Portable unmanned aerial vehicle self-driving device

Abstract

The utility model discloses a portable unmanned aerial vehicle self-driving device, relates to the technical field of unmanned aerial vehicles, and solves the technical problem that an existing unmanned aerial vehicle self-driving device cannot well meet the requirements of portability and automatic control. The device comprises a suitcase, a remote controller and a self-driving instrument, the remote controller is detachably connected in the suitcase, the self-driving instrument is fixed in the suitcase, and the remote controller is in communication connection with the self-driving instrument; the self-driving instrument is used for issuing a flight instruction to the remote controller; and the remote controller is used for being in communication connection with the unmanned aerial vehicle, controlling the unmanned aerial vehicle through the received flight instruction, and forwarding data returned by the unmanned aerial vehicle to the self-driving instrument. The remote controller and the self-driving instrument are integrated in the suitcase, the portability of the self-driving device of the unmanned aerial vehicle is improved, and the self-driving instrument issues a flight instruction to the remote controller to automatically control the unmanned aerial vehicle.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, in particular to a portable unmanned aerial vehicle self-driving device. Background Art

[0002] With the rapid development of unmanned aerial vehicles, in order to ensure that unmanned aerial vehicles can successfully meet the usage requirements of various tasks, such as taking off urgently to start operations, or downloading data logs in the powered-on state, etc., and to enrich the diversity of unmanned aerial vehicle hangars and application scenarios, a set of fully automatic unmanned aerial vehicle ground control devices is required.

[0003] Existing unmanned aerial vehicle ground control devices come in various types. Currently, the common unmanned aerial vehicle ground control devices on the market are remote controllers and ground control stations. The remote controller is small in size and light in weight, but it requires user operation and can only be operated at close range. The ground control station is large in size and heavy in weight. Although it can perform remote automatic control, it is usually a fixed equipment facility, without mobility, or needs to be transported by vehicle. Existing unmanned aerial vehicle self-driving devices cannot well meet the requirements of both portability and automatic control.

[0004] In the process of implementing the present utility model, the applicant found that there are at least the following problems in the prior art:

[0005] Existing unmanned aerial vehicle self-driving devices cannot well meet the requirements of both portability and automatic control. Summary of the Utility Model

[0006] The purpose of the present utility model is to provide a portable unmanned aerial vehicle self-driving device to solve the technical problem in the prior art that existing unmanned aerial vehicle self-driving devices cannot well meet the requirements of both portability and automatic control. The many technical effects that can be produced by the preferred technical solutions provided by the present utility model are described in detail below.

[0007] To achieve the above object, the present utility model provides the following technical solutions:

[0008] A portable unmanned aerial vehicle self-driving device provided by the present utility model includes a suitcase, a remote controller, and a self-pilot. The remote controller is detachably connected in the suitcase, the self-pilot is fixed in the suitcase, and the remote controller is communicatively connected with the self-pilot; the self-pilot is used to send flight instructions to the remote controller; the remote controller is used to be communicatively connected with an unmanned aerial vehicle, control the unmanned aerial vehicle according to the received flight instructions, and forward the data transmitted back by the unmanned aerial vehicle to the self-pilot.

[0009] Preferably, the suitcase includes an upper shell and a lower shell. The first side of the upper shell is hingedly connected to the first side of the lower shell, and the second side of the upper shell is snap-connected to the second side of the lower shell to form a receiving cavity. A panel is fixed at the opening of the lower shell. The panel includes a groove structure, a power switch, a charging interface, a network port, and a wire passing hole. The groove structure is used to accommodate the remote controller.

[0010] Preferably, it further includes a power supply module and a communication module. The power supply module is connected to the communication module, the autopilot, and the remote controller. The communication module is connected to the autopilot. The power supply module, the communication module, and the autopilot are all fixed on the first surface of the panel. The communication module is used to externally connect to a network cable and / or an internal SIM card to supply network to the autopilot and the remote controller.

[0011] Preferably, a display window is further included on the panel. The display window corresponds to the display screen of the power supply module. The display window is used to view the power display of the display screen.

[0012] Preferably, the power supply module includes a boost module and a voltage stabilizing module. Both the boost module and the voltage stabilizing module are connected to the autopilot.

[0013] Preferably, a heat dissipation module is further included. The heat dissipation module is fixed on the panel and is adjacent to the heat dissipation holes on the groove structure. The heat dissipation module is connected to the power supply module and the autopilot.

