Ignition management system of hail prevention and rain enhancement rocket projectile and operation method thereof

Abstract

The application provides a kind of ignition management system of hail prevention and rain enhancement rocket and its operating method.The ignition management system of hail prevention and rain enhancement rocket is composed of hardware and software, wherein the hardware part is composed of electronic delay chip, password manager and safety lock; the software part is composed of password management platform, the electronic delay chip is installed inside the hail prevention and rain enhancement rocket, replaces the original ignition module, and the chip code, equipment code and launch password are injected inside; the password manager is used to store and transmit the relevant code information and the state information of hail prevention and rain enhancement rocket; the safety lock obtains the fusion code from the password manager, decrypts the fusion code into chip code, equipment code and launch password according to the agreement, and matches the chip code, equipment code and launch password of the electronic delay chip in the hail prevention and rain enhancement rocket in the launch link.The application can effectively enhance the control ability of artificial weather modification operation and improve the safety of hail prevention and rain enhancement rocket.

Description

TECHNICAL FIELD

[0001] The present application relates to weather modification operation and production of explosive materials, in particular to a kind of ignition management system of hail prevention and rain enhancement rocket. BACKGROUND

[0002] The existing rocket, in production, transportation, storage, use process must be strictly managed, formalities cumbersome, while reliability and safety are lower, and responsibility accident is prone to appear. SUMMARY

[0003] Therefore, the present application provides a kind of ignition management system of hail prevention and rain enhancement rocket and its operation method to solve the technical problems of low reliability and safety caused by traditional ignition mode in prior art.

[0004] In the first aspect, the present application provides a kind of ignition management system of hail prevention and rain enhancement rocket, which is composed of hardware and software, wherein the hardware part is composed of password manager, electronic delay chip and safety lock, and the software part is composed of password management platform;

[0005] The password manager is used to obtain chip code and rocket code and randomly generate launch password and inject into the electronic delay chip built in hail prevention and rain enhancement rocket during production, and then encrypt and combine chip code, rocket code and launch password into fusion code, and bind with rocket code and upload to password management platform;Rocket code is uploaded to password management platform after obtaining rocket code during operation, and then fusion code bound with rocket code is downloaded through password management platform;

[0006] The electronic delay chip is used to replace the original delay tube of initiating explosive, and is installed inside hail prevention and rain enhancement rocket;It can store and send the injected chip code, rocket code and launch password, and simultaneously collect and send real-time pitch angle and overload data of hail prevention and rain enhancement rocket and resistance of each ignition channel inside hail prevention and rain enhancement rocket;

[0007] The safety lock is used to decrypt the fusion code from the password manager, and match with chip code, rocket code and launch password in the electronic delay chip in launch link;At the same time, read and judge the real-time state and launch condition of hail prevention and rain enhancement rocket;

[0008] The password management platform is used for manufacturer platform part to report and approve chip code, rocket code and fusion code after production of hail prevention and rain enhancement rocket, and to report and approve operation before operation and download fusion code.

[0009] Further, the password manager is a production unit after production is completed by scanning the chip code and the rocket code of the two-dimensional code of the rocket code (injecting the chip code at the same time injecting the random and invisible launch password) corresponding to the rocket code, when the password manager reads the three codes in the electronic delay chip, the fusion code is automatically generated according to the national secret algorithm, the generated fusion code is bound and stored with the corresponding rocket code, all fusion codes will be automatically stored in an EXCEL table according to the order. When the production unit completes the production of the batch of rocket, the EXCEL table in the password manager is used as an attachment through the password management platform of the production unit entrance for acceptance declaration, and the fusion code of the rocket enters the database of the password management platform after the acceptance is passed.

[0010] Further, the password management platform is a production unit after production is completed by scanning the chip code and the rocket code of the two-dimensional code of the rocket code (injecting the chip code at the same time injecting the random and invisible launch password) corresponding to the rocket code, when the password manager reads the three codes in the electronic delay chip, the fusion code is automatically generated according to the national secret algorithm, the generated fusion code is bound and stored with the corresponding rocket code, all fusion codes will be automatically stored in an EXCEL table according to the order. When the production unit completes the production of the batch of rocket, the EXCEL table in the password manager is used as an attachment through the password management platform of the production unit entrance for acceptance declaration, and the fusion code of the rocket enters the database of the password management platform after the acceptance is passed.

[0011] Further, the password management platform is a production unit after production is completed by scanning the chip code and the rocket code of the two-dimensional code of the rocket code (injecting the chip code at the same time injecting the random and invisible launch password) corresponding to the rocket code, when the password manager reads the three codes in the electronic delay chip, the fusion code is automatically generated according to the national secret algorithm, the generated fusion code is bound and stored with the corresponding rocket code, all fusion codes will be automatically stored in an EXCEL table according to the order. When the production unit completes the production of the batch of rocket, the EXCEL table in the password manager is used as an attachment through the password management platform of the production unit entrance for acceptance declaration, and the fusion code of the rocket enters the database of the password management platform after the acceptance is passed.

