Shape rocket launching control terminal, method and system

Abstract

The invention relates to a shadow rocket launch control terminal, method and system, and belongs to the technical field of shadow rocket launch control, the launch control terminal comprises an identity authentication module, an operation information acquisition module, an operation control module, a launch control module and an operation log module; through whole-process management of identity authentication, data acquisition, attitude adjustment, state detection, ignition control and operation logs, safety, accuracy and data traceability of rocket launching operation are realized. Wherein the identity authentication ensures the safety of the operation authority, the data acquisition provides real-time information support for posture adjustment and state detection, the posture adjustment and the safe firing range judgment ensure the accuracy and the safety of launching, and the ignition control ensures that the launching is carried out under authorization; the recording and uploading of the job log enable the emission operation to have complete data record and traceability. The automation degree and reliability of figure rocket launching are improved.

Description

Technical Field

[0001] The present application relates to the technical field of shadow rocket launch control, and in particular to a shadow rocket launch control terminal, method and system. Background Art

[0002] Artificial weather modification is an important means of modern meteorological control, mainly used in the fields of rain enhancement and hail prevention. In order to achieve the desired operation effect, catalysts are usually spread into the target cloud layer by launching shadow rockets to promote weather changes. In this process, the shadow rocket launch control system, as the core equipment, undertakes the key tasks of ensuring the safety of rocket launch, operation accuracy and real-time response capability.

[0003] At present, the common human shadow rocket launch control system mainly provides basic launch control functions, lacks intelligent logical judgment and autonomous analysis capabilities. During the launch process, the system cannot automatically adjust the launch parameters according to operational requirements, and the operation process is relatively cumbersome, which affects the accuracy and operational efficiency of the human shadow rocket launch control system and limits the potential of rocket launch operations in improving launch accuracy and safety. Summary of the invention

[0004] In order to improve the safety and accuracy of shadow rocket launch operations, the present application provides a shadow rocket launch control terminal, method and system.

[0005] In the first aspect, the present application provides a human shadow rocket launch control terminal, which adopts the following technical solution: A human shadow rocket launch control terminal, the launch control terminal is used to connect a human shadow command platform and a human shadow rocket launcher loaded with human shadow rockets, the launch control terminal includes an identity authentication module, an operation information collection module, an operation control module, a launch control module and an operation log module; The identity authentication module is used to receive the identity information of the human shadow operator and perform user identity authentication, and authorize the human shadow operator to access the user operation interface after the user identity authentication is passed; The operation information acquisition module is used to collect the real-time posture information and operation status information of the human shadow rocket launcher and the ID information of the human shadow rocket; wherein the operation status information includes the position information, base state parameter information and track deformation detection information of the human shadow rocket launcher and the resistance state information and ID information of the human shadow rocket on the human shadow rocket launcher; The operation control module is used to receive the launcher target attitude parameters sent by the human shadow command platform; The operation control module is connected to the operation information acquisition module, and is also used to generate a launcher attitude adjustment instruction and send it to the human shadow rocket launcher according to the real-time attitude information of the human shadow rocket launcher and the target attitude parameter of the launcher; wherein the launcher attitude adjustment instruction includes an azimuth adjustment instruction and a pitch angle adjustment instruction; The launch control module is connected to the operation information collection module, and is used to detect the operation status information of the human shadow rocket launcher and the ID information of the human shadow rocket to obtain the detection result; The launch control module is further used to send ignition application information to the human shadow command platform when the detection result is a detection pass, generate an ignition control instruction in response to the launch operation signal sent by the human shadow command platform, and send it to the human shadow rocket launcher; The operation log module is used to record the launch operation information and generate operation log information, and upload the operation log information to the human shadow command platform.

[0006] By adopting the above technical solution, through the collaborative work of modules such as identity authentication, information collection, attitude adjustment, status detection, ignition control and log record upload, an efficient and safe rocket launch operation process is realized. The system can accurately control the attitude adjustment of the launcher to ensure that the rocket is launched in the preset direction and angle. At the same time, it performs ignition control under the premise of meeting safety and launch operation conditions. Through real-time collection and log recording of operation information, the whole process monitoring and data preservation of the launch operation are realized. This technical solution can significantly improve the safety and reliability of human shadow operations, while simplifying the operation process, reducing human intervention, ensuring the accuracy and traceability of rocket launches, and achieving the technical effect of intelligent and automated control.

[0007] Optionally, the identity authentication module includes: A face information collection unit, used to collect face information of shadow workers; An identity recognition and authentication unit, used to perform identity recognition and authentication based on the face information to obtain an identity recognition and authentication result; An authorization management unit is used to authorize the human shadow operator to access the user operation interface according to the identity recognition and authentication result.

[0008] By adopting the above technical solutions, the face information collection unit ensures the real-time and accuracy of the data, the identity recognition and authentication unit provides an efficient comparison algorithm to verify the identity of the human shadow operator, and the authorization management unit effectively controls the operation authority to ensure that only verified personnel can access the system. This multi-level identity authentication solution not only improves the security of the system, but also enhances the user's operating experience and data traceability, thereby providing a more reliable security guarantee for the human shadow rocket launch operation.

[0009] Optionally, the operation information collection module includes: A posture information acquisition unit, used to acquire real-time posture information of the shadow rocket launcher, wherein the posture information includes azimuth information and pitch angle information; A position information acquisition unit, used to acquire the position information of the human shadow rocket launcher; A base state parameter acquisition unit, used to acquire base state parameter information of the human shadow rocket launcher; A track deformation information acquisition unit, used to acquire track deformation detection information of the shadow rocket launcher; A resistance information acquisition unit, used to acquire resistance status information of the human shadow rocket on the human shadow rocket launcher; The rocket ID information collection unit is used to collect the ID information of the shadow rocket on the shadow rocket launcher.

[0010] By adopting the above technical solutions, the attitude information acquisition unit ensures that the angle and direction of the launcher meet the mission requirements, the position information acquisition unit provides the geographic positioning data of the launcher, the base status parameter acquisition unit monitors the health status of the launcher base, the track deformation information acquisition unit ensures the flatness and accuracy of the track, the resistance information acquisition unit provides the safety guarantee of the ignition circuit, and the rocket ID information acquisition unit realizes the unique identification of the rocket. Through these information acquisition functions, the system can grasp the launch conditions in real time, ensure the safety, accuracy and reliability of the launch operation, and provide rich basic data for subsequent operation records and data analysis.

[0011] Optionally, the job control module includes: A target attitude parameter receiving unit is used to receive the launcher target attitude parameters sent by the human shadow command platform; wherein the launcher target attitude parameters include target azimuth parameters and target pitch angle parameters; A target attitude judgment unit is used to judge whether the target attitude parameters of the launcher meet the preset safe firing range information, and if so, output a target attitude qualified result; The attitude adjustment calculation unit calculates the launcher attitude adjustment parameters according to the real-time attitude information of the shadow rocket launcher and the launcher target attitude parameters in response to the qualified result of the target attitude; An attitude adjustment control unit is used to generate a launcher attitude adjustment control instruction according to the launcher attitude adjustment parameters and send it to the shadow rocket launcher.

