Vehicle-mounted unmanned aerial vehicle swarm launching control system and method

Abstract

The invention discloses a vehicle-mounted unmanned aerial vehicle swarm launching control system and method in the technical field of unmanned aerial vehicles, and the system comprises a master control platform, a launching controller, a launching device, an energy storage device, a variable-frequency driving power supply, a signal wall box and a large-screen display which are integrated on a vehicle-mounted platform. The master control platform is connected with the energy storage device, the signal box, the large-screen display and the emission controller, the emission controller is connected with the emission device and the variable-frequency driving power supply, the variable-frequency driving power supply is connected with the energy storage device, and the signal box is connected with the antenna; a vehicle is used as a mobile master control platform, charging and emission control are carried out on an unmanned aerial vehicle swarm, good environmental adaptability is achieved, in order to improve the reliability in a complex environment, modular reliability design is further carried out, and the adaptability of the system provided by the invention in the complex and special environment is further enhanced; the platform has the advantages of being flexible, good in concealment, high in universality, good in reliability, low in use cost and the like.

Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicles, and in particular to a vehicle-mounted unmanned aerial vehicle swarm launch control system and method. Background Art

[0002] With the maturity of drone technology, drone swarm technology has emerged and has become a research hotspot in recent years. Drone swarm refers to a group system composed of a large number of drones through self-organization and collaboration. They can complete complex tasks through mutual cooperation, just like bee swarms and bird flocks in nature.

[0003] Drone swarms have many advantages. First, in terms of mission execution efficiency, multiple drones working together can greatly improve the speed of mission completion. For example, in large-scale search and rescue missions, drone swarms can search different areas at the same time, and can cover a larger area in a shorter time than a single drone. Secondly, in terms of mission adaptability, swarms are more robust. When some drones fail or are attacked, the mission execution capability of the entire swarm will not be completely lost, and other drones can automatically adjust task allocation and flight paths to continue to complete the mission. In addition, drone swarms excel in functional diversity. Drones of different types and functions can be combined into clusters to achieve the integrated execution of multiple functions such as reconnaissance, strike, and communication relay.

[0004] As a mobile launch and control carrier for UAVs, the vehicle-mounted platform has unique advantages and important application value.

[0005] From the perspective of mobility, vehicles can move quickly under different terrain and environmental conditions, breaking through the geographical limitations of fixed base stations. Whether in natural terrain such as mountains, hills, and plains, or in artificial environments such as urban streets and rural trails, the vehicle-mounted drone swarm launch control system can quickly reach the vicinity of the mission designated area, greatly shortening the time interval from drone deployment to mission execution. For example, in border control tasks, the vehicle-mounted system can patrol along the border line and immediately launch a drone swarm for reconnaissance when an abnormal situation is found, so as to keep abreast of border dynamics and effectively prevent illegal border crossings.

[0006] In terms of integration, the vehicle provides a multifunctional integrated platform for the drone swarm. The vehicle can carry the drone's charging equipment, spare batteries, maintenance tools, and various data processing and storage devices. This not only facilitates the energy replenishment and equipment maintenance of the drone during the mission, but also enables on-site processing, analysis and storage of the data collected by the drone, improving the timeliness and security of the data. At the same time, the vehicle-mounted platform can also integrate communication equipment, such as satellite communication terminals, microwave communication equipment, etc., to enhance the communication capabilities between the drone and the control center, and ensure the stability and reliability of data transmission in complex environments.

[0007] In addition, the vehicle-mounted platform also has certain advantages in terms of concealment and protection. In military applications, the vehicle can use terrain and objects for concealment and camouflage to reduce the probability of being discovered by the enemy. At the same time, the vehicle's own armor protection and other measures can to a certain extent protect the drone swarm launch control system and operators in the vehicle from enemy fire attacks or harsh environments.

[0008] In order to improve the ability of a vehicle-mounted UAV launch and control platform to work in various outdoor environments, the present invention provides a vehicle-mounted UAV swarm launch and control system and method. Summary of the invention

[0009] The purpose of this section is to summarize some aspects of the embodiments of the present invention and briefly introduce some preferred embodiments. Some simplifications or omissions may be made in this section and the specification abstract and the invention title of the present invention to avoid blurring the purpose of this section, the specification abstract and the invention title, and such simplifications or omissions cannot be used to limit the scope of the present invention.