[0012] Further, the password management platform is a production unit after production is completed by scanning the chip code and the rocket code of the two-dimensional code of the rocket code (injecting the chip code at the same time injecting the random and invisible launch password) corresponding to the rocket code, when the password manager reads the three codes in the electronic delay chip, the fusion code is automatically generated according to the national secret algorithm, the generated fusion code is bound and stored with the corresponding rocket code, all fusion codes will be automatically stored in an EXCEL table according to the order. When the production unit completes the production of the batch of rocket, the EXCEL table in the password manager is used as an attachment through the password management platform of the production unit entrance for acceptance declaration, and the fusion code of the rocket enters the database of the password management platform after the acceptance is passed.

[0013] Further, the security lock is a fusion code that can obtain job permission and issue by external password manager, the fusion code is solved by algorithm to corresponding chip code, rocket code and launch password, and is matched with the code in the launch link. The rocket that matches successfully will allow launching, and the rocket that does not match successfully will be stationary for launching. At the same time, the security lock can detect the state information of each channel resistance, launch pitch angle and power of the rocket in real time, and determine the launch condition according to the state information, and report the related job information such as rocket code, launch angle, launch time and launch latitude and longitude to the password management platform in real time when the job is completed.

[0014] Further, the electronic delay chip is loaded on the rocket, and is connected with each ignition channel in the rocket respectively. When connected with the security lock, the resistance value of each ignition channel, the launch pitch angle of the hail suppression and rain enhancement rocket and the capacitance capacity in the electronic delay chip are sent to the security lock in real time. At the same time, the job instruction containing the delay time and overload parameter of each ignition channel is received from the security lock, and each channel ignition operation is performed according to the setting of the delay time and overload parameter of each ignition channel issued.

[0015] Further, the password manager includes a processing module, a two-dimensional code scanning module, a display module, a battery, a power module, a storage module and an injection module, the processing module is connected with the two-dimensional code scanning module, the display module, the power module, the storage module and the injection module respectively; the two-dimensional code scanning module is connected with a two-dimensional code picture externally; the power module is connected with an external power supply externally and a battery internally; the storage module is connected with a password management platform externally; and the injection module is connected with an electronic delay chip externally.

[0016] Further, the electronic delay chip includes a processing module, an overload module, a capacitance module, a resistance detection module and a delay ignition module; the processing module is connected with a security lock externally and connected with the overload module, the capacitance module, the resistance detection module and the delay ignition module internally; the capacitance module is connected with the delay ignition module; and the resistance detection module and the delay ignition module are connected with other ignition channels in the rocket externally.

[0017] Further, the security lock includes a processing module, a key module, a fingerprint module, a battery, a power module, a display module and a communication module; the processing module is connected with a password manager and a hail suppression and rain enhancement rocket externally and connected with the key module, the fingerprint module, the power module, the display module and the communication module internally; the power module is connected with an external power supply externally and connected with a battery internally; and the communication is connected with a wireless network externally;

[0018] Further, the password management platform comprises a manufacturer platform, a user platform and a management platform; the management platform is connected to a management unit externally and connected to the manufacturer platform and the user platform internally; the manufacturer platform is connected to a production unit externally; and the user platform is connected to a work unit externally.

[0019] In a second aspect, the present application provides an operation method of the ignition management system of the hail prevention and rain enhancement rocket projectile, and the operation method comprises:

[0020] The production unit reads the information of the chip code and the rocket projectile code produced according to the coding rule through the password manager after completing the production of the ammunition, and randomly generates a launch password to be injected into the electronic delay chip;

[0021] The password manager records the information of the chip code, the rocket projectile code and the launch password of the rocket projectile, and combines the above three code information into a fusion code through an encryption rule, and stores the chip code and the rocket projectile code in the form of an EXCEL table (one EXCEL table can store in batches, and each row is a rocket projectile data) in the password manager;

[0022] The production unit completes the product group batch, and reports the information of the three codes combined in the password manager through the password management platform for acceptance. The management unit receives the reporting application for acceptance and approval, and the related ammunition information automatically enters the finished product warehouse after the acceptance, and the unaccepted ammunition information will be returned for processing;

[0023] When the user unit obtains the work demand, the rocket projectile code on the rocket projectile shell required for this work is read through the password manager and stored in the password manager in the form of an EXCEL table (one EXCEL table can store in batches, and each row is a rocket projectile data);

[0024] The user unit reports the rocket projectile code stored in the password manager through the password management platform, and the corresponding fusion code of the reported rocket projectile code is issued after the report is passed, and the fusion code is transmitted to the safety locker after being stored in the password manager;

[0025] The safety locker decrypts the received fusion code into the corresponding chip code, rocket projectile code and launch password through the decryption rule, and matches the chip code, rocket projectile code and launch password existing in the launch link, and the rocket projectile that matches successfully can be launched. At the same time, the safety locker will combine the real-time state of the electronic delay chip in the rocket projectile returned at the work site to determine whether the rocket projectile meets the work requirements;

[0026] The safety lock determines that the operation condition is met and the code matches, and then the launch command is issued. The electronic delay chip receives the launch command and delays the ignition for a specified time. If the overload parameter of the rocket is set, the subsequent delay ignition command will not be effective if the agreed overload parameter is not met.