[0012] By adopting the above technical solution, the target attitude parameter receiving unit obtains the target attitude information from the command platform, the target attitude judgment unit automatically checks the safety of the parameters, the attitude adjustment calculation unit dynamically calculates the adjustment amount based on real-time information, and the attitude adjustment control unit finally generates and issues adjustment instructions, thereby ensuring that the launcher is quickly and accurately adjusted to the target attitude that meets safety requirements and mission requirements. This technical solution improves launch accuracy while ensuring safety, providing strong support for the smooth progress of rocket launch operations.

[0013] Optionally, the emission control module includes: An operation status information detection unit, used to detect whether the operation status information of the human shadow rocket launcher is in a normal state, and if so, output an operation status detection pass result; A rocket ID information detection unit is used to detect whether the ID information of the shadow rocket is matched successfully, and if so, output an ID information detection pass result; An ignition application unit, used for sending ignition application information to the human shadow command platform according to the operation status detection result and the ID information detection result; The ignition control unit generates an ignition control instruction in response to the launch operation signal sent by the human shadow command platform and sends it to the human shadow rocket launcher.

[0014] By adopting the above technical solution, the operation status information detection unit ensures that the launcher is in a normal state, the rocket ID information detection unit verifies the correctness of the ammunition, the ignition application unit applies for ignition permission from the command platform when the launch conditions are met, and the ignition control unit issues an ignition command after obtaining authorization from the command platform. This technical solution fully verifies and confirms the key parameters before launch, ensures the accuracy and safety of the rocket launch operation, and realizes the effective control of the ignition operation under the authorization of the command platform, providing a reliable guarantee for the smooth completion of the rocket launch mission.

[0015] Optionally, the rocket ID information detection unit includes: A rocket parameter acquisition unit, configured to acquire corresponding rocket parameter information based on a preset database according to the rocket ID information; An ammunition verification unit, used to perform a comparison verification based on the rocket parameter information, and output an ammunition verification pass result after the verification passes; A rocket parameter sending unit, in response to the ammunition verification passing result, sends the rocket parameter information to the human shadow rocket launcher; The detection result output unit outputs the ID information detection pass result in response to the rocket parameter matching success signal fed back by the human shadow rocket launcher.

[0016] By adopting the above technical solution, the key parameters of the rocket are extracted from the database, the parameters are compared and verified to ensure that they meet the mission requirements, and then the parameters are sent to the base controller for automatic adjustment. The detection result output unit outputs the confirmation result after the verification is completed. This technical solution effectively compares the rocket ID before launch and fully verifies the rocket parameters to ensure that the information of the rocket to be launched is accurate, effectively improving the safety, automation and accuracy of the launch operation, and providing a solid guarantee for the smooth progress of the rocket launch process.

[0017] Optionally, the job log module includes: An operation log generating unit, used to record the launch operation information and generate the operation log information; the launch operation information includes the operation time, operation location, operation mode, ammunition model and ammunition quantity; The operation log uploading unit is used to upload the operation log information to the human shadow command platform.

[0018] By adopting the above technical solution, the key data of each launch operation is recorded in detail, ensuring the integrity and standardization of the log, and then uploading the generated log information to the command platform, realizing remote data storage and real-time access. The operation log module effectively improves the data management level of the launch operation, enables the command platform to grasp the launch situation in real time, and provides reliable data support for subsequent management, analysis and decision-making. Through the standardized recording and real-time uploading of logs, the traceability, transparency and data management efficiency of the launch operation are greatly enhanced.

[0019] Optionally, the transmission control terminal further includes: The operation interface display module is used to display the user operation interface and provide human-computer interaction functions after the user identity authentication is passed; The safety shooting range display module is used to display the angle range of the preset safety shooting range information.

[0020] By adopting the above technical solutions, the operation interface display module provides an intuitive operation platform for the shadow operators, which is convenient for real-time monitoring and operation control, and improves the operability of the launch operation; the safe firing range display module provides a safety reference for the shadow operators by displaying the safe firing range angle range in real time, ensuring the safety of the launch process. By configuring the display function, not only the visualization and interactivity of the system are enhanced, but also the safety control capability of the operation is significantly improved, ensuring the smooth and safe progress of the rocket launch operation.

[0021] In the second aspect, the present application provides a human shadow rocket launch control method, which adopts the following technical solution: A human shadow rocket launch control method is applied to the human shadow rocket launch control terminal described in the first aspect, and the control method includes: Receiving identity information of a human shadow operator and performing user identity authentication, and authorizing the human shadow operator to access a user operation interface after the user identity authentication passes; Collecting real-time attitude information and operation status information of the shadow rocket launcher and ID information of the shadow rocket; wherein the operation status information includes position information, base state parameter information and track deformation detection information of the shadow rocket launcher and resistance state information and ID information of the shadow rocket on the shadow rocket launcher; Receiving the launcher target attitude parameters sent by the human shadow command platform; Determining whether the target attitude parameters of the launcher meet the preset safe firing range information; If yes, then based on the real-time attitude information of the shadow rocket launcher and the target attitude parameters of the launcher, a launcher attitude adjustment instruction is generated and sent to the shadow rocket launcher; wherein the launcher attitude adjustment instruction includes an azimuth adjustment instruction and a pitch angle adjustment instruction; Detect the operating status information of the human shadow rocket launcher and the ID information of the human shadow rocket to determine whether the detection is passed. If so, send ignition application information to the human shadow command platform; In response to the launch operation signal sent by the human shadow command platform, an ignition control instruction is synchronously generated and sent to the human shadow rocket launcher; Record the launch operation information and generate operation log information, and upload the operation log information to the human shadow command platform.

[0022] By adopting the above technical solution, the safety, accuracy and data traceability of rocket launch operations are achieved through the whole process management of identity authentication, data collection, attitude adjustment, status detection, ignition control and operation log. Among them, identity authentication ensures the security of operation authority, data collection provides real-time information support for attitude adjustment and status detection, attitude adjustment and safe firing range judgment ensure the accuracy and safety of launch, ignition control ensures that the launch is carried out under authorization, and operation log recording and uploading enable the launch operation to have complete data records and traceability. This technical solution significantly improves the automation and reliability of rocket launches, and provides comprehensive technical support and safety guarantees for the launch of human shadow rockets.

[0023] In a third aspect, the present application provides a human shadow rocket launch control system, which adopts the following technical solution: A human shadow rocket launch control system, the launch control system includes a human shadow command platform, a human shadow rocket launcher loaded with human shadow rockets, and a human shadow rocket launch control terminal as described in the first aspect, the human shadow rocket launch control terminal is respectively connected to the human shadow command platform and the human shadow rocket launcher.

[0024] In summary, the present application includes at least one of the following beneficial technical effects: through the whole process management of identity authentication, data collection, attitude adjustment, status detection, ignition control and operation log, the safety, accuracy and data traceability of rocket launch operations are achieved. Among them, identity authentication ensures the security of operating authority, data collection provides real-time information support for attitude adjustment and status detection, attitude adjustment and safe firing range judgment ensure the accuracy and safety of the launch, ignition control ensures that the launch is carried out under authorization, and operation log recording and uploading enable the launch operation to have complete data records and traceability. This technical solution significantly improves the automation and reliability of human shadow rocket launches, and provides comprehensive technical support and safety guarantees for human shadow rocket launches. BRIEF DESCRIPTION OF THE DRAWINGS

[0025] Figure 1 This is a structural block diagram of a human shadow rocket launch control terminal according to one of the embodiments of the present application.