[0014] Preferably, an installation part and a fixing sheet metal are further included. The fixing sheet metal is fixedly connected to the upper shell. The installation part is fixedly connected to the fixing sheet metal and corresponds to the groove structure. The installation part is used to install and fix remote controllers of different models.

[0015] Preferably, the remote controller is a micro unmanned aerial vehicle remote controller, a light unmanned aerial vehicle remote controller, a small unmanned aerial vehicle remote controller, a medium-sized unmanned aerial vehicle remote controller, or a large unmanned aerial vehicle remote controller. The antenna structure of the remote controller is a retractable structure or a non-retractable structure.

[0016] Preferably, a TYPE-C output port is provided on the autopilot. The autopilot controls the on / off of the TYPE-C output port through an input level signal to switch between the USB debugging mode and the fast charging mode. When the TYPE-C output port switches to the USB debugging mode, the autopilot can debug the remote controller through a debugging bridge. When the TYPE-C output port switches to the fast charging mode, the autopilot can supply power to the remote controller.

[0017] Preferably, the material of the suitcase is a plastic material or an alloy material.

[0018] Implementing one of the above technical solutions of the present utility model has the following advantages or beneficial effects:

[0019] The present utility model integrates a remote controller and an autopilot in a suitcase, improving the portability of the UAV autopilot device. The autopilot automatically controls the UAV by sending flight instructions to the remote controller. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] In order to more clearly illustrate the technical solutions of the embodiments of the present utility model, the following will briefly introduce the drawings required for the description of the embodiments. Obviously, the following-described drawings are only some embodiments of the present utility model. For those of ordinary skill in the art, without creative efforts, other drawings can be obtained based on these drawings. In the drawings:

[0021] Figure 1 is the first exploded view of the embodiment of the portable UAV autopilot device of the present utility model;

[0022] Figure 2 is the perspective view of the embodiment of the portable UAV autopilot device of the present utility model;

[0023] Figure 3 is the second exploded view of the embodiment of the portable UAV autopilot device of the present utility model.

[0024] In the figure: 1, suitcase; 11, upper shell; 12, lower shell; 13, panel; 131, groove structure; 132, power switch; 133, charging interface; 134, network port; 135, wire passing hole; 136, display window; 137, heat dissipation hole; 14, mounting part; 15, fixed sheet metal; 2, remote controller; 3, autopilot; 4, power supply module; 41, display screen; 5, communication module; 6, heat dissipation module; 7, boost module. DETAILED DESCRIPTION OF THE EMBODIMENTS

[0025] In order to make the purpose, technical solutions and advantages of the present utility model clearer, the following various exemplary embodiments will refer to the corresponding drawings, which form a part of the exemplary embodiments, and describe various exemplary embodiments that may be adopted to implement the present utility model. Unless otherwise indicated, the same numbers in different drawings represent the same or similar elements. The embodiments described in the following exemplary embodiments do not represent all embodiments consistent with the present disclosure. It should be understood that they are only examples of processes, methods and devices, etc. consistent with some aspects of the present utility model disclosed in the appended claims in detail. Other embodiments may also be used, or structural and functional modifications may be made to the embodiments listed herein without departing from the scope and essence of the present utility model.

[0026] In the description of the present utility model, it should be understood that the terms "center", "longitudinal", "lateral", etc. indicate the orientation or positional relationship based on the orientation shown in the drawings. These are only for the convenience of describing the present utility model and simplifying the description, rather than indicating or implying that the indicated elements must have a specific orientation, be constructed and operated in a specific orientation. The terms "first", "second", etc. are only used for descriptive purposes and cannot be understood as indicating or implying relative importance or implicitly specifying the quantity of the indicated technical features. The meaning of the term "plurality" is two or more. The terms "connected" and "connected to" should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, an integral connection, a mechanical connection, an electrical connection, a communication connection, a direct connection, an indirect connection through an intermediate medium. It can be the communication inside two elements or the interaction relationship between two elements. The term "and / or" includes any and all combinations of one or more of the related listed items. For those of ordinary skill in the art, the specific meanings of the above terms in the present utility model can be understood according to specific circumstances.

[0027] In order to illustrate the technical solution of the present utility model, the following will be described through specific embodiments, and only the parts related to the embodiments of the present utility model are shown.