[0027] The safety lock records the operation parameters of each rocket, such as rocket code, fusion code, launch time, launch angle, launch point latitude and longitude, and rocket resistance, and uploads the data to the password management platform.

[0028] Further, the operation method further comprises:

[0029] After obtaining the operation demand, the user unit scans the two-dimensional code on the rocket shell through the password manager to obtain the rocket code of the rocket used in this operation;

[0030] Then connect the password manager with the computer, and upload the obtained rocket code to the password management platform through the user platform in the password management platform for operation application;

[0031] The management platform in the password management platform receives the operation application and performs operation approval. The fusion code corresponding to the rocket code submitted during the operation application is encrypted and issued back to the account of the application after the approval. The account downloads the fusion code into the password manager. The application is not passed, and the information of prohibiting operation is issued to the user account of the application;

[0032] The password manager is connected with the safety lock and transmits the fusion code to the safety lock. The safety lock receives the fusion code and decrypts it according to the agreement. After decryption, the chip code, launch password and rocket code are obtained and saved online (the three codes saved should not be cleared in the case of the safety lock not being turned off);

[0033] The safety lock matches the rocket code in the three codes with the rocket code in the ignition link before operation. If they match, the corresponding launch command is issued through the ignition link. The electronic delay chip in the rocket receives the launch command and matches it with its own launch command. If the launch password matches, the electronic delay chip allows the safety lock to operate, and the safety lock displays the matching successful rocket; if the launch password does not match, the electronic delay chip refuses to be operated by the safety lock, and the safety lock displays the matching failed rocket;

[0034] According to the safety locker, the launch instruction of the rocket projectile is sent according to the working site condition, and the electronic delay chip in the rocket projectile judges whether the launch pitch angle of the position of the rocket projectile meets the launch requirement on site.If the launch pitch angle meets the requirement, the rocket projectile is launched normally; if the launch pitch angle does not meet the requirement, the rocket projectile cancels the launch, and needs to be adjusted to the launch pitch angle for re-launching;

[0035] After the rocket projectile launch instruction is executed, the electronic delay chip in the rocket projectile judges whether the acceleration value of the rocket projectile meets the requirement on site.If the acceleration value meets the requirement, the electronic delay chip ignites each channel according to the specified delay time; if the acceleration value does not meet the requirement, the electronic delay chip cancels the delay operation of all channels.

[0036] Compared with the prior art, the beneficial effects of the ignition management system of the hail prevention and rain enhancement rocket projectile and the operation method thereof are as follows: first, by adopting the national secret algorithm as the generation means of the fusion code, the reliability and safety of the fusion code in the use process are effectively guaranteed; second, the electronic delay chip built in the hail prevention and rain enhancement rocket projectile can effectively and reliably obtain the resistance value of each ignition channel of the hail prevention and rain enhancement rocket projectile, and provide a judgment basis for whether the hail prevention and rain enhancement rocket projectile is qualified; third, by setting the overload module on the electronic delay chip, the electronic delay chip can reliably obtain the pitch angle and overload parameters of the position of the hail prevention and rain enhancement rocket projectile, and transmit the pitch angle data to the safety locker, the safety locker can set the pitch angle data to determine whether to allow launching, and the electronic delay chip can set the overload parameters to determine whether to allow delay ignition after launching; in addition, by setting the capacitor module on the electronic delay chip, the electronic delay chip has the energy storage function, and can provide energy for subsequent delay ignition after being separated from the safety locker; finally, by setting the two-dimensional code scanning module on the password manager, the password manager has the functions of automatically reading the chip code and the rocket projectile code, without manual input and confirmation, and the national secret algorithm is set in the processing module in the password manager, so that the password manager generates the fusion code through the national secret algorithm under the condition that the chip code, the rocket projectile code and the launch password are complete, and binds the fusion code with the rocket projectile code, without manual input and confirmation, and the accuracy and reliability of the code are ensured.

[0037] The ignition management system of the hail prevention and rain enhancement rocket projectile and the operation method thereof, by setting the fingerprint module on the safety locker, the safety locker has the function of fingerprint identification, and can effectively confirm and record the real identity of the operator. By setting the communication module on the safety locker, the safety locker has the communication function, and can real-time and reliably return the operation parameters to the password management platform. BRIEF DESCRIPTION OF DRAWINGS

[0038] Figure 1 Structure diagram of the ignition management system of the hail prevention and rainfall enhancement rocket projectile shown in the figure;

[0039] Figure 2 Structure diagram of the password manager of the ignition management system of the hail prevention and rainfall enhancement rocket projectile shown in the figure; Figure 1

[0040] Figure 3 Structure diagram of the electronic delay chip of the ignition management system of the hail prevention and rainfall enhancement rocket projectile shown in the figure; Figure 1

[0041] Figure 4 Structure diagram of the safety lock of the ignition management system of the hail prevention and rainfall enhancement rocket projectile shown in the figure; Figure 1

[0042] Figure 5 Structure diagram of the password management platform of the ignition management system of the hail prevention and rainfall enhancement rocket projectile shown in the figure; Figure 1

[0043] Figure 6 Working principle diagram of the ignition management system of the hail prevention and rainfall enhancement rocket projectile shown in the figure; Figure 1

[0044] Figure 7 Operation flow diagram of the ignition management system of the hail prevention and rainfall enhancement rocket projectile shown in the figure. Figure 1 DETAILED DESCRIPTION In order to facilitate the understanding of the present application, the present application will be described in more detail below with reference to the relevant drawings. The preferred embodiments of the present application are shown in the drawings. However, the present application can be implemented in many different forms and is not limited to the embodiments described herein. On the contrary, the purpose of providing these embodiments is to make the disclosure of the present application more thorough and comprehensive.