[0026] Figure 2 It is a flow chart of a human shadow rocket launch control method according to one of the embodiments of the present application. DETAILED DESCRIPTION

[0027] In order to make the purpose, technical solutions and advantages of this application more clear, the following Figure 1-2 It should be understood that the specific embodiments described herein are only used to explain the present application and are not used to limit the present application.

[0028] At present, the existing human shadow rocket launch control system has exposed some technical deficiencies in practical applications and needs to be improved urgently.

[0029] First, in terms of data processing capabilities, launch control systems usually need to process a large amount of real-time data, including the attitude and position of the launcher and parameter information of the rocket. However, the hardware configuration and software architecture of the existing system are relatively backward, making it difficult to quickly respond to and process these real-time data. This results in low system feedback speed and data accuracy in complex weather conditions and multi-task collaborative operations, which cannot meet the operators' needs for fast and efficient decision support. At the same time, the lack of real-time monitoring and analysis capabilities of the system status makes it difficult to ensure safety and reliability during the launch control process.

[0030] Secondly, in terms of user interface design and human-computer interaction experience, existing launch control systems often use traditional LCD character displays or LED indicators to display key operation information. This design has a low degree of visualization, which makes it difficult for human shadow operators to quickly identify and understand key data during the launch process. In high-intensity or emergency situations, operators may make erroneous operations or make wrong decisions due to untimely information acquisition, affecting the safety and effectiveness of operations. In addition, the traditional interface lacks intuitive graphical and dynamic display functions, which makes it inconvenient for human shadow operators to track and adjust the launch status in real time, and the user experience is poor.

[0031] Then, in terms of functional diversity and automation level, the existing human-powered rocket launch control system mainly provides basic launch control functions, lacks intelligent logical judgment and autonomous analysis capabilities, and many processes still rely on manual operation. This not only increases the burden on operators, but also leads to a decrease in launch efficiency and accuracy, especially in emergencies, and cannot achieve rapid and automated responses.

[0032] In addition, the existing system's operating procedures are cumbersome and its safety is also insufficient. Due to the lack of comprehensive automatic fault diagnosis and emergency handling functions, the system fails to meet the expected standards in terms of operational safety. Human shadow operators need to closely monitor the system status, which increases their workload.

[0033] Based on this, in order to meet the needs of modern artificial weather modification operations for higher efficiency and safety, an embodiment of the present application discloses a human shadow rocket launch control terminal.

[0034] Reference Figure 1 , a human shadow rocket launch control terminal, the launch control terminal is used to connect the human shadow command platform and the human shadow rocket launcher loaded with human shadow rockets, the launch control terminal includes an identity authentication module, an operation information collection module, an operation control module, a launch control module and an operation log module; An identity authentication module is used to receive the identity information of the human shadow operator and perform user identity authentication, and authorize the human shadow operator to access the user operation interface after the user identity authentication is passed; Among them, the identity authentication module performs user identity authentication by receiving the identity information of the shadow operator (such as face recognition, biometric fingerprint or password). Only after the identity authentication is passed, the system will authorize the user to access the operation interface of the rocket launch control terminal, ensuring that the shadow operator has a legal identity. The system effectively prevents unauthorized operations and ensures the safety and legality of rocket launch operations.

[0035] The operation information collection module is used to collect the real-time attitude information and operation status information of the shadow rocket launcher and the ID information of the shadow rocket; The operation status information includes the position information of the shadow rocket launcher, the base status parameter information and the track deformation detection information, and the resistance status information and ID information of the shadow rocket on the shadow rocket launcher; Specifically, the operation status information includes location information (longitude, latitude, altitude), base status parameters (voltage, temperature, etc.), track deformation detection information (to ensure that the track is not deformed), and the resistance status of the rocket (to ensure electrical safety) and ID.

[0036] The operation control module is used to receive the launcher target attitude parameters sent by the human shadow command platform; The operation control module is connected to the operation information collection module, and is also used to generate a launcher attitude adjustment instruction and send it to the launcher according to the real-time attitude information of the launcher and the target attitude parameters of the launcher; wherein the launcher attitude adjustment instruction includes an azimuth adjustment instruction and a pitch angle adjustment instruction; Specifically, the launch pad attitude adjustment instruction is sent to the launch pad for execution and adjustment. The adjustment instruction includes specific azimuth and pitch angle instructions to ensure that the launch pad's attitude reaches the target attitude to meet mission requirements and improve operation accuracy and success rate.

[0037] The launch control module is connected to the operation information collection module and is used to detect the operation status information of the shadow rocket launcher and the ID information of the shadow rocket to obtain the detection result; Among them, the launch control module is responsible for detecting the operating status information and rocket ID information of the shadow rocket launcher to determine whether the launch conditions are met.

[0038] The launch control module is also used to send ignition application information to the human shadow command platform when the detection result is that the detection is passed, and generate an ignition control instruction in response to the launch operation signal sent by the human shadow command platform and send it to the human shadow rocket launcher; Specifically, once the launch control module detects that the resistance value of the rocket is within the normal range, the orbital status is normal, and the ID information of the rocket is successfully matched, it can send an ignition request information to the command platform, and generate an ignition control instruction after receiving the launch operation signal, and finally send the instruction to the launch pad to complete the ignition.

[0039] In some embodiments, when the rocket launcher enters the launch state, the launch control module performs a safe boost operation by starting the fire control switch and the boost enable switch; this step ensures that all state parameters meet the launch requirements before ignition, which can effectively prevent failures during the ignition process, thereby improving the success rate of the launch. After completing the boost operation, the launch control module can select a specific launch channel and perform ignition control. This function supports independent control of each launch channel, allowing the operator to accurately control the launch sequence and time of a single or multiple rockets. This control method not only improves the accuracy and flexibility of the launch, but also ensures that the rocket launch is completed in sequence within the scheduled time.

[0040] The operation log module is used to record the launch operation information and generate operation log information, and upload the operation log information to the human shadow command platform.

[0041] Specifically, the operation log module records the operation information in real time during the entire launch process, including key parameters such as launch time, location, attitude angle, rocket ID and resistance status. After the operation is completed, the log module will generate a complete launch operation log and upload it to the Human Shadow Command Platform through the network for recording and analysis by the Human Shadow Command Platform.

[0042] In the above implementation, through the collaborative work of modules such as identity authentication, information collection, attitude adjustment, status detection, ignition control and log record upload, an efficient and safe rocket launch operation process is achieved. The system can accurately control the attitude adjustment of the launcher to ensure that the rocket is launched in a preset direction and angle. At the same time, it performs ignition control under the premise of meeting safety and launch operation conditions. Through real-time collection and log recording of operation information, full monitoring and data preservation of the launch operation are achieved. This technical solution can significantly improve the safety and reliability of human shadow operations, while simplifying the operating process, reducing human intervention, ensuring the accuracy and traceability of rocket launches, and achieving the technical effect of intelligent and automated control.