[0010] Therefore, the purpose of the present invention is to provide a vehicle-mounted UAV swarm launch control system and method, which uses the vehicle as a mobile general control platform to charge and control the launch of the UAV swarm, has good environmental adaptability, and in order to improve the reliability in complex environments, a modular reliability design is also carried out to further enhance the adaptability of the system provided by the present invention in complex and special environments; the platform has the advantages of mobility, good concealment, strong versatility, good reliability, and low cost of use.

[0011] In order to solve the above technical problems, the present invention provides a vehicle-mounted unmanned aerial vehicle swarm launch control system and method, adopting the following technical scheme: including a master control platform integrated on the vehicle-mounted platform, a launch controller, a launch device, an energy storage device, a variable frequency drive power supply, a signal wall box and a large-screen display, the master control platform is connected to the energy storage device, the signal wall box, the large-screen display and the launch controller, the launch controller is connected to the launch device and the variable frequency drive power supply, the variable frequency drive power supply is connected to the energy storage device, and the signal wall box is connected to the antenna.

[0012] Optionally, the launching device includes a launching motor, a launching frame mounting seat and an electromechanical lock, and the launching frame mounting seat is fixedly mounted on the vehicle-mounted platform.

[0013] Optionally, the energy storage device stores electrical energy, and the electrical energy storage includes a high-performance battery pack and a supercapacitor.

[0014] Optionally, the variable frequency drive power supply is used to convert the electric energy of the energy storage device into a form of electric energy used by the transmitting motor, and the variable frequency drive power supply adjusts the output electric power according to the power requirements of the transmitting motor in different transmitting stages.

[0015] Optionally, the signal wall box includes a filtering circuit.

[0016] Optionally, the large-screen display is used to display the current status of the UAV in real time, including the speed and current of the transmitting motor, the remaining energy of the energy storage device, and the system operation mode and task progress, and various operation instructions are input to the master control platform through the touch operation interface equipped by the large-screen display or an external input device.

[0017] Optionally, the launch controller controls data communication between the launch device and the master control platform, and at the same time adjusts the launch angle of the vehicle-mounted UAV, performs closed-loop control of the drive power supply, launches the UAV, and resets the launch motor through the launch stand mounting bracket, launch motor, electromechanical lock, and variable frequency drive power supply.

[0018] Optionally, a vehicle-mounted UAV swarm launch control method is also included, which specifically includes the following steps:

[0019] Step S1: First, perform a system self-test to conduct a comprehensive self-test of the entire system, including checking whether each hardware component is working properly, whether the software system is running stably, and whether the communication link of the system is unobstructed, ensuring that data can be normally exchanged between each subsystem;

[0020] Step S2: Then query the status of the vehicle-mounted platform and the launcher, check the physical status of the vehicle-mounted platform, including the stability of the platform and whether it is in a suitable launch position, check whether the mechanical structure of the launcher is intact, including whether the launcher mounting base is stable and whether the guide rail is smooth, verify whether various electronic equipment on the launch motor is working properly, and obtain real-time status data;

[0021] Step S3: Sending a launch ready instruction, and the launch device continuously monitors whether the launch ready instruction is received;

[0022] Step S4: After receiving the launch ready instruction, first release the motor lock of the launcher mounting seat, and adjust the angle of the launcher mounting seat until it meets the angle requirement for UAV launch;

[0023] Step S5: The launch motor detects whether there is a drone stored in the launch position, and reports the storage position without a drone to the launch controller. The launch controller issues a control instruction to the variable frequency drive power supply, activates the variable frequency drive power supply, and supplies power to the position of the drone to be launched according to the control instruction, while the launch controller itself is ready to launch;

[0024] Step S6: Sending a launch command. When the launch device has completed all preparations and is in a ready state, the master control platform sends a launch command to the launch device. The launch command contains key information about the launch mission, including the launch initial velocity and launch angle parameters pre-set according to the mission requirements of the UAV and the flight path planning;

[0025] Step S7: closed-loop control of the variable frequency drive power supply. After receiving the transmission command, the control unit inside the variable frequency drive power supply starts to work. The control unit will perform closed-loop control according to the received command parameters. The variable frequency drive power supply monitors the output state in real time and adjusts it according to the difference with the set target.