[0045] Please refer to

[0046] The present application provides an ignition management system of a hail prevention and rainfall enhancement rocket projectile, which is composed of hardware and software, wherein the hardware part is composed of a password manager, an electronic delay chip and a safety lock, and the software part is composed of a password management platform; Figures 1-7 The password manager is used to obtain the chip code and the rocket projectile code and randomly generate a launch password during production, and inject the launch password into the electronic delay chip built in the hail prevention and rainfall enhancement rocket projectile, and encrypt and combine the chip code, the rocket projectile code and the launch password into a fusion code, and then upload the fusion code bound with the rocket projectile code to the password management platform; during operation, the rocket projectile code is obtained and uploaded to the password management platform, and then the fusion code bound with the rocket projectile code is downloaded through the password management platform;

[0047] The present application has the advantages that the ignition management system of the hail prevention and rainfall enhancement rocket projectile is composed of hardware and software, and the hardware part is composed of a password manager, an electronic delay chip and a safety lock, and the software part is composed of a password management platform, which can realize the automatic management of the launch password of the hail prevention and rainfall enhancement rocket projectile, and can realize the automatic management of the launch password of the hail prevention and rainfall enhancement rocket projectile.​​​​​

[0048] The electronic delay chip is used to replace the original delay tube of the pyrotechnic product, and is installed in the inside of the hail prevention and rain enhancement rocket projectile; can store and send the injected chip code, rocket projectile code and launch password, and at the same time collect and send the real-time pitch angle and overload data of the hail prevention and rain enhancement rocket projectile and the resistance of each ignition channel in the hail prevention and rain enhancement rocket projectile;

[0049] The security locker is used to decrypt the fusion code from the password manager, and match the chip code, rocket projectile code and launch password in the electronic delay chip in the launch link; at the same time, read and judge the real-time state and launch condition of the hail prevention and rain enhancement rocket projectile;

[0050] The password management platform is used for the chip code, rocket projectile code and fusion code declaration and approval after the production of the hail prevention and rain enhancement rocket projectile, and the operation declaration and approval before the operation and the download of the fusion code.

[0051] Further, the password manager is used for the production unit to scan the two-dimensional code of the chip code and the rocket projectile code after the production is completed, and to inject the corresponding chip code of the rocket projectile code (inject the random and invisible launch password at the same time), when the password manager reads the three codes in the electronic delay chip, the fusion code is automatically generated according to the national secret algorithm, the generated fusion code is bound and stored with the corresponding rocket projectile code, and all the fusion codes are automatically stored in an EXCEL table according to the order. When the production unit completes the production of the rocket projectile, the EXCEL table in the password manager is used as an attachment through the password management platform of the production unit entrance for product acceptance, and the fusion code of the rocket projectile is changed into the database of the password management platform after the acceptance is passed.

[0052] Further, the password management platform is used for the production unit to scan the two-dimensional code of the chip code and the rocket projectile code after the production is completed, and to inject the corresponding chip code of the rocket projectile code (inject the random and invisible launch password at the same time), when the password manager reads the three codes in the electronic delay chip, the fusion code is automatically generated according to the national secret algorithm, the generated fusion code is bound and stored with the corresponding rocket projectile code, and all the fusion codes are automatically stored in an EXCEL table according to the order. When the production unit completes the production of the rocket projectile, the EXCEL table in the password manager is used as an attachment through the password management platform of the production unit entrance for product acceptance, and the fusion code of the rocket projectile is changed into the database of the password management platform after the acceptance is passed.

[0053] Further, the password manager is used by the unit to obtain the job requirements after the password manager scans the rocket shell required for this job Rocket code, Rocket code will be stored in an EXCEL table according to the order. The job personnel will use the EXCEL table in the password manager as an attachment through the password management platform user unit entrance to report the job, and the corresponding fusion code (also in EXCEL table format) will be issued after the job approval, and the EXCEL table with the fusion code will be downloaded to the password manager, and the password manager will be connected with the security locker for fusion code transmission.

[0054] Further, the password management platform is used by the unit to obtain the corresponding rocket code by scanning the rocket shell two-dimensional code on the rocket shell required for this job through the password manager, and the job is reported through the user platform in the password management platform. The management unit performs approval operation through the management platform in the password management platform. The job permit approved will extract the corresponding fusion code of the rocket code from the database and issue it to the account of the job report. The job personnel will download the EXCEL table containing the fusion code to the password manager for further job operation. The job permit not approved will not issue the fusion code.