[0043] In some embodiments, the rocket launch control terminal may be a smart mobile terminal, such as a mobile phone, a tablet computer, etc. The rocket launch control terminal and the human shadow command platform communicate based on 4G / 5G, and the rocket launch control terminal and the rocket launcher communicate based on LORA wireless communication or RS485 wired communication.

[0044] As an implementation of the identity authentication module, the identity authentication module includes: A face information collection unit, used to collect face information of shadow workers; Among them, the facial information of the shadow operator is captured through a camera or similar optical equipment. This unit is responsible for collecting the facial feature data of the shadow operator in real time and transmitting the data to the identity recognition and authentication unit for further processing; facial information collection ensures the authenticity and real-time nature of the data and is the basis of identity authentication.

[0045] An identity recognition and authentication unit, used to perform identity recognition and authentication based on face information and obtain an identity recognition and authentication result; Among them, by receiving facial feature data from the face information collection unit and comparing it with the authorized personnel face database stored in the system. The comparison process can use algorithms such as pattern matching and deep learning to compare the similarity of features to confirm the identity. The comparison result will generate an identity recognition and authentication result, including the matching degree and authentication status (passed or failed), so as to effectively distinguish between authorized and unauthorized personnel, avoid unauthorized personnel from misoperating the rocket launch system, and improve the system's security protection level by ensuring the accuracy of identity recognition.

[0046] The authorization management unit is used to authorize human shadow operators to access the user operation interface based on the identity recognition and authentication results.

[0047] Specifically, the authorization management unit decides whether to allow the shadow operator to access the user operation interface based on the authentication result of the identity recognition authentication unit. When the authentication result is "passed", the authorization management unit will open the user operation interface permission and record the authorization process; when the authentication result is "failed", the authorization management unit will reject the shadow operator's access request and may trigger a security alarm.

[0048] In the above implementation, the face information collection unit ensures the real-time and accuracy of the data, the identity recognition and authentication unit provides an efficient comparison algorithm to verify the identity of the human shadow operator, and the authorization management unit effectively controls the operation authority to ensure that only verified personnel can access the system. This multi-level identity authentication scheme not only improves the security of the system, but also enhances the user's operating experience and data traceability, thereby providing a more reliable security guarantee for the human shadow rocket launch operation.

[0049] As an implementation of the operation information collection module, the operation information collection module includes: The attitude information acquisition unit is used to collect the real-time attitude information of the human shadow rocket launcher, and the attitude information includes azimuth information and pitch angle information; Among them, the attitude information acquisition unit collects the attitude information of the human shadow rocket launcher in real time through sensors or angle detection equipment. The attitude information includes azimuth information and pitch angle information, which can accurately describe the current direction and angle of the launcher; the azimuth information is used to determine the horizontal direction of the launcher, and the pitch angle reflects the vertical angle of the launcher. This information is crucial for the precise launch of the rocket.

[0050] A position information acquisition unit, used to acquire position information of a human shadow rocket launcher; Among them, the location information collection unit collects the geographical location of the human shadow rocket launcher, including longitude, latitude and altitude, through GPS or other positioning devices. This information is crucial for the launch positioning, trajectory calculation and safety control of the rocket. Especially in the case of environmental changes or a wide range of operations, the location information can provide the command center with an accurate launch location.

[0051] A base state parameter acquisition unit is used to collect base state parameter information of the human shadow rocket launcher; Among them, the status information of the launcher base is collected, including the status parameters of key equipment such as batteries, displacement sensors, communication modules, servo systems, GPS and compasses. It is understandable that the normal status of the base is crucial to the stability of the launcher and the safety of the launch process. Collecting these parameters can help the system determine whether the base is in the best working state and promptly discover and resolve potential anomalies.

[0052] Track deformation information acquisition unit, used to collect track deformation detection information of the human shadow rocket launcher; Among them, since the accuracy of rocket launch is affected by the flatness and deformation of the track, the deformation of the track needs to be tested before each launch. If the deformation of the track exceeds the allowable range, it may affect the launch angle and accuracy of the rocket.

[0053] A resistance information acquisition unit, used to acquire resistance status information of the shadow rocket on the shadow rocket launcher; The resistance information is used to determine the electrical contact of the rocket and ensure that there is no short circuit or open circuit in the electrical circuit before ignition. The resistance status is the basis of rocket ignition safety, and abnormal resistance may lead to ignition failure or other safety risks.

[0054] For example, after loading a rocket, the resistance information acquisition unit measures the rocket resistance to be 2.5 ohms, which is within the preset safety range. If the resistance value is too high or too low (such as less than 1 ohm or more than 8 ohms), the system will display an abnormality and prompt you to check the connection of the rocket to ensure the safety and stability of the ignition circuit.

[0055] The rocket ID information collection unit is used to collect the ID information of the shadow rocket on the shadow rocket launcher.

[0056] In one of the embodiments of the present application, the rocket ID information collection unit obtains the unique ID information of the rocket by scanning the QR code or other identifier on the rocket; the ID information is used to identify the model, batch and other detailed information of the rocket, ensure the use of ammunition that meets the current operation requirements, and provide a basis for operation records and data traceability.

[0057] In the above implementation, the attitude information acquisition unit ensures that the angle and direction of the launcher meet the mission requirements, the position information acquisition unit provides the geographic positioning data of the launcher, the base state parameter acquisition unit monitors the health status of the launcher base, the track deformation information acquisition unit ensures the flatness and accuracy of the track, the resistance information acquisition unit provides abnormality inspection of the ignition circuit and safety inspection of the rocket to be launched, and the rocket ID information acquisition unit realizes the unique identification of the rocket. Through these information acquisition functions, the system can grasp the launch conditions in real time, ensure the safety, accuracy and reliability of the launch operation, and provide rich basic data for subsequent operation records and data analysis.

[0058] As an implementation of the job control module, the job control module includes: A target attitude parameter receiving unit is used to receive the launcher target attitude parameters sent by the human shadow command platform; Among them, the launcher target attitude parameters include target azimuth parameters and target pitch angle parameters; Specifically, the target azimuth parameters and target pitch angle parameters are used to set the direction and angle of the launcher during launch. After these data are set in the command center, they are remotely sent to the launch control terminal to ensure that the launcher is adjusted to the precise launch posture according to mission requirements.

[0059] The target attitude judgment unit is used to judge whether the target attitude parameters of the launcher meet the preset safe firing range information, and if so, output the target attitude qualified result; Specifically, the target attitude judgment unit compares the received target attitude parameters with the preset safe firing range information to determine whether the parameters meet the safe firing range. The safe firing range refers to the safe range for launch, which ensures that the safety of personnel or the surrounding environment will not be threatened when the rocket is launched. If the target attitude meets the safe firing range, the target attitude judgment unit outputs "target attitude qualified result", otherwise, it returns "unqualified" information to remind you to reset the parameters.

[0060] It can be understood that the target attitude judgment unit ensures that the attitude parameters of the launch pad meet safety specifications by automatically checking the safety of the target attitude, effectively avoiding unsafe launch angles and ensuring the safety of rocket launch operations.