[0028] Embodiment 1:

[0029] As Figure 1 shown, the present utility model provides a portable UAV self-driving device, which includes a carrying case 1, a remote controller 2 and an autopilot 3. The remote controller 2 is detachably connected in the carrying case 1, the autopilot 3 is fixed in the carrying case 1, and the remote controller 2 is communicatively connected to the autopilot 3. The autopilot 3 is used to send flight instructions to the remote controller 2. The remote controller 2 is used to communicate with the UAV, control the UAV according to the received flight instructions, and forward the data transmitted back by the UAV to the autopilot 3. Specifically, the portable UAV self-driving device is communicatively connected to the cloud. The cloud sends tasks to the autopilot 3. After receiving the tasks sent by the cloud, the autopilot 3 sends flight instructions to the remote controller 2 through the TCP / IP protocol. After receiving the flight instructions, the remote controller 2 controls the UAV according to the flight instructions. The data collected by the UAV during the cruise is transmitted back to the remote controller 2, and the remote controller 2 uploads the obtained data to the autopilot 3. The autopilot 3 sends the transmission status data and flight results to the cloud.

[0030] The present utility model integrates the remote controller 2 and the autopilot 3 in the carrying case 1, improves the portability of the UAV self-driving device, and automatically controls the UAV by the autopilot 3 sending flight instructions to the remote controller 2.

[0031] As an optional implementation manner, as Figure 2As shown in the figure, the suitcase 1 includes an upper shell 11 and a lower shell 12. The first side of the upper shell 11 is hingedly connected to the first side of the lower shell 12, and the second side of the upper shell 11 is snap-connected to the second side of the lower shell 12 to form a receiving cavity. A panel 13 is fixed at the opening of the lower shell 12. The panel 13 includes a groove structure 131, a power switch 132, a charging interface 133, a network port 134, and a wire passing hole 135. The groove structure 131 is used to accommodate the remote controller 2. Specifically, the material of the panel 13 is a metal material, preferably an aluminum alloy material. The first side of the upper shell 11 is hingedly connected to the first side of the lower shell 12. The hinge connection includes hinge connection, bearing connection, pin connection, etc. The second side of the upper shell 11 is snap-connected to the second side of the lower shell 12, which is convenient to open or close the suitcase 1 through the snap connection. When the suitcase 1 is opened, the first side of the upper shell 11 is connected to the first side of the lower shell 12, which is convenient for use. For example, when the suitcase 1 is closed, it is convenient for the upper shell 11 and the lower shell 12 to correspond. The upper shell 11 is connected to the lower shell 12 to form a receiving cavity for accommodating functional modules such as the remote controller 2 and the autopilot 3. The panel 13 is fixed at the opening of the lower shell 12, which is convenient to fix functional modules such as the autopilot 3, the power supply module 4, the communication module 5, and the heat dissipation module 6 on the panel 13 and at the same time, they are encapsulated in the lower shell 12 by the panel 13. The groove structure 131 on the panel 13 is used to accommodate the remote controller 2 fixed on the upper shell 11, making the internal structure of the suitcase 1 compact, reducing the volume, and facilitating carrying. The power switch 132 is provided on the panel 13 to facilitate the user to start the portable UAV autopilot device. The charging interface 133 provided on the panel 13 is connected to the power supply module 4 (described below), which is convenient for the portable UAV autopilot device to be connected to an external power supply to charge the power supply module 4. The network port 134 provided on the panel 13 is connected to the communication module 5 (described below), which is convenient for the portable UAV autopilot device to externally connect a network cable through the network port 134 to supply network to the communication module 5. The signal line of the line between the remote controller 2 and the communication module 5 can pass through the wire passing hole 135, which is convenient for the remote controller 2 to be connected to the communication module 5.