[0026] Step S8: After the variable frequency drive power supply completes parameter adjustment and preparation, it starts to energize the transmitting motor. As the current passes through the winding of the transmitting motor, the motor generates a strong electromagnetic force according to the principle of electromagnetic induction. The electromagnetic force acts on the structural components connected to the drone body. Since the direction of the electromagnetic force is consistent with the exit direction of the drone body, the body begins to accelerate under the impetus of the electromagnetic force.

[0027] Step S9: The launch motor continuously provides electromagnetic force to push the drone body to accelerate in the launch motor. During the acceleration process, the speed of the drone increases continuously until it reaches the initial speed required by the master control platform command. When the drone reaches the initial speed, it leaves the launch device exit at the initial speed and enters the flight phase. At this time, the drone's own flight control system starts to work and adjusts the flight attitude and altitude parameters to perform subsequent flights according to the preset flight mission.

[0028] Step S10: Report the detachment status of the drone. After the drone obtains initial power and leaves the launcher mounting seat, it is necessary to report the successful launch of the drone, and at the same time report the initial speed, angle, and energy consumption data of the drone;

[0029] Step S11: The launch motor is reset. After the UAV safely leaves the launch device, the actuator in the launch motor returns to the launch start position under the control of electromagnetic force, and the launch device re-enters the launch waiting state, waiting for instructions for the next launch.

[0030] In summary, the present invention includes at least one of the following beneficial effects:

[0031] The vehicle is used as a mobile general control platform to charge and launch the drone swarm, which has good environmental adaptability. In order to improve the reliability in complex environments, a modular design is carried out, which further enhances the adaptability of the system provided by the present invention in complex and special environments. The platform has the advantages of flexibility, good concealment, strong versatility, good reliability, and low cost of use. BRIEF DESCRIPTION OF THE DRAWINGS

[0032] In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the accompanying drawings required for describing the embodiments will be briefly introduced below. Obviously, the accompanying drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other accompanying drawings can be obtained based on these accompanying drawings without paying creative work.

[0033] Figure 1 This is a schematic diagram of the framework of the vehicle-mounted UAV swarm launch control system of the present invention;

[0034] Figure 2 This is a diagram of the architecture of the transmitting controller of the present invention;

[0035] Figure 3 This is a flow chart of the vehicle-mounted UAV swarm launch control method of the present invention. DETAILED DESCRIPTION

[0036] The following will combine the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all the embodiments. All other embodiments obtained by ordinary technicians in this field without creative work based on the embodiments of the present invention belong to the scope of protection of the present invention.

[0037] In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "top / bottom" and the like indicate positions or positional relationships based on the positions or positional relationships shown in the drawings, and are only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific position, be constructed and operated in a specific position, and therefore cannot be understood as limiting the present invention. In addition, the terms "first" and "second" are used for descriptive purposes only and cannot be understood as indicating or implying relative importance.

[0038] In the description of the present invention, it should be noted that, unless otherwise clearly specified and limited, the terms "installed", "provided with", "mounted / connected", "connected", etc. should be understood in a broad sense. For example, "connected" can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be indirectly connected through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.

[0039] Embodiment 1

[0040] Reference Figure 1 The present invention discloses a vehicle-mounted unmanned aerial vehicle swarm launch control system, comprising a master control platform, a launch controller, a launch device, an energy storage device, a variable frequency drive power supply, a signal wall box and a large-screen display integrated on the vehicle-mounted platform, the master control platform is connected to the energy storage device, the signal wall box, the large-screen display and the launch controller, the launch controller is connected to the launch device and the variable frequency drive power supply, the variable frequency drive power supply is connected to the energy storage device, and the signal wall box is connected to an antenna.

