Portable running-firing test-launch control system

By designing a portable, continuous-fire measurement and control system, and adopting a multi-layered storage box structure and communication bus, the problems of low operating efficiency and poor portability of existing measurement and control systems are solved, enabling efficient control and convenient deployment of multiple targets.

CN223741334UActive Publication Date: 2025-12-30SHIJIAZHUANG HONGJING CULTURAL COMM CO LTD
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Patent Information

Application Number
CN202520374522.1
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-03-05
Publication Date
2025-12-30
Estimated Expiration
2035-03-05

AI Technical Summary

Technical Problem

Existing measurement, launch, and control systems have limited control capabilities, making it difficult to efficiently control multiple targets in a short period of time. Furthermore, the equipment is large in size and inconvenient to transport and deploy.

Method used

Design a portable continuous-fire test and control system. The system adopts a multi-layer storage space box structure and arranges the internal components in a reasonable manner, including the host, ephemeris receiver and integrated test adapter. It realizes efficient control of multiple targets through a communication bus and is equipped with a shock absorption mechanism and heat dissipation system to ensure stability.

Benefits of technology

It enables efficient control of multiple targets, reduces system space occupancy, improves portability and control efficiency, and saves manpower and resources.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model provides a portable running test launch control system, which comprises a box body, the interior of the box body is divided into an upper storage space, a middle storage space and a lower storage space by a plurality of horizontal partition plates, a host is arranged in the lower storage space, an ephemeris receiver and a power supply are arranged in the middle storage space, and a comprehensive test adapter is arranged in the upper storage space; the power supply is connected with the comprehensive test adapter, the ephemeris receiver is used for receiving satellite signals and outputting ephemeris data to the host, the host is in data communication with the comprehensive test adapter through a communication bus, the host is in data interaction with the controller on the target through the comprehensive test adapter, and the controller receives a control instruction sent by the host. The state information of the target is returned; the top of the box body is provided with a state display and operation panel, and the state display and operation panel is connected with the comprehensive test adapter. According to the utility model, a plurality of targets can be efficiently operated and controlled, the portability is good, and rapid deployment and use in various test sites are facilitated.
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Description

TECHNICAL FIELD

[0001] The utility model relates to target test and launch control technical field, concretely relates to a portable continuous launch test control system. BACKGROUND

[0002] In the field of target test and launch control, the test control system plays a vital role, which is used for comprehensive test and launch control of the target in the test site.

[0003] At present, the common test control system in the market has many defects and deficiencies. On the one hand, its control ability is limited, only one target can be controlled, and it is difficult to control multiple targets continuously in a short time, which is extremely low in efficiency in the scene of batch test or multi-target cooperative operation, and seriously affects the test progress and test effect. On the other hand, the existing equipment is large in size, which is extremely inconvenient in transportation and deployment, and it is difficult to meet the actual needs for flexible target test and launch tasks in different sites.

[0004] With the increasing complexity and diversification of target test and launch tasks, higher requirements are put forward for the portability and control efficiency of the test control system, and a new test control system is needed to overcome the defects of the prior art. UTILITY MODEL CONTENT

[0005] The technical problem to be solved by the utility model is to provide a portable continuous launch test control system to realize efficient control of multiple targets, and at the same time, to have good portability, so as to facilitate rapid deployment