[0032] As an optional implementation manner, such as Figure 3As shown in the figure, it further includes a power supply module 4 and a communication module 5. The power supply module 4 is connected to the communication module 5, the autopilot 3, and the remote controller 2. The communication module 5 is connected to the autopilot 3. The power supply module 4, the communication module 5, and the autopilot 3 are all fixed on the first surface of the panel 13. The communication module 5 is used to externally connect an Ethernet cable and / or internally install a SIM card to supply network to the autopilot 3 and the remote controller 2. Specifically, the power supply module 4 is used to supply power to each functional module in the portable UAV autopilot device. For example, since the power supply module 4 is connected to the communication module 5, the autopilot 3, and the remote controller 2, it can supply power to the communication module 5, the autopilot 3, and the remote controller 2. The power supply module 4 is fixed on the first surface of the panel 13 through a battery mounting bracket. The communication module 5 is arranged adjacent to the power supply module 4, and the communication module 5 is fixedly connected to the panel 13 through the battery mounting bracket. The autopilot 3 is also fixed on the first surface of the panel 13. The first surface of the panel 13 faces the inner bottom of the lower housing 12. By integrating the autopilot 3, the power supply module 4, and the communication module 5 inside the lower housing 12 and shielding them with the panel 13, it can protect each functional module integrated inside the lower housing 12 and improve the service life of the portable UAV autopilot device. The power supply module 4 is connected to the power switch 132 and the charging interface 133 provided on the panel 13. The power supply module 4 is connected to an external power supply through the charging interface 133 to realize the charging of the power supply module 4 and store the power. The power switch 132 can control the on-off between the power supply module 4, the communication module 5, the autopilot 3, and the remote controller 2 to realize the start or shutdown of the portable UAV autopilot device. When the power switch 132 connects the circuits between the power supply module 4, the communication module 5, the autopilot 3, and the remote controller 2, the portable UAV autopilot device can be turned on. Conversely, the portable UAV autopilot device can be turned off. The communication module 5 can externally connect an Ethernet cable and / or internally install a SIM card to provide network services to the autopilot 3 and the remote controller 2. The communication module 5 is connected to the remote controller 2 by wire to supply network to the remote controller 2 in a wired manner. The communication module 5 is preferably a router. By integrating the power supply module 4 and the communication module 5 inside the portable UAV autopilot device, it can save the resources and time for deploying external power supplies and external networks and has higher efficiency.

[0033] As an optional implementation, as Figure 1 shown in the figure, the panel 13 further includes a display window 136. The display window 136 corresponds to the display screen 41 of the power supply module 4. The display window 136 is used to view the power display on the display screen 41. Specifically, a display window 136 is provided on the panel 13. When the power supply module 4 is fixed on the panel 13, the display screen 41 is arranged corresponding to the display window 136 to ensure that the user can view the power information displayed on the display screen 41 through the display window 136. The display window 136 and the display screen 41 of the power supply module 4 are matched with each other to ensure that the display screen 41 can be completely exposed inside the display window 136 without blocking the display screen 41.

[0034] As an optional implementation, as Figure 3 shown, the power supply module 4 includes a boost module 7 and a voltage stabilization module. Both the boost module 7 and the voltage stabilization module are connected to the autopilot 3. Specifically, the boost module 7 is connected to the TYPE-C input port of the autopilot 3 through a DC-to-PD module (DC charging to fast charging module). The Type-C output port of the autopilot 3 is connected to the remote controller 2. A switching device of the patent with the publication number CN117375152A is integrated on the autopilot 3. This switching device is connected between the TYPE-C input port and the Type-C output port, and controls the on / off between the TYPE-C input port and the Type-C output port through the switching device integrated on the autopilot 3 to achieve full-power charging or prohibited charging of the remote controller 2. The boost module 7 can boost the 12V voltage output by the power supply module 4 to 24V voltage. The voltage stabilization module is arranged between the power supply module 4 and the autopilot 3, and the voltage stabilization module can ensure the reliable power input of the autopilot 3. The power supply module provides a 12V voltage to the autopilot 3. Both the boost module 7 and the voltage stabilization module are fixed on the first surface of the panel 13.

[0035] As an optional implementation, as Figure 3 shown, it further includes a heat dissipation module 6. The heat dissipation module 6 is fixed on the panel 13 and is adjacent to the heat dissipation holes 137 on the groove structure 131. The heat dissipation module 6 is connected to the power supply module 4 and the autopilot 3. Specifically, the heat dissipation module 6 is connected to the power supply module 4, and the power supply module 4 powers the heat dissipation module 6 to ensure that the heat dissipation module 6 can operate. The heat dissipation module 6 is connected to the autopilot 3, and the heat dissipation module 6 is started by controlling the autopilot 3. The heat dissipation module 6 includes at least two heat dissipation fans. Each heat dissipation fan is fixed on the panel 13 and is adjacent to the heat dissipation holes 137 on the groove structure 131, and is used to dissipate the heat generated when other devices such as the power supply module 4 and the autopilot 3 fixed on the first surface of the panel 13 work to the outside, so as to adjust the temperature of the internal working environment of the portable UAV autopilot device and ensure the safe operation of each functional module. The number of heat dissipation holes 137 is multiple, and they are arranged on the side wall and the bottom of the groove structure 131.