[0041] The master control platform is the command center of the vehicle-mounted UAV swarm launch system, responsible for receiving the operator's instructions and converting them into actions that the UAV can perform. It is connected to the signal wall box, the large-screen display and the launch controller. The signal wall box provides wireless or wired communication to transmit the operator's instructions. The large-screen display displays the real-time status of each component of the system described in the present invention. The launch controller controls the communication data between the launch device and the master control platform, and at the same time undertakes the functions of communication with the launch device, power supply of the launch device, battery activation, launch permission, etc., so as to complete the continuous launch of the UAV swarm. The launch controller is connected to the launch device and the variable frequency drive power supply. The variable drive power supply converts direct current into alternating current required by the launch device, and controls the motor speed in the launch device and the direction of the launch frame mounting seat. The launch device is responsible for converting electrical energy into mechanical energy and providing initial lift to the UAV. The launch frame mounting seat in the launch device is designed as an adjustable inclination structure, which is used for the early verification of the UAV launch, so as to facilitate the rapid adjustment of the launch inclination for verification.

[0042] In detail, in this embodiment, the launch device includes a launch motor, a launcher mounting seat and an electromechanical lock, etc. The launch motor converts energy forms such as electrical energy into mechanical energy to provide initial lift to the drone, so that the drone can quickly obtain sufficient speed, overcome its own gravity and air resistance, and thus smoothly leave the ground and enter the flight state. Drones of different types, sizes and weights have different requirements for take-off power; the launcher mounting seat provides a stable and reliable drone installation foundation for the entire launch system, and the launcher mounting seat is firmly installed on the vehicle platform to ensure that the entire launch device will not shake or shift during the launch of the drone. Preferably, the launcher mounting seat can be accurately positioned and calibrated so that the drone can be in an accurate initial posture and position before launching. The launcher mounting seat is provided with corresponding positioning slots, adjustment devices, etc., which can adjust the parameters such as the horizontality, pitch angle and azimuth angle of the launcher mounting seat to ensure that the drone is launched according to the predetermined flight trajectory.

[0043] In detail, in this embodiment, the energy stored in the energy storage device can be quickly released at the moment of the UAV launch to meet the demand for high-power energy during launch. Common forms of energy storage include electrical energy storage (such as high-performance battery packs, supercapacitors, etc.). Preferably, the energy storage device of the present invention can adjust the stored energy according to actual needs to ensure that the energy released during each launch is relatively stable and meets the take-off conditions of the UAV. At the same time, after completing a launch, energy can be replenished through a corresponding energy supply device (such as a charging circuit) to prepare for the next launch and ensure that the launch system can continue to operate.

[0044] In detail, in this embodiment, the variable frequency drive power supply converts the power supply of the on-board energy storage device into an electric energy form suitable for use by electrical components such as the transmitting motor, including adjusting parameters such as voltage and frequency. For example, different models of transmitting motors may require different AC frequencies and voltages to achieve optimal performance. The variable frequency drive power supply can convert the input DC power into AC power of corresponding specifications according to actual needs, provide stable and suitable electric energy for the transmitting motor, ensure the normal operation of the motor, and exert the power output capacity as it should. Further, according to the power requirements of the transmitting motor at different launch stages, the variable frequency drive power supply can flexibly adjust the output electric power. In the early stage of the UAV launch, the transmitting motor may need to quickly reach a higher speed to provide a larger initial thrust. At this time, the variable frequency drive power supply will increase the output power accordingly; and when the UAV is close to leaving the launch device and is about to enter a stable flight state, it can reduce the power output, so that the motor speed transitions smoothly, avoiding the adverse effects of power mutation on the UAV flight posture. Through precise power regulation, the working performance of the transmitting motor is optimized, and the energy efficiency and reliability of the entire launch system are improved.

[0045] In detail, in this embodiment, the signal wall box receives various control signals from the master control platform, the transmitting controller and other components, and accurately forwards these signals to the corresponding receiving components, such as the transmitting device, the energy storage device, the transmitting controller, the antenna, etc., according to the preset lines and rules. During the signal transmission process, the signal wall box can enhance the signal processing, improve the signal strength and anti-interference ability, and ensure that the signal can still be accurately and stably transmitted under the influence of the complex vehicle-mounted electromagnetic environment and external interference factors. Furthermore, the signal wall box also has certain signal protection functions, such as filtering out external clutter signals, electromagnetic interference, etc. by setting filtering circuits, etc., to prevent these bad signals from damaging the normal control signals and communication signals in the system, and to ensure the reliability and accuracy of communication between components.

