西座头鲸无人机科技有限公司

Dates

Publication Date: 20260505
Application Date: 20250519

Claims (10)

1. Multi-element control system suitable for unmanned aerial vehicle, its characterized in that includes: The power supply unit comprises a battery, a battery shell, a power supply circuit and a power supply controller; The signal transmission unit comprises an electromagnetic signal converter, a signal processor, a first communication module and a second communication module; a notification unit including a light source and a light source controller; the battery is arranged in the battery shell, and the power supply controller is connected with and controls the battery to output electric energy through the power supply circuit; The signal processor is used for modulating an electric signal, the electromagnetic signal converter is used for converting the modulated electric signal into a corresponding electromagnetic wave signal, and the first communication module is used for outputting the electromagnetic wave signal; The second communication module is respectively connected with the signal processor, the power supply controller and the light source controller; The power supply unit, the signal transmission unit and the notification unit are arranged on the unmanned aerial vehicle, at least two sets of the signal transmission unit and the notification unit are arranged, and the second communication modules are correspondingly in communication connection; When one of the second communication modules is disconnected, at least one of the power supply controller, the signal processor and the light source controller in the other set starts corresponding functions according to a preset program.
2. The multiple control system for an unmanned aerial vehicle according to claim 1, wherein the battery case is a combined case, one end of the battery case is provided with an opening, the inside of the opening is provided with a contact point, and the contact point is connected to the signal transmission unit or the notification unit through a tubular connection line and/or a strip connection line.
3. The multi-element control system for the unmanned aerial vehicle according to claim 2, wherein openings are respectively provided at both sides of one end of the battery case, wherein one opening is connected with a tubular connection line, and the other opening is connected with a strip connection line; the tubular connecting wire and the strip connecting wire are used for realizing electric connection or communication connection.
4. A multiple control system for an unmanned aerial vehicle according to claim 3, wherein the notification unit is provided with a combined protective housing, the light source being a matrix of lamps; the upper surface of the protective shell is provided with the lamp matrix and a stripe-type concave-convex structure; The side of the protective shell is provided with a connecting inlet for connecting the tubular connecting wire and the strip connecting wire.
5. The multiple control system for a drone of claim 4, wherein the bottoms of the notification unit and the power supply unit are secured to a pole of the drone by clamps.
6. The multiple control system for an unmanned aerial vehicle of claim 4, wherein the light source controller is configured to control the light matrix such that the light fixtures in the light matrix are turned on, changed in brightness, and turned off according to a specified rule.
7. The multiple control system for a drone of claim 6, wherein the drone is provided with a third communication module communicatively connected to the first communication module and/or the second communication module; The unmanned aerial vehicle transmits a signal to be output to the first communication module and/or the second communication module through the third communication module.
8. The multiple control system according to claim 7, wherein the first communication module is configured to transmit the signal to be output to the signal processor, the signal processor is configured to process the signal to be output to obtain the modulated electrical signal, the electromagnetic signal converter is configured to convert the modulated electrical signal corresponding to the signal to be output into a corresponding electromagnetic wave signal, and the first communication module outputs the electromagnetic wave signal.
9. The multiple control system for an unmanned aerial vehicle of claim 7, wherein the second communication module is configured to communicate the signal to be output to the light source controller, the light source controller causing the light fixtures in the light matrix to illuminate, change brightness, and extinguish based on the signal to be output.
10. The multi-element control system for a drone of claim 9, wherein the third communication module is connected to the first communication module and/or the second communication module; the first communication module and/or the second communication module are/is configured to acquire an external control signal, and transmit the external control signal to the unmanned aerial vehicle through the third communication module.

Description

Multi-element control system suitable for unmanned aerial vehicle Technical Field The utility model relates to the technical field of unmanned aerial vehicles, in particular to a multi-element control system suitable for an unmanned aerial vehicle. Background The unmanned aerial vehicle is used as a carrier of the unmanned aerial vehicle, can be suitable for various complex environments, and is high in efficiency and good in adaptability. Meanwhile, due to the existence of some special environments, various accidents can be caused to the unmanned aerial vehicle in work, so that the unmanned aerial vehicle is abnormal in function, and similar abnormal functions comprise abnormal communication functions, abnormal flight functions, abnormal power supply functions and the like. In practical application, it is difficult to find out what abnormality occurs in time, and at this time, if a control plan is not provided, the unmanned aerial vehicle can be disabled and damaged. Disclosure of utility model The utility model provides a multi-element control system suitable for an unmanned aerial vehicle, which aims to solve the problem of insufficient control scheme of the existing unmanned aerial vehicle. In order to achieve the above purpose, the technical scheme adopted by the utility model is as follows: the multi-element control system suitable for the unmanned aerial vehicle comprises a power supply unit, a signal transmission unit, a notification unit and at least two sets of power supply units, wherein the power supply unit comprises a battery, a battery shell, a power supply circuit and a power supply controller, the signal transmission unit comprises an electromagnetic signal converter, a signal processor, a first communication module and a second communication module, the notification unit comprises a light source and a light source controller, the battery is arranged in the battery shell, the power supply controller is connected with and controls the battery to output electric energy through the power supply circuit, the signal processor is used for modulating an electric signal, the electromagnetic signal converter is used for converting the modulated electric signal into a corresponding electromagnetic wave signal, the first communication module is used for outputting the electromagnetic wave signal, the second communication module is respectively connected with the signal processor, the power supply controller and the light source controller, the power supply unit, the signal transmission unit and the notification unit are arranged in the unmanned aerial vehicle, at least two sets of corresponding communication connection between the second communication modules are arranged, and when one of the second communication modules is disconnected, the other sets of controllers, the signal processor and the light source controller is started according to at least one preset function. Further, the battery shell is a combined shell, an opening is formed in one end of the battery shell, a contact point is arranged on the inner side of the opening, and the contact point is connected with the signal transmission unit or the notification unit through a tubular connecting wire and/or a strip connecting wire. Furthermore, openings are respectively arranged on two sides of one end of the battery shell, one opening is connected with a tubular connecting wire, the other opening is connected with a strip connecting wire, and the tubular connecting wire and the strip connecting wire are used for realizing electric connection or communication connection. Further, the notification unit is provided with a combined type protective shell, the light source is a lamp matrix, the upper surface of the protective shell is provided with the lamp matrix and a stripe-shaped concave-convex structure, and the side surface of the protective shell is provided with a connection inlet for connecting the tubular connecting wire and the stripe-shaped connecting wire. Further, the bottoms of the notification unit and the power supply unit are fixed on the rod of the unmanned aerial vehicle through a clamp. Further, the light source controller is used for controlling the lamp matrix to enable the lamps in the lamp matrix to be lightened, changed in brightness and extinguished according to a specified rule. Further, the unmanned aerial vehicle is provided with a third communication module which is in communication connection with the first communication module and/or the second communication module, and the unmanned aerial vehicle transmits signals to be output to the first communication module and/or the second communication module through the third communication module. Further, the first communication module is configured to transmit the signal to be output to the signal processor, the signal processor is configured to process the signal to be output to obtain the modulated electrical signal, the electromagnetic signal converter is configured to