[0036] As an optional implementation, as Figure 1As shown in the figure, it further includes a mounting member 14 and a fixing sheet metal 15. The fixing sheet metal 15 is fixedly connected to the upper shell 11. The mounting member 14 is fixedly connected to the fixing sheet metal 15 and corresponds to the groove structure 131. The mounting member 14 is used to mount and fix remote controllers 2 of different models. Specifically, the fixing sheet metal 15 is fixed on the upper shell 11, which is convenient for mounting the remote controller 2 on the upper shell 11. The mounting member 14 is fixed on the upper fixing sheet metal 15 through connecting parts such as screws or bolts, which is convenient for supporting and fixing the remote controller 2. Mounting holes adapted to remote controllers 2 of different models are provided at different positions of the mounting member 14. Different remote controllers 2 of different models can be switched and mounted through different mounting holes to adapt to different models of unmanned aerial vehicles. At the same time, different remote controllers 2 of different models can also be switched and mounted by replacing different mounting members 14. The mounting member 14 corresponds to the groove structure 131, ensuring that when the upper shell 11 is closed on the lower shell 12, the remote controller 2 fixed on the mounting member 14 can be placed in the groove structure 131, ensuring that the suitcase 1 can be closed, and at the same time avoiding hitting the remote controller 2 and damaging the remote controller 2. Accommodating the remote controller 2 into the groove structure 131 makes the internal structure of the suitcase 1 compact, which can reduce the volume of the suitcase 1 and is convenient for carrying.

[0037] As an optional implementation manner, the remote controller 2 is a micro unmanned aerial vehicle remote controller, a light unmanned aerial vehicle remote controller, a small unmanned aerial vehicle remote controller, a medium unmanned aerial vehicle remote controller or a large unmanned aerial vehicle remote controller, and the antenna structure of the remote controller 2 is a retractable structure or a non-retractable structure. Specifically, different models of remote controllers 2 can be assembled inside the portable unmanned aerial vehicle self-driving device according to requirements to adapt to different models of unmanned aerial vehicles and meet the usage requirements of the portable unmanned aerial vehicle self-driving device in different scenarios. By providing mounting holes both above and below the fixing sheet metal 15, the mounting member 14 of the small unmanned aerial vehicle remote controller 2 or the mounting member 14 of the light unmanned aerial vehicle remote controller is fixed through screws or bolts on the corresponding mounting holes, and then the corresponding remote controller 2 is fixed through the mounting member 14. By removing the fastened screws or bolts, the mounting member 14 can be removed, which is convenient for quickly switching and mounting different remote controllers 2. The light unmanned aerial vehicle remote controller is preferably the remote controller 2 of DJI RC Pro, and the small unmanned aerial vehicle remote controller 2 is preferably DJI RCPlus. The antenna structure of the remote controller 2 can be retracted to enhance the signal.

[0038] As an alternative implementation, the autopilot 3 is provided with a TYPE-C output port. The autopilot 3 controls the on / off of the TYPE-C output port through an input level signal, which is used to switch between the USB debugging mode and the fast charging mode. When the TYPE-C output port is switched to the USB debugging mode, the autopilot 3 can debug the remote controller 2 through the debugging bridge. When the TYPE-C output port is switched to the fast charging mode, the autopilot 3 can supply power to the remote controller 2. Specifically, the Type-C output port of the autopilot 3 is connected to the remote controller 2. The autopilot 3 inputs high and low level signals to control the on / off of the wiring between the TYPE-C output port and the TYPE-C input port, so as to switch the TYPE-C output port to support the PD protocol (fast charging protocol) and be in the fast charging mode, or the TYPE-C output port supports single data transmission and is in the USB debugging mode. When the TYPE-C output port is switched to the USB debugging mode, the autopilot 3 debugs the remote controller 2 through the debugging bridge and uses ADB (Android debugging mode) through the TYPE-C output port of the USB debugging mode, such as instructions to open an APP. When the TYPE-C output port is switched to the fast charging mode, the autopilot 3 can perform fast charging on the remote controller 2.

[0039] As an alternative implementation, the material of the suitcase 1 is a plastic material or an alloy material. Specifically, when the material of the suitcase 1 is a plastic material, it is preferably a PP material with an IP67 protection level, which has good waterproof, dustproof and moisture-proof characteristics and can withstand vibrations and collisions during transportation. At the same time, it also has the characteristics of light weight and is convenient to carry. The alloy material of the suitcase 1 has the advantages of high strength and good wear resistance.