[0046] In detail, in this embodiment, the large-screen display is an important interface for human-computer interaction in the present invention, and can display various key information of the vehicle-mounted UAV swarm launch system in an intuitive and clear visual manner. The current state of the UAV can be displayed in real time, and the working state of each component of the launch system provided by the present invention can also be presented, such as the speed and current of the launch motor, the remaining energy of the energy storage device, and the operation mode and task progress of the entire system, so that the operator can understand the overall operation status of the system at a glance. The operator can input various operation instructions to the master control platform through the touch operation interface equipped by the large-screen display or an external input device (such as a keyboard, mouse, etc.), such as starting or pausing the UAV swarm launch mission, adjusting the flight plan of the UAV, modifying the relevant parameters of the launch system, etc., to achieve convenient and flexible control of the entire system, so as to facilitate timely decision-making and adjustment according to actual conditions, and ensure that the vehicle-mounted UAV swarm launch system can complete various tasks efficiently and safely.

[0047] In detail, in this embodiment, the master control platform, as the core command unit of the vehicle-mounted UAV swarm launch system of the present invention, is responsible for comprehensive planning of the tasks of the UAV swarm. It reasonably arranges the flight path, flight altitude, operation time and coordination mode between each UAV according to the preset task objectives, ensuring that the entire swarm can efficiently complete the task. At the same time, it can also dynamically schedule the task according to the actual situation. Collect a large amount of data information feedback from each UAV and other components of the launch system, including the real-time flight status data of the UAV (such as position, speed, attitude, etc.), the working status parameters of each component (such as the current, voltage of the launch motor, the residual energy of the energy storage device, etc.), and integrate and sort out these complex data, and use the corresponding algorithm to analyze, extract valuable content from it, judge whether the UAV has an abnormal flight condition, whether each link of the launch system is operating normally, etc., and provide a strong basis for the decision-making of the operator; the master control platform communicates and interacts with the launch controller, signal wall box and other components to ensure the accurate issuance of instructions and the orderly coordination of various parts. For example, when it is necessary to launch a swarm of drones, the master control platform issues a launch command sequence to the launch controller, and coordinates the energy storage device, variable frequency drive power supply, etc. to provide corresponding support for the launch as planned, ensuring the smooth progress of the entire launch process and the continuity of subsequent drone swarm flight operations.

[0048] The architecture of the transmitter controller is as follows Figure 2 As shown, the launch controller controls the data communication between the launch device and the vehicle-mounted platform (master control platform), and at the same time, the vehicle-mounted UAV is adjusted for launch angle, closed-loop control of the drive power supply, UAV launch, and reset of the launch motor through the launch stand mounting seat, launch motor, electromechanical lock, and variable frequency drive power supply to realize automatic launch of the UAV swarm and reset of the launch device. Preferably, the communication interfaces of each component of the system are unified in design and retain redundancy, and the functions of each component are designed separately, so that independent UAV installation, status monitoring, and launch control function adjustment can be realized.

[0049] Embodiment 2

[0050] Reference Figure 3 Based on the same concept as the first embodiment, a vehicle-mounted UAV swarm launch control method is also included, which specifically includes the following steps:

[0051] Step S1: First, perform a system self-test to conduct a comprehensive self-test of the entire UAV vehicle-mounted launch system, including checking whether each hardware component (such as the launcher mounting bracket, launch motor, electromechanical lock, etc.) is working properly, whether the software system is running stably, and whether the system's communication link is unobstructed, ensuring that the various subsystems can exchange data normally;

[0052] Step S2: Then query the status of the vehicle-mounted platform and the launch device, check the physical status of the vehicle-mounted platform, including the stability of the platform, whether it is in a suitable launch position, etc., check whether the mechanical structure of the launch device is intact, such as whether the launcher mounting seat is stable, whether the guide rail is smooth, etc., verify whether various electronic equipment (such as sensors, controllers, etc.) on the launch motor are working properly, and obtain their real-time status data;

[0053] Step S3: Sending a launch ready instruction, and the launch device continuously monitors whether the launch ready instruction is received;