[0055] Further, the security locker can obtain the job permit and issue the fusion code by connecting the password manager. The fusion code is solved by algorithm to obtain the corresponding chip code, rocket code and launch password, and matched with the code in the launch link. The rocket that matches successfully will allow launching, and the rocket that does not match successfully will be stationary for launching. At the same time, the security locker can detect the state information of each channel resistance, launch pitch angle and power of the rocket in real time, and determine the launch condition according to the state information. When the job is completed, the related job information such as rocket code, launch angle, launch time and launch longitude and latitude is reported to the password management platform in real time.

[0056] Further, the electronic delay chip is loaded on the rocket, and is connected to each ignition channel inside the rocket. When connected to the security locker, the resistance value of each ignition channel, the launch pitch angle of the hail suppression and rain enhancement rocket and the capacitance capacity in the electronic delay chip are sent to the security locker in real time. At the same time, it receives the job instruction containing the delay time and overload parameter of each ignition channel sent from the security locker, and performs each channel ignition operation according to the setting of the delay time and overload parameter of each ignition channel issued.

[0057] The password manager includes a processing module, a two-dimensional code scanning module, a display module, a battery, a power module, a storage module and an injection module, the processing module is connected with the two-dimensional code scanning module, the display module, the power module, the storage module and the injection module respectively, the two-dimensional code scanning module is connected with a two-dimensional code picture externally, the power module is connected with an external power supply externally and the battery internally, the storage module is connected with a password management platform externally, and the injection module is connected with an electronic delay chip externally.

[0058] Please refer to Figure 2 The processing module in the password manager is used for processing signals of various modules in the password manager, the two-dimensional code scanning module is used for acquiring external two-dimensional code information, the display module is used for displaying various data externally, the battery is used for storing power required by the password manager when being used independently, the power module is used for providing power supply guarantee for various modules of the password manager, the storage module is used for storing relevant information required when producing, reporting work and downloading work, and the injection module is used for injection operation of the electronic delay chip on production of a rocket projectile code, a chip code and a launch password.

[0059] The electronic delay chip includes a processing module, an overload module, a capacitor module, a resistance detection module and a delay ignition module, the processing module is connected with a safety lock externally and connected with the overload module, the capacitor module, the resistance detection module and the delay ignition module internally, the capacitor module is connected with the delay ignition module, and the resistance detection module and the delay ignition module are connected with other ignition channels in the rocket projectile externally.

[0060] Please refer to Figure 3 The processing module in the electronic delay chip is used for processing signals of various modules in the electronic delay chip, the overload module is used for acquiring pitch angle information when the rocket projectile is launched and overload information after the rocket projectile is launched, the capacitor module is used for storing ignition power required by various ignition channels of the rocket projectile, the resistance detection module is used for resistance detection operation of various ignition channels of the rocket projectile, and the delay ignition module is used for delay ignition operation of various ignition channels of the rocket projectile.

[0061] The safety lock includes a processing module, a key module, a fingerprint module, a battery, a power module, a display module and a communication module, the processing module is connected with a password manager and a hail prevention and rain enhancement rocket projectile externally and connected with the key module, the fingerprint module, the power module, the display module and the communication module internally, the power module is connected with an external power supply externally and connected with the battery internally, and the communication module is connected with a wireless network externally.

[0062] Please refer to Figure 4The processing module in the safety lock is used for processing signals of various modules in the safety lock; the key module is used for obtaining various operation instructions inputted by an external person; the fingerprint module is used for storing and identifying fingerprint information of an operator; the battery is used for storing power required when the password manager is independently used; the power module is used for providing power supply guarantee for various modules of the password manager; the display module is used for displaying various data externally; and the communication module is used for reporting relevant operation information externally.

[0063] Please refer to Figure 5 The password management platform comprises a manufacturer platform, a user platform and a management platform; the management platform is connected with a management unit externally and connected with the manufacturer platform and the user platform internally; the manufacturer platform is connected with a production unit externally; and the user platform is connected with an operation unit externally.

[0064] The application further provides an operation method of the ignition management system of the hail prevention and rain enhancement rocket projectile, and the operation method comprises the following steps:

[0065] After the production unit completes ammunition production, the information of the chip code and the rocket projectile code produced according to the coding rule is read by the password manager, and a launch password is randomly generated and injected into the electronic delay chip;

[0066] The password manager records the information of the chip code, the rocket projectile code and the launch password of the rocket projectile, and combines the above three code information into a fusion code through an encryption rule, and stores the chip code and the rocket projectile code in the password manager in the format of an EXCEL table (one EXCEL table can store in batches, and each row is a rocket projectile data);

[0067] After the production unit completes product grouping, the password management platform is used to report the information of the three codes combined in the password manager for acceptance. After receiving the reporting application, the management unit carries out acceptance examination and approval, and after the acceptance is passed, the relevant ammunition information automatically enters the finished product warehouse, and the unaccepted ammunition information is returned for processing;