[0061] The attitude adjustment calculation unit calculates the launcher attitude adjustment parameters according to the real-time attitude information of the launcher and the launcher target attitude parameters in response to the qualified result of the target attitude; Specifically, after receiving the "target attitude qualified result", the attitude adjustment calculation unit starts to calculate the attitude adjustment parameters of the launch pad. By comparing the real-time attitude information with the target attitude parameters, it calculates the required adjustment amount, which includes the difference between the azimuth angle and the pitch angle, and converts it into specific adjustment instructions to ensure that the launch pad can be accurately adjusted to the target attitude position set by the command platform, thereby improving the flexibility and accuracy of attitude control.

[0062] The attitude adjustment control unit is used to generate launcher attitude adjustment control instructions according to the launcher attitude adjustment parameters and send them to the human shadow rocket launcher.

[0063] After receiving the attitude adjustment parameters, the attitude adjustment control unit generates corresponding attitude adjustment control instructions according to the calculated azimuth and pitch angle adjustment amounts. Subsequently, the control instructions are sent to the launcher, which drives the actuator (such as a motor) to complete the precise attitude adjustment after receiving the instructions to ensure that the final attitude of the launcher meets the mission requirements.

[0064] Exemplarily, the adjustment amount generated by the attitude adjustment calculation unit is an increase of 10 degrees in azimuth and 5 degrees in pitch. The attitude adjustment control unit generates a motor control signal and sends it to the launch pad control system. The launch pad automatically rotates to an azimuth of 30 degrees and a pitch of 65 degrees according to the command to achieve the specified target attitude.

[0065] It should be noted that after the launch mission is completed, in order to prepare for the next launch or maintenance, the attitude adjustment control unit can control the launcher to return to its initial state through the state return to zero command. State return to zero is an important part of the daily maintenance and re-preparation of the launcher, ensuring that the launcher is always in the best condition and ready for the next launch at any time.

[0066] In the above implementation, the target attitude parameter receiving unit obtains the target attitude information from the command platform, the target attitude judgment unit automatically checks the safety of the parameters, the attitude adjustment calculation unit dynamically calculates the adjustment amount based on real-time information, and the attitude adjustment control unit finally generates and issues adjustment instructions, thereby ensuring that the launcher is quickly and accurately adjusted to the target attitude that meets safety requirements and mission requirements. This technical solution improves launch accuracy while ensuring safety, providing strong support for the smooth progress of rocket launch operations.

[0067] As an implementation of the launch control module, the launch control module includes: An operation status information detection unit is used to detect whether the operation status information of the shadow rocket launcher is in a normal state, and if so, output an operation status detection pass result; Specifically, the operating status information includes position information, base status parameters (such as the status information of the battery, displacement sensor, communication module, servo system, GPS and compass) and track deformation detection information. By analyzing the collected status information, it is determined whether the launcher is in normal working condition and whether it meets the launch requirements. If all parameters are within the normal range, the "operating status detection pass result" is output, allowing the launch process to continue, effectively avoiding failures and safety hazards caused by abnormal status.

[0068] The rocket ID information detection unit is used to detect whether the ID information of the shadow rocket is matched successfully. If so, the ID information detection pass result is output; Specifically, it determines whether the currently loaded rocket matches the rocket ID preset by the command platform. The matching verification of ID information can ensure the use of the correct rocket model and avoid launch failure or risk caused by wrong ammunition. If the ID match is successful, the "ID information detection pass result" is output to ensure that the rocket loaded on the launcher meets the mission requirements.

[0069] The ignition application unit is used to detect the pass result according to the operation status and ID information, and send the ignition application information to the human shadow command platform; The ignition application information includes the detection results of the operation status and the rocket ID, which serves as the basis for the command platform to approve the ignition; the function of this unit is to ensure that the ignition application is made when all launch conditions are met, thereby further ensuring the safety of the launch process. For example, the ignition application information content may include: "The operation status is normal, the ID match is successful, and the ignition permission is applied for."

[0070] The ignition control unit, in response to the launch operation signal issued by the Human Shadow command platform, generates an ignition control instruction and sends it to the Human Shadow rocket launcher.

[0071] Specifically, the ignition control unit ensures that the ignition command can only be executed after obtaining authorization from the command platform, ensuring the controllability and safety of the ignition operation. After the ignition control command is issued, the launcher starts the ignition device according to the set program, thereby completing the rocket launch mission.

[0072] It is understandable that the ignition control unit ensures the safety and precise control of the ignition operation through authorized linkage with the command platform, making the rocket launch process more standardized and reliable.

[0073] In the above implementation, the operation status information detection unit ensures that the launcher is in a normal state, the rocket ID information detection unit verifies the correctness of the ammunition, the ignition application unit applies to the command platform for ignition permission when the launch conditions are met, and the ignition control unit issues an ignition command after obtaining authorization from the command platform. This technical solution fully verifies and confirms the key parameters before launch, ensures the accuracy and safety of the rocket launch operation, and realizes effective control of the ignition operation under the authorization of the command platform, providing a reliable guarantee for the smooth completion of the rocket launch mission.

[0074] As an implementation method of the rocket ID information detection unit, the rocket ID information detection unit includes: A rocket parameter acquisition unit, used to acquire corresponding rocket parameter information based on a preset database according to the rocket ID information; The rocket parameter acquisition unit retrieves the corresponding rocket parameter information from the preset database in the system according to the scanned rocket ID information. The rocket parameter information usually includes the rocket model, diameter, length, weight, fuel type and other key attributes. These parameters must be matched with the launcher settings before launch to ensure the accuracy and safety of the launch.

[0075] The ammunition verification unit is used to perform comparison verification based on the rocket parameter information and output the ammunition verification result after passing the verification; Specifically, the ammunition verification unit is responsible for comparing and verifying the acquired rocket parameter information to confirm whether the parameters of the rocket meet the requirements of the launch mission. The verification process can be compared with the preset launch mission parameters to ensure that the model and specifications of the rocket used match the operational requirements. After the verification is passed, the unit outputs "Ammunition Verification Pass Result", otherwise, it prompts that the verification failed and prevents further operation.

[0076] The rocket parameter sending unit sends the rocket parameter information to the human shadow rocket launcher in response to the ammunition verification passing result; Among them, after receiving the "ammunition verification result", the parameter information of the rocket is sent to the base controller of the human shadow rocket launcher. After receiving these parameters, the base controller automatically adjusts the launch track according to the specific parameters of the rocket (such as the diameter) to ensure the precise coordination of the rocket and the track, and prepare for the rocket launch.

[0077] It can be understood that by transmitting the rocket parameters to the base controller, the rocket and the launcher are accurately matched, the loading efficiency and launching accuracy are improved, the error of manual adjustment is reduced, and the automation level of the launching operation is further improved.

[0078] The detection result output unit outputs the ID information detection pass result in response to the rocket parameter matching success signal fed back by the human shadow rocket launcher.

[0079] Specifically, after ensuring that the rocket and the launch track are correctly matched, the base controller of the human shadow rocket launcher can feedback the rocket parameter matching success signal. This signal indicates that the matching of the rocket parameters and the launcher track has been completed, and the loading of the rocket meets the launch requirements, providing a confirmation basis for the subsequent launch process.