[0054] Step S4: After receiving the launch ready instruction, first release the electronic lock of the launcher mounting seat, and adjust the angle of the launcher mounting seat until it meets the angle requirement for UAV launch;

[0055] Step S5: The launch motor detects whether there is a drone stored in the launch position, and reports the storage position without a drone to the launch controller. The launch controller issues a control instruction to the variable frequency drive power supply, activates the variable frequency drive power supply, and supplies power to the position of the drone to be launched according to the control instruction, while the launch controller itself is ready to launch;

[0056] Step S6: Sending a launch instruction. When the launch device has completed all preparations and is in a ready state, the vehicle-mounted platform of the present invention sends a launch instruction to the launch device. The launch instruction contains key information about the launch mission, such as the expected initial launch velocity, launch angle and other parameters. These parameters are pre-set according to the mission requirements of the UAV, flight path planning, etc.

[0057] Step S7: closed-loop control of the variable frequency drive power supply. After receiving the transmission command, the control unit inside the variable frequency drive power supply starts to work. The control unit will perform closed-loop control according to the received command parameters. The variable frequency drive power supply monitors the output state in real time and adjusts it according to the difference with the set target.

[0058] For example, it will monitor the motor's current, voltage and other parameters, and compare these actual parameters with the parameters calculated according to the launch mission. If it is found that the actual parameters deviate from the preset parameters, it will be corrected through the internal adjustment mechanism (such as adjusting the power module, etc.) to ensure that the motor can work as required;

[0059] Step S8: After the variable frequency drive power supply completes parameter adjustment and preparation, it starts to energize the transmitting motor. As the current passes through the winding of the transmitting motor, the motor generates a strong electromagnetic force according to the principle of electromagnetic induction. The electromagnetic force acts on the structural component (motor) connected to the drone body. Since the direction of the electromagnetic force is consistent with the exit direction of the drone body, the body begins to accelerate under the impetus of the electromagnetic force.

[0060] Step S9: The launch motor continues to provide electromagnetic force to push the drone body to accelerate in the launch motor. During the acceleration process, the speed of the drone continues to increase until it reaches the initial speed required by the command of the control console. When the drone reaches the initial speed, it leaves the launch device exit at this speed and enters the flight phase. At this time, the drone's own flight control system will start to work, adjusting the flight attitude, altitude and other parameters to carry out subsequent flights according to the preset flight mission;

[0061] Step S10: Report the detachment status of the drone. After the drone obtains initial power and leaves the launcher mounting seat, it is necessary to report the successful launch of the drone, and at the same time report the initial speed, angle, energy consumption and other data of the drone;

[0062] Step S11: The launch motor is reset. After the UAV safely leaves the launch device, the actuator in the launch motor returns to the launch start position under the control of electromagnetic force, and the launch device re-enters the launch waiting state, waiting for instructions for the next launch.

[0063] The above are all preferred embodiments of the present invention, and are not intended to limit the protection scope of the present invention. Therefore, any equivalent changes made based on the structure, shape, and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. A vehicle-mounted UAV swarm launch control system, characterized by: It includes a master control platform, a transmitting controller, a transmitting device, an energy storage device, a variable frequency drive power supply, a signal wall box and a large-screen display integrated on the vehicle-mounted platform. The master control platform is connected to the energy storage device, the signal wall box, the large-screen display and the transmitting controller. The transmitting controller is connected to the transmitting device and the variable frequency drive power supply. The variable frequency drive power supply is connected to the energy storage device. The signal wall box is connected to the antenna.

2. The vehicle-mounted UAV swarm launch control system according to claim 1, characterized in that: The launching device comprises a launching motor, a launching frame mounting seat and an electromechanical lock, and the launching frame mounting seat is fixedly mounted on the vehicle-mounted platform.

3. The vehicle-mounted UAV swarm launch control system according to claim 1, characterized in that: The energy storage device stores electrical energy, which includes high-performance battery packs and supercapacitors.

4. The vehicle-mounted UAV swarm launch control system according to claim 2, characterized in that: The variable frequency drive power supply is used to convert the electric energy of the energy storage device into the electric energy form used by the transmitting motor, and the variable frequency drive power supply adjusts the output electric power according to the power demand of the transmitting motor in different transmitting stages.