[0040] The embodiment is only a special case and does not indicate that the present utility model has only such an implementation manner.

[0041] The above are only the preferred embodiments of the present utility model. Those skilled in the art know that without departing from the spirit and scope of the present utility model, various changes or equivalent replacements can be made to these features and embodiments. In addition, under the teaching of the present utility model, these features and embodiments can be modified to adapt to specific situations and materials without departing from the spirit and scope of the present utility model. Therefore, the present utility model is not limited by the specific embodiments disclosed herein, and all embodiments falling within the scope of the claims of this application belong to the protection scope of the present utility model.

Claims

1. A portable drone self-driving device, characterized in that: The invention comprises a suitcase (1), a remote controller (2) and an autopilot (3), wherein the remote controller (2) is detachably connected to the suitcase (1), the autopilot (3) is fixed to the suitcase (1), and the remote controller (2) is communicatively connected to the autopilot (3); the autopilot (3) is used to send flight instructions to the remote controller (2); the remote controller (2) is communicatively connected to an unmanned aerial vehicle (UAV), controls the UAV by receiving the flight instructions, and forwards data sent back by the UAV to the autopilot (3).

2. The portable drone self-driving device according to claim 1, characterized in that: The suitcase (1) comprises an upper shell (11) and a lower shell (12); a first side of the upper shell (11) is hingedly connected to a first side of the lower shell (12); a second side of the upper shell (11) is snap-connected to a second side of the lower shell (12) to form a receiving cavity; a panel (13) is fixed at an opening of the lower shell (12); the panel (13) comprises a groove structure (131), a power switch (132), a charging interface (133), a network port (134) and a wire hole (135); the groove structure (131) is used to receive the remote control (2).

3. The portable drone self-driving device according to claim 2, characterized in that: It also comprises a power supply module (4) and a communication module (5), wherein the power supply module (4) is connected to the communication module (5), the autopilot (3) and the remote controller (2), and the communication module (5) is connected to the autopilot (3); the power supply module (4), the communication module (5) and the autopilot (3) are all fixed on the first surface of the panel (13); the communication module (5) is used to connect an external network cable and / or a built-in SIM card to supply network to the autopilot (3) and the remote controller (2).

4. The portable drone self-driving device according to claim 3, characterized in that: The panel (13) also includes a display window (136), the display window (136) corresponds to the display screen (41) of the power supply module (4), and the display window (136) is used to view the power display on the display screen (41).

5. The portable drone self-driving device according to claim 4, characterized in that: The power supply module (4) comprises a voltage boost module (7) and a voltage stabilizing module, and both the voltage boost module (7) and the voltage stabilizing module are connected to the autopilot (3).

6. The portable drone self-driving device according to claim 4, characterized in that: It also comprises a heat dissipation module (6), the heat dissipation module (6) being fixed on the panel (13) and arranged adjacent to the heat dissipation hole (137) on the groove structure (131); the heat dissipation module (6) being connected to the power supply module (4) and the autopilot (3).

7. The portable drone self-driving device according to claim 2, characterized in that: It also includes a mounting member (14) and a fixing sheet metal (15), wherein the fixing sheet metal (15) is fixedly connected to the upper housing (11), the mounting member (14) is fixedly connected to the fixing sheet metal (15), and the mounting member (14) corresponds to the groove structure (131); the mounting member (14) is used to mount and fix remote controllers (2) of different models.

8. The portable UAV self-driving device according to claim 7, characterized in that: The remote controller (2) is a micro UAV remote controller, a light UAV remote controller, a small UAV remote controller, a medium UAV remote controller or a large UAV remote controller, and the antenna structure of the remote controller (2) is a retractable structure or a non-retractable structure.

9. The portable drone self-driving device according to claim 1, characterized in that: The autopilot (3) is provided with a TYPE-C output port, and the autopilot (3) controls the on and off of the TYPE-C output port through an input level signal, so as to switch between a USB debugging mode and a fast charging mode; when the TYPE-C output port is switched to the USB debugging mode, the autopilot (3) can debug the remote control (2) through a debugging bridge; and when the TYPE-C output port is switched to the fast charging mode, the autopilot (3) can supply power to the remote control (2).

10. The portable UAV self-driving device according to any one of claims 1 to 9, characterized in that: The suitcase (1) is made of plastic or alloy.

Images