[0080] In the above implementation, the key parameters of the rocket are extracted from the database, the parameters are compared and verified to ensure that they meet the mission requirements, and then the parameters are sent to the base controller for automatic adjustment. The detection result output unit outputs the confirmation result after the verification is completed. This technical solution fully verifies and adjusts the ID and parameters of the rocket before launch to ensure that the rocket matches the launch track correctly, effectively improving the safety, automation and accuracy of the launch operation, and providing a solid guarantee for the smooth progress of the rocket launch process.

[0081] As an implementation of the job log module, the job log module includes: An operation log generation unit is used to record the launch operation information and generate the operation log information; the launch operation information includes the operation time, operation location, operation method, ammunition model and ammunition quantity; Specifically, during each rocket launch operation, the key information of the launch operation is automatically recorded and the corresponding operation log information is generated. The log information includes the operation time, operation location, operation method, ammunition model and ammunition quantity. The operation time is used to record the specific operation time, the operation location is the geographical coordinates of the launch location, and the operation method indicates the purpose of the launch (such as rain enhancement, hail prevention, etc.). The ammunition model and ammunition quantity record the type and quantity of rockets used, providing a basis for subsequent inventory management and analysis.

[0082] The operation log uploading unit is used to upload the operation log information to the human shadow command platform.

[0083] Specifically, the operation log upload unit is responsible for uploading the generated operation log information to the human shadow command platform through a network connection to achieve remote monitoring and data storage. The upload function ensures that the operation information can be transmitted to the command platform in real time or regularly so that the command platform can grasp the situation of the on-site launch operation in a timely manner. These data not only provide support for subsequent analysis, but also provide a basis for the supervision and management of the launch.

[0084] In the above implementation, the key data of each launch operation is recorded in detail to ensure the integrity and standardization of the log, and then the generated log information is uploaded to the command platform, realizing remote data storage and real-time access. The operation log module effectively improves the data management level of the launch operation, enables the command platform to grasp the launch situation in real time, and provides reliable data support for subsequent management, analysis and decision-making. Through the standardized recording and real-time uploading of the log, the traceability, transparency and data management efficiency of the launch operation are greatly enhanced.

[0085] As a further implementation of the transmission control terminal, the transmission control terminal further includes: The operation interface display module is used to display the user operation interface and provide human-computer interaction functions after the user identity authentication is passed; Specifically, after the user identity authentication is passed, the display operation interface is activated and the human-computer interaction function is provided. The module integrates the display area of ​​all operation instructions and feedback information on the interface, so that the shadow operator can view the status of the launcher, rocket parameters and operation status information in real time. Through the user operation interface, the shadow operator can perform relevant operation controls for rocket launch and receive various operation results fed back by the system, thereby realizing real-time control and management of the entire launch process.

[0086] The safety shooting range display module is used to display the angle range of the preset safety shooting range information.

[0087] Specifically, according to the preset safe firing range information, the safe angle range is displayed in real time to provide a safe reference for the human shadow operator. The safe firing range information includes a pre-set launch safety area. Through the visual display of the angle range, the human shadow operator can clearly know whether the current launcher is within the safe range, so as to avoid entering the dangerous area during launch.

[0088] In the above implementation, the operation interface display module provides an intuitive operation platform for the human shadow operator, which is convenient for real-time monitoring and operation control, and improves the operability of the launch operation; the safe firing range display module provides a safety reference for the human shadow operator by displaying the safe firing range angle range in real time, ensuring the safety of the launch process. By configuring the display function, not only the visualization and interactivity of the system are enhanced, but also the safety control capability of the operation is significantly improved, ensuring the smooth and safe progress of the rocket launch operation.

[0089] As a specific implementation of the hardware configuration of the human shadow rocket launch control terminal, the human shadow rocket launch control terminal mainly includes a main processing unit, a co-processing unit, a human-computer interaction unit, a communication unit, a data encryption unit, an image acquisition unit, a voice call unit, a LORA wireless communication unit, an RS485 communication unit and a GPS communication unit; Among them, the main processing unit adopts MTK6771 central processing unit chip, equipped with Cortex-A73 octa-core CPU, responsible for processing large amounts of data and complex computing tasks, with multi-standard video codecs, rich hardware interfaces, independent power management system, powerful network expansion capabilities and display interfaces. As the core of the entire system, the main processing unit can be connected to the 10.1-inch LCD screen of the human-machine interaction unit through the LVDS interface, support the display of the operation interface, and help operators to operate intuitively. Connect the capacitive touch screen through the I2C bus to capture human-machine interaction operation information. Connect to the communication unit through the PCIE interface, use the 4G / 5G network to receive operation instructions from the human shadow command center and upload operation log information, ensuring the efficiency of data transmission. Connect to the image acquisition unit through the USB interface, and scan the rocket QR code through the front camera to obtain information such as rocket model, diameter, length, weight and production date; in addition, the face detection camera is used to realize the face recognition and authentication of the operator. The voice call unit can also be connected through the USB interface to support two-way audio intercom with the command center, which is used for operators to apply for operation time and airspace. The data encryption unit is connected via the I2C interface, and the security encryption chip is used to ensure the safe storage and encryption and decryption of the operating data.

[0090] In addition, the co-processing unit uses the STM32H750ZBT6 controller, which is mainly used to assist the main processing unit in completing data processing and communication tasks. It is connected to the main processing unit through Ethernet to achieve high-speed data transmission, which improves data processing and response efficiency. It is connected to the LORA wireless communication unit through the serial port, sends acquisition and control instructions to the launcher base controller, and receives the return data from the base controller to achieve remote control. It is connected to the RS485 communication unit through the serial port to support wired data transmission with the launcher base controller to ensure the stability of data transmission. It is connected to the GPS communication unit through the serial port to obtain GPS positioning information in real time, including longitude, latitude and altitude, and supports GPS timing function to achieve high-precision time synchronization.

[0091] Based on the above implementation method, the launch control terminal of the human shadow rocket realizes efficient, safe and reliable operation control through the collaborative work of multiple communication technologies and functional units, providing strong technical support for artificial weather modification operations.

[0092] The human shadow rocket launch control terminal of this application has many significant advantages in the actual application process, which improves the automation level, safety, operation convenience and information processing ability of the system, making the rocket launch operation of artificial weather modification more efficient, accurate and reliable. First of all, the control terminal can authenticate the identity of the operator and provide corresponding operation authorization according to the authentication result, which enhances the safety management of the operation. At the same time, the system has automatic detection and alarm functions, covering key detection items such as launch track deformation, rocket resistance, power supply system status, servo system status, communication system efficiency, boost status, position information and attitude information, ensuring the adequacy of launch preparation and improving the reliability and safety of the system. In addition, the control terminal realizes intelligent control function, which can automatically adjust the azimuth and pitch angle of the launcher according to the preset operation parameters, and automatically adjust the launch track spacing to adapt to different types of rockets, thereby reducing human errors and improving operation efficiency. The terminal also quickly obtains the model, size and parameter information of the rocket through QR code scanning, which significantly improves the speed and accuracy of loading and data processing. At the same time, the terminal has a safe firing range identification function, which can read and judge the safe firing range data, and make safety judgments based on the current firing angle to avoid potential safety risks. In addition, the control terminal supports remote uploading of operation logs and has a breakpoint resume function, ensuring timely data transmission and record integrity. These advantages make the terminal highly secure, automated, and accurate in actual applications, significantly improving the overall effect of weather modification operations.