5. The vehicle-mounted UAV swarm launch control system according to claim 1, characterized in that: The signal wall box includes a filtering circuit.

6. The vehicle-mounted UAV swarm launch control system according to claim 1, characterized in that: The large-screen display is used to display the current status of the drone in real time, including the speed and current of the transmitting motor, the remaining energy of the energy storage device, and the system operation mode and task progress. Various operation instructions are input to the master control platform through the touch operation interface equipped by the large-screen display or an external input device.

7. The vehicle-mounted UAV swarm launch control system according to claim 2, characterized in that: The launch controller controls the data communication between the launch device and the master control platform, and at the same time adjusts the launch angle of the vehicle-mounted UAV, performs closed-loop control of the drive power supply, launches the UAV, and resets the launch motor through the launch frame mounting seat, the launch motor, the electromechanical lock, and the variable frequency drive power supply.

8. A vehicle-mounted UAV swarm launch control system according to any one of claims 1 to 7, characterized in that: The invention also includes a vehicle-mounted UAV swarm launch control method, which specifically includes the following steps: Step S1: First, perform a system self-test to conduct a comprehensive self-test of the entire system, including checking whether each hardware component is working properly, whether the software system is running stably, and whether the communication link of the system is unobstructed, ensuring that data can be normally exchanged between each subsystem; Step S2: Then query the status of the vehicle-mounted platform and the launcher, check the physical status of the vehicle-mounted platform, including the stability of the platform and whether it is in a suitable launch position, check whether the mechanical structure of the launcher is intact, including whether the launcher mounting base is stable and whether the guide rail is smooth, verify whether various electronic equipment on the launch motor is working properly, and obtain real-time status data; Step S3: Sending a launch ready instruction, and the launch device continuously monitors whether the launch ready instruction is received; Step S4: After receiving the launch ready instruction, first release the motor lock of the launcher mounting seat, and adjust the angle of the launcher mounting seat until it meets the angle requirement for UAV launch; Step S5: The launch motor detects whether there is a drone stored in the launch position, and reports the storage position without a drone to the launch controller. The launch controller issues a control instruction to the variable frequency drive power supply, activates the variable frequency drive power supply, and supplies power to the position of the drone to be launched according to the control instruction, while the launch controller itself is ready to launch; Step S6: Sending a launch command. When the launch device has completed all preparations and is in a ready state, the master control platform sends a launch command to the launch device. The launch command contains key information about the launch mission, including the launch initial velocity and launch angle parameters pre-set according to the mission requirements of the UAV and the flight path planning; Step S7: closed-loop control of the variable frequency drive power supply. After receiving the transmission command, the control unit inside the variable frequency drive power supply starts to work. The control unit will perform closed-loop control according to the received command parameters. The variable frequency drive power supply monitors the output state in real time and adjusts it according to the difference with the set target. Step S8: After the variable frequency drive power supply completes parameter adjustment and preparation, it starts to energize the transmitting motor. As the current passes through the winding of the transmitting motor, the motor generates a strong electromagnetic force according to the principle of electromagnetic induction. The electromagnetic force acts on the structural components connected to the drone body. Since the direction of the electromagnetic force is consistent with the exit direction of the drone body, the body begins to accelerate under the impetus of the electromagnetic force. Step S9: The launch motor continuously provides electromagnetic force to push the drone body to accelerate in the launch motor. During the acceleration process, the speed of the drone increases continuously until it reaches the initial speed required by the master control platform command. When the drone reaches the initial speed, it leaves the launch device exit at the initial speed and enters the flight phase. At this time, the drone's own flight control system starts to work and adjusts the flight attitude and altitude parameters to perform subsequent flights according to the preset flight mission. Step S10: Report the detachment status of the drone. After the drone obtains initial power and leaves the launcher mounting seat, it is necessary to report the successful launch of the drone, and at the same time report the initial speed, angle, and energy consumption data of the drone; Step S11: The launch motor is reset. After the UAV safely leaves the launch device, the actuator in the launch motor returns to the launch start position under the control of electromagnetic force, and the launch device re-enters the launch waiting state, waiting for instructions for the next launch.

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