[0068] When the user unit obtains operation demand, the rocket projectile code on the rocket projectile shell required for this operation is read by the password manager and stored in the password manager in the format of an EXCEL table (one EXCEL table can store in batches, and each row is a rocket projectile data);

[0069] The user unit reports the rocket projectile code stored in the password manager through the password management platform, and after the report is passed, the fusion code corresponding to the reported rocket projectile code is issued, and the fusion code is transmitted to the safety lock after being stored in the password manager;

[0070] The security lock decrypts the received fusion code into corresponding chip code, rocket code and launch password by decryption rule, and matches with the chip code, rocket code and launch password existing in the launch link. The rocket that matches successfully can be launched. Meanwhile, the security lock combines the real-time state of the electronic delay chip in the rocket returned in the operation site to determine whether the rocket meets the operation requirements;

[0071] The security lock determines the operation conditions meet and the code matching passes, and then issues a launch instruction. The electronic delay chip delays ignition for each path according to the specified delay time after receiving the launch instruction. If there is a set rocket overload parameter, the subsequent delay ignition instruction is invalid if the agreed overload parameter is not reached;

[0072] The security lock records the operation parameters of each rocket operation, such as rocket code, fusion code, launch time, launch angle, launch point latitude and longitude, rocket resistance value, etc., and uploads the data to the password management platform;

[0073] Further, the operation method further includes that the user unit obtains the rocket code of the rocket used in this operation by scanning the two-dimensional code on the rocket shell through the password manager after obtaining the operation demand;

[0074] Then the password manager is connected with the computer, and the rocket code obtained is uploaded to the password management platform through the user platform in the password management platform for operation application;

[0075] The management platform in the password management platform performs operation approval after receiving the operation application. The fusion code corresponding to the rocket code submitted in the operation application is encrypted and issued back to the account of the application after the approval. The account downloads the fusion code into the password manager. The application is not passed, and the information of prohibiting operation is issued to the user account of the application;

[0076] The password manager is connected with the security lock and transmits the fusion code to the security lock. The security lock decrypts the received fusion code according to the agreement, obtains the chip code, launch password and rocket code after decryption, and saves the three codes online (the saved three codes should not be cleared in the case that the security lock is not turned off);

[0077] The safety lock matches the rocket code in the three codes with the rocket code in the ignition link before operation. If the match is consistent, the corresponding launch command is issued through the ignition link. The electronic delay chip in the rocket matches the received launch command with its own launch command. If the launch password matches, the electronic delay chip allows the safety lock to operate and the safety lock displays the matching successful rocket; if the launch password does not match, the electronic delay chip refuses to be operated by the safety lock and the safety lock displays the matching failed rocket.

[0078] According to the operation site situation, the safety lock issues the launch command of the rocket. The electronic delay chip in the rocket judges whether the launch pitch angle of the position where the rocket is located meets the launch requirement. If the launch pitch angle meets the requirement, the rocket is launched normally; if the launch pitch angle does not meet the requirement, the rocket cancels the launch and needs to adjust the launch pitch angle for re-launching.

[0079] After the rocket launch command is executed, the electronic delay chip in the rocket judges whether the acceleration value of the rocket meets the requirement. If the acceleration value meets the requirement, the electronic delay chip ignites each channel according to the specified delay time; if the acceleration value does not meet the requirement, the electronic delay chip cancels the delay operation of all channels.

[0080] Compared with the prior art, the ignition management system of hail prevention and rain enhancement rocket and the operation method thereof have the following beneficial effects: first, by adopting the national secret algorithm as the generation means of the fusion code, the reliability and safety of the fusion code in use are effectively ensured; second, by the electronic delay chip built in the hail prevention and rain enhancement rocket, the resistance of each ignition channel of the hail prevention and rain enhancement rocket can be effectively and reliably obtained, thereby providing a basis for determining whether the hail prevention and rain enhancement rocket is qualified; third, by setting the overload module on the electronic delay chip, the electronic delay chip can reliably obtain the pitch angle and overload parameters of the position of the hail prevention and rain enhancement rocket and transmit the pitch angle data to the safety locker, and the safety locker can determine whether to allow the launch according to the pitch angle data, and the electronic delay chip can determine whether to allow the delay ignition after the launch according to the overload parameters; in addition, by setting the capacitor module on the electronic delay chip, the electronic delay chip has the energy storage function and can provide energy for the subsequent delay ignition after being separated from the safety locker; finally, by setting the two-dimensional code scanning module on the password manager, the password manager has the function of automatically reading the chip code and the rocket code, without manual input and confirmation, and by setting the processing module in the password manager to meet the national secret algorithm, the password manager can automatically generate the fusion code through the national secret algorithm under the condition that the chip code, the rocket code and the launch password are complete, and the fusion code is bound with the rocket code, without manual input and confirmation, thereby ensuring the accuracy and reliability of the code.

[0081] The ignition management system of hail prevention and rain enhancement rocket and the operation method thereof of the present application have the fingerprint module on the safety locker, so that the safety locker has the fingerprint identification function and can effectively confirm and record the real identity of the operator. The safety locker has the communication function by setting the communication module on the safety locker, and can real-timely and reliably return the operation parameters to the password management platform.