[0093] The embodiment of the present application also discloses a shadow rocket launch control method.

[0094] Reference Figure 2 A human shadow rocket launch control method is applied to the human shadow rocket launch control terminal, and the control method includes: Step S101, receiving the identity information of the human shadow operator and performing user identity authentication, and authorizing the human shadow operator to access the user operation interface after the user identity authentication passes; Among them, the system receives the identity information of the shadow operator, and can usually verify the identity through face recognition or other biometric recognition methods. After the identity authentication is passed, the system authorizes the person to access the operation interface to ensure that only authorized personnel can operate the rocket launch control system.

[0095] Step S102, collecting real-time attitude information and operation status information of the shadow rocket launcher and ID information of the shadow rocket; The operation status information includes the position information of the shadow rocket launcher, the base status parameter information and the track deformation detection information, and the resistance status information and ID information of the shadow rocket on the shadow rocket launcher; It is understandable that real-time data collection can ensure that the status of the launch pad and rocket meet the launch requirements, provide reliable support for subsequent launch operations, and ensure that the system has a comprehensive grasp of the real-time status of the rocket launch pad and the properties of the rocket to ensure the safety and accuracy of the launch process.

[0096] Step S103, receiving the launcher target attitude parameters sent by the human shadow command platform; Specifically, the launcher target attitude parameters include target azimuth and pitch angle, which are set according to the mission requirements and are used to guide the launcher to adjust to a posture suitable for launch.

[0097] Step S104, determining whether the launcher target attitude parameters meet the preset safe firing range information; if not, jump to step S105; if yes, jump to step S106; The system compares the received target attitude parameters with the preset safe shooting range information to determine whether they are within the safe range. If they are within the safe shooting range, the system allows further adjustment; otherwise, it issues a warning and terminates the operation.

[0098] Step S105, issuing a warning and terminating the operation; Step S106, generating a launcher attitude adjustment instruction based on the real-time attitude information of the human shadow rocket launcher and the launcher target attitude parameters and sending it to the human shadow rocket launcher; Among them, the launcher attitude adjustment command includes an azimuth adjustment command and a pitch angle adjustment command; Specifically, the system calculates the adjustment amount based on the real-time attitude information of the launcher and the target attitude parameters, generates and issues attitude adjustment instructions, including azimuth and pitch angle adjustment instructions, and the launcher can automatically complete the attitude adjustment.

[0099] Step S107, detecting the operation status information of the shadow rocket launcher and the ID information of the shadow rocket; Step S108, determine whether the test is passed, if yes, jump to step S109; if no, jump to step S105; Step S109, sending ignition application information to the human shadow command platform; Specifically, the system detects the operating status information of the launch pad and the rocket ID information to determine whether it is in a normal state and whether it matches the launch mission. After the detection passes, the system sends an ignition application information to the command platform and waits for launch authorization.

[0100] Step S110, in response to the launch operation signal sent by the human shadow command platform, synchronously generate an ignition control instruction and send it to the human shadow rocket launcher; Among them, the system generates an ignition control instruction after receiving the launch operation signal from the command platform, and the instruction is transmitted to the launch pad to start the ignition program, thereby realizing the rocket launch.

[0101] Step S111, record the launch operation information and generate operation log information, and upload the operation log information to the human shadow command platform.

[0102] The system automatically records detailed information about the launch operation, including the time, location, method, ammunition type and amount of ammunition used, and generates a log, which is then uploaded to the command platform for data storage and analysis.

[0103] In the above implementation, the safety, accuracy and data traceability of rocket launch operations are achieved through the whole process management of identity authentication, data collection, attitude adjustment, status detection, ignition control and operation log. Among them, identity authentication ensures the security of operating authority, data collection provides real-time information support for attitude adjustment and status detection, attitude adjustment and safe firing range judgment ensure the accuracy and safety of launch, ignition control ensures that the launch is carried out under authorization, and operation log recording and uploading enable the launch operation to have complete data records and traceability. This technical solution significantly improves the automation and reliability of human shadow rocket launches, and provides comprehensive technical support and safety guarantees for human shadow rocket launches.

[0104] The human shadow rocket launch control terminal of the embodiment of the present application can implement any of the above-mentioned human shadow rocket launch control methods, and the specific working process of each step in the human shadow rocket launch control method can refer to the corresponding process in the above-mentioned terminal embodiment.

[0105] The embodiment of the present application also discloses a human shadow rocket launch control system.

[0106] A human shadow rocket launch control system, the launch control system includes a human shadow command platform, a human shadow rocket launcher loaded with human shadow rockets and the above-mentioned human shadow rocket launch control terminal, the human shadow rocket launch control terminal is respectively connected to the human shadow command platform and the human shadow rocket launcher.

[0107] In actual operation, the human shadow operator can scan the rocket body QR code by operating the rocket launch control terminal control interface, automatically obtain the rocket type information, and adjust the orbit inclusion circle diameter of the rocket launcher director to the appropriate state to match the projectile diameter and achieve rapid loading. The rocket launch control terminal can receive the human shadow operation parameters issued by the human shadow command platform, and transmit the operation instructions to the base controller of the rocket launcher through a wireless or wired network by operating the rocket launch control terminal control interface. After receiving the control instructions, the base controller executes the corresponding execution and transmits the rocket launcher status information back to the rocket launch control terminal and displays it synchronously. At the same time, the rocket launch control terminal encrypts the real-time status information and operation log information through the 4G / 5G network and transmits it to the human shadow command center.

[0108] It should be noted that before loading, the shadow operator should remotely shut down the power supply of the launcher through the rocket launch control terminal to cut off all possible power outputs to prevent accidental startup or safety accidents caused by current during loading. After loading is completed, the loaders evacuate to a safe area, and the shadow operator issues a resistance detection command through the rocket launch control terminal, and the system automatically detects the resistance value of each track of the launcher. The shadow operator can observe the test results through the control terminal. When the resistance test results of all tracks are normal, the fire control switch, boost and launch buttons of the ignition control part will automatically take effect to ensure the safety and reliability of the operation.

[0109] In the several embodiments provided in this application, it should be understood that the provided methods and systems can be implemented in other ways. For example, the system embodiments described above are only illustrative; for example, the division of a certain module is only a logical function division, and there may be other division methods in actual implementation, such as multiple modules can be combined or integrated into another system, or some features can be ignored or not executed.

[0110] It should be noted that in the above embodiments, the description of each embodiment has different emphases, and for parts that are not described in detail in a certain embodiment, reference can be made to the relevant descriptions of other embodiments.

[0111] The above are all preferred embodiments of the present application, and are not intended to limit the protection scope of the present application. Any feature disclosed in this specification (including the abstract and drawings), unless otherwise stated, can be replaced by other equivalent or alternative features with similar purposes. That is, unless otherwise stated, each feature is only an example of a series of equivalent or similar features.

Claims

1. A human shadow rocket launch control terminal, characterized in that: The launch control terminal is used to connect the human shadow command platform and the human shadow rocket launcher loaded with human shadow rockets, and the launch control terminal includes an identity authentication module, an operation information collection module, an operation control module, a launch control module and an operation log module; The identity authentication module is used to receive the identity information of the human shadow operator and perform user identity authentication, and authorize the human shadow operator to access the user operation interface after the user identity authentication is passed; The operation information acquisition module is used to collect the real-time posture information and operation status information of the human shadow rocket launcher and the ID information of the human shadow rocket; wherein the operation status information includes the position information, base state parameter information and track deformation detection information of the human shadow rocket launcher and the resistance state information and ID information of the human shadow rocket on the human shadow rocket launcher; The operation control module is used to receive the launcher target attitude parameters sent by the human shadow command platform; The operation control module is connected to the operation information acquisition module, and is also used to generate a launcher attitude adjustment instruction and send it to the human shadow rocket launcher according to the real-time attitude information of the human shadow rocket launcher and the target attitude parameter of the launcher; wherein the launcher attitude adjustment instruction includes an azimuth adjustment instruction and a pitch angle adjustment instruction; The launch control module is connected to the operation information collection module, and is used to detect the operation status information of the human shadow rocket launcher and the ID information of the human shadow rocket to obtain the detection result; The launch control module is further used to send ignition application information to the human shadow command platform when the detection result is a detection pass, generate an ignition control instruction in response to the launch operation signal sent by the human shadow command platform, and send it to the human shadow rocket launcher; The operation log module is used to record the launch operation information and generate operation log information, and upload the operation log information to the human shadow command platform.

2. A human shadow rocket launch control terminal according to claim 1, characterized in that , the identity authentication module includes: A face information collection unit, used to collect face information of shadow workers; An identity recognition and authentication unit, used to perform identity recognition and authentication based on the face information to obtain an identity recognition and authentication result; An authorization management unit is used to authorize the human shadow operator to access the user operation interface according to the identity recognition and authentication result.

3. A human shadow rocket launch control terminal according to claim 1, characterized in that ,The operation information collection module includes: A posture information acquisition unit, used to acquire real-time posture information of the shadow rocket launcher, wherein the posture information includes azimuth information and pitch angle information; A position information acquisition unit, used to acquire the position information of the human shadow rocket launcher; A base state parameter acquisition unit, used to acquire base state parameter information of the human shadow rocket launcher; A track deformation information acquisition unit, used to acquire track deformation detection information of the shadow rocket launcher; A resistance information acquisition unit, used to acquire resistance status information of the human shadow rocket on the human shadow rocket launcher; The rocket ID information collection unit is used to collect the ID information of the shadow rocket on the shadow rocket launcher.

4. A human shadow rocket launch control terminal according to claim 3, characterized in that: The job control module comprises: A target attitude parameter receiving unit is used to receive the launcher target attitude parameters sent by the human shadow command platform; wherein the launcher target attitude parameters include target azimuth parameters and target pitch angle parameters; A target attitude judgment unit is used to judge whether the target attitude parameters of the launcher meet the preset safe firing range information, and if so, output a target attitude qualified result; The attitude adjustment calculation unit calculates the launcher attitude adjustment parameters according to the real-time attitude information of the shadow rocket launcher and the launcher target attitude parameters in response to the qualified result of the target attitude; An attitude adjustment control unit is used to generate a launcher attitude adjustment control instruction according to the launcher attitude adjustment parameters and send it to the shadow rocket launcher.

5. The human shadow rocket launch control terminal according to claim 3, characterized in that: The launch control module comprises: An operation status information detection unit, used to detect whether the operation status information of the human shadow rocket launcher is in a normal state, and if so, output an operation status detection pass result; A rocket ID information detection unit is used to detect whether the ID information of the shadow rocket is matched successfully, and if so, output an ID information detection pass result; An ignition application unit, used for sending ignition application information to the human shadow command platform according to the operation status detection result and the ID information detection result; The ignition control unit generates an ignition control instruction in response to the launch operation signal sent by the human shadow command platform and sends it to the human shadow rocket launcher.

6. A human shadow rocket launch control terminal according to claim 5, characterized in that: The rocket ID information detection unit includes: A rocket parameter acquisition unit, configured to acquire corresponding rocket parameter information based on a preset database according to the rocket ID information; An ammunition verification unit, used to perform a comparison verification based on the rocket parameter information, and output an ammunition verification pass result after the verification passes; A rocket parameter sending unit, in response to the ammunition verification passing result, sends the rocket parameter information to the human shadow rocket launcher; The detection result output unit outputs the ID information detection pass result in response to the rocket parameter matching success signal fed back by the human shadow rocket launcher.

7. The human shadow rocket launch control terminal according to claim 1, characterized in that: The job log module includes: An operation log generating unit, used to record the launch operation information and generate the operation log information; the launch operation information includes the operation time, operation location, operation mode, ammunition model and ammunition quantity; The operation log uploading unit is used to upload the operation log information to the human shadow command platform.

8. A human shadow rocket launch control terminal according to any one of claims 1 to 6, characterized in that: The transmission control terminal also includes: The operation interface display module is used to display the user operation interface and provide human-computer interaction functions after the user identity authentication is passed; The safety shooting range display module is used to display the angle range of the preset safety shooting range information.

9. A human shadow rocket launch control method, characterized in that: A human shadow rocket launch control terminal applied to any one of claims 1 to 8, wherein the control method comprises: Receiving identity information of a human shadow operator and performing user identity authentication, and authorizing the human shadow operator to access a user operation interface after the user identity authentication passes; Collecting real-time attitude information and operation status information of the shadow rocket launcher and ID information of the shadow rocket; wherein the operation status information includes position information, base state parameter information and track deformation detection information of the shadow rocket launcher and resistance state information and ID information of the shadow rocket on the shadow rocket launcher; Receiving the launcher target attitude parameters sent by the human shadow command platform; Determining whether the target attitude parameters of the launcher meet the preset safe firing range information; If yes, then based on the real-time attitude information of the shadow rocket launcher and the target attitude parameters of the launcher, a launcher attitude adjustment instruction is generated and sent to the shadow rocket launcher; wherein the launcher attitude adjustment instruction includes an azimuth adjustment instruction and a pitch angle adjustment instruction; Detect the operating status information of the human shadow rocket launcher and the ID information of the human shadow rocket to determine whether the detection is passed. If so, send ignition application information to the human shadow command platform; In response to the launch operation signal sent by the human shadow command platform, an ignition control instruction is synchronously generated and sent to the human shadow rocket launcher; Record the launch operation information and generate operation log information, and upload the operation log information to the human shadow command platform.

10. A human shadow rocket launch control system, characterized in that: The launch control system includes a human shadow command platform, a human shadow rocket launcher loaded with human shadow rockets, and a human shadow rocket launch control terminal as described in any one of claims 1 to 8, and the human shadow rocket launch control terminal is respectively connected to the human shadow command platform and the human shadow rocket launcher.

Images