[0082] The above embodiments only express the embodiments of the present application, and the description is more specific and detailed, but it cannot be understood as the limitation of the patent scope of the present application. It should be noted that, for ordinary skilled in the art, without departing from the concept of the present application, a number of modifications and improvements can be made, which are all within the protection scope of the present application. Therefore, the protection scope of the patent of the present application should be subject to the appended claims.

Claims

1. A firing management system for hail suppression and rain enhancement rockets, characterized by: It is composed of hardware and software, the hardware part is composed of a password manager, an electronic delay chip and a security locker, and the software part is composed of a password management platform; The password manager is used for obtaining a chip code and a rocket code and randomly generating a launch password and injecting them into the electronic delay chip of the hailproof and rain-increasing rocket at the production time, and encrypting and combining the chip code, the rocket code and the launch password into a fusion code and uploading the fusion code bound with the rocket code to the password management platform, obtaining the rocket code at the operation time and uploading it to the password management platform, and downloading the fusion code bound with the rocket code through the password management platform; The electronic delay chip is used for replacing the original delay tube of the initiating explosive, and is installed inside the hailproof and rain-increasing rocket, and can store and send the injected chip code, rocket code and launch password, collect and send real-time pitch angle and overload data of the hailproof and rain-increasing rocket, and collect resistances of each ignition channel inside the hailproof and rain-increasing rocket; The security locker is used for decrypting the fusion code from the password manager, and matching the chip code, the rocket code and the launch password in the electronic delay chip in the launch link, and reading and judging real-time state and launch conditions of the hailproof and rain-increasing rocket; The password management platform is suitable for declaring and approving the chip code, the rocket code and the fusion code after the hailproof and rain-increasing rocket is produced, and is also suitable for the platform for declaring and approving before operation and downloading the fusion code; The password manager comprises a processing module, a two-dimensional code scanning module, a display module, a battery, a power module, a storage module and an injection module, the processing module is connected with the two-dimensional code scanning module, the display module, the power module, the storage module and the injection module respectively, the two-dimensional code scanning module is connected with a two-dimensional code picture externally, the power module is connected with an external power supply externally and connected with the battery internally, the storage module is connected with the password management platform externally, and the injection module is connected with the electronic delay chip externally; The electronic delay chip comprises a processing module, an overload module, a capacitor module, a resistance detection module and a delay ignition module, the processing module is connected with the security locker externally and connected with the overload module, the capacitor module, the resistance detection module and the delay ignition module internally respectively, the capacitor module is connected with the delay ignition module, and the resistance detection module and the delay ignition module are connected with other ignition channels in the rocket externally; The security locker comprises a processing module, a key module, a fingerprint module, a battery, a power module, a display module and a communication module, the processing module is connected with the password manager and the hailproof and rain-increasing rocket externally and connected with the key module, the fingerprint module, the power module, the display module and the communication module internally respectively, the power module is connected with an external power supply externally and connected with the battery internally, and the communication module is connected with a wireless network externally.

2. The ignition management system for hail suppression and precipitation enhancement rocket projectile of claim 1, wherein: The password manager reads the corresponding rocket shell code by scanning the chip code and the rocket shell code two-dimensional code after production is completed, and when the password manager reads three codes in the electronic delay chip, a fusion code is automatically generated according to the national secret algorithm, the generated fusion code is bound and stored with the corresponding rocket shell code, and all fusion codes are stored according to the order, when the production unit completes the rocket production, the data in the password manager is used as an accessory to report the acceptance through the production unit entrance of the password management platform, and after the acceptance, the fusion code of the rocket enters the database of the password management platform.

3. The ignition management system for hail-suppression and rain-enhancement rockets according to claim 2, characterized in that: The password management platform is used for production reporting of the same batch of rockets and fusion codes through the manufacturer platform in the password management platform after production is completed, the management unit performs approval operation through the management platform in the password management platform, the approved product is stored in the database, and the unqualified product is not stored in the database.

4. The ignition management system for hail suppression and rain enhancement rocket projectile of claim 3, wherein: The password manager is used for scanning the rocket shell code of the rocket shell required for the operation by the password manager after the user unit obtains the operation demand, the rocket shell code is automatically stored according to the order, the data in the password manager is used as an accessory to report the operation through the user unit entrance of the password management platform, the corresponding fusion code is issued after the operation is approved, the data containing the fusion code is downloaded to the password manager, and the password manager is connected with the safety lock for fusion code transmission.

5. The ignition management system for hail suppression and rain enhancement rocket projectile of claim 4, wherein: The password management platform is used for scanning the rocket shell code of the rocket shell required for the operation by the password manager after the user unit obtains the operation demand, the rocket shell code is automatically stored according to the order, the data in the password manager is used as an accessory to report the operation through the user unit entrance of the password management platform, the corresponding fusion code is issued after the operation is approved, the data containing the fusion code is downloaded to the password manager, and the password manager is connected with the safety lock for fusion code transmission.

6. The ignition management system for hail-suppression and rain-enhancement rockets according to claim 5, characterized in that: The safety lock is used for obtaining the fusion code of the operation permission through the external password manager, the fusion code is solved by an algorithm to obtain the corresponding chip code, rocket shell code and launch password, and the codes are matched with the codes in the launch link, the rocket shell that is successfully matched is allowed to be launched, the rocket shell that is not successfully matched is static for launching, the safety lock detects the state information of each channel of the rocket shell in real time, and determines the launch condition according to the state information, and reports the rocket shell code, launch angle, launch time and launch longitude and latitude and other related operation information to the password management platform in real time after the operation is completed.

7. The ignition management system for hail-suppression and rain-enhancement rockets according to claim 6, characterized in that: The electronic delay chip is loaded on the rocket projectile and is connected with each ignition channel in the rocket projectile. When connected with the safety lock, the resistance value of each ignition channel, the launch pitch angle of the hail and rain increasing rocket projectile and the capacitance capacity in the electronic delay chip are acquired and sent to the safety lock in real time. Meanwhile, the operation instruction containing the delay time and overload parameter of each ignition channel is received from the safety lock, and each channel ignition operation is performed according to the set delay time and overload parameter.

8. A method of operating the ignition management system of the hail-suppression and rain-enhancement rocket projectile according to any one of claims 1 to 7, characterized in that: The operation method comprises: After the production unit completes the production of the ammunition, the chip code and the rocket projectile code produced according to the coding rule are read by the password manager, and the launch password is randomly generated and injected into the electronic delay chip; The password manager records the chip code, the rocket projectile code and the launch password of the rocket projectile, and combines the above three code information into a fusion code through the encryption rule, and stores the corresponding chip code and rocket projectile code in the password manager; After the production unit completes the product grouping, the three-in-one information stored in the password manager is reported for acceptance through the password management platform, and the management unit performs acceptance inspection after receiving the reporting application. If the acceptance is passed, the related ammunition information automatically enters the finished product warehouse, and if the acceptance is not passed, the related ammunition information is returned for processing; When the user unit obtains the operation demand, the rocket projectile code on the rocket projectile shell required for this operation is read by the password manager and stored in the password manager; The user unit reports the rocket projectile code stored in the password manager through the password management platform, and the corresponding fusion code of the reported rocket projectile code is issued after the report is passed. The fusion code is transmitted to the safety lock after being stored in the password manager; The safety lock decrypts the received fusion code into the corresponding chip code, rocket projectile code and launch password through the decryption rule, and matches the chip code, rocket projectile code and launch password existing in the launch link. The rocket projectile that passes the matching can be launched, and the safety lock will determine whether the rocket projectile meets the operation requirements by combining the real-time state of the electronic delay chip in the rocket projectile returned in the operation site: After the safety lock determines that the operation conditions meet the requirements and the coding matches are passed, the launch instruction is issued. The electronic delay chip delays the ignition of each channel according to the specified delay time after receiving the launch instruction. If there is a set overload parameter of the rocket projectile, the subsequent delay ignition instruction will not be effective if the overload parameter is not met; The safety lock records the operation parameters of each rocket projectile during the operation, and uploads the data to the password management platform.

9. The method of operation of claim 8, wherein: The operation method further comprises: After the user unit obtains the operation demand, the rocket projectile code of the rocket projectile required for this operation is obtained by scanning the two-dimensional code on the rocket projectile shell through the password manager; Then, the password manager is connected with the computer, and the rocket projectile code obtained is uploaded to the password management platform through the user platform in the password management platform for operation application. The management platform in the password management platform carries out job approval after receiving the job application, and the fusion code corresponding to the rocket code submitted by the job application is encrypted and issued back to the account of the application after the approval, and the account downloads the fusion code into the password manager, and the application is not passed. The information of prohibiting the job is issued to the user account of the application; The password manager is connected with the security locker in a wired manner and transmits the fusion code to the security locker, and the security locker decrypts the received fusion code according to the agreement, obtains the chip code, the launch password and the rocket code after decryption, and saves the three codes online; The security locker matches the rocket code in the three codes with the rocket code of the rocket in the ignition link before the operation, and if the matching is consistent, the corresponding launch instruction is issued through the ignition link, the electronic delay chip in the rocket receives the launch instruction and matches it with the launch instruction of itself, if the launch password matches, the electronic delay chip allows the security locker to operate and the security locker displays the matching successful rocket, if the launch password does not match, the electronic delay chip refuses to be operated by the security locker and the security locker displays the matching failed rocket; According to the operation site situation, the security locker issues the launch instruction to the rocket, and the electronic delay chip in the rocket judges whether the launch pitch angle of the position of the rocket meets the launch requirement, if the launch pitch angle meets the requirement, the rocket is launched normally, if the launch pitch angle does not meet the requirement, the rocket cancels the launch and needs to adjust the launch pitch angle for re-launching; After the execution of the rocket launch instruction, the electronic delay chip in the rocket judges whether the acceleration value of the rocket meets the requirement, if the acceleration value meets the requirement, the electronic delay chip ignites each channel according to the specified delay time, if the acceleration value does not meet the requirement, the electronic delay chip cancels the delay operation of all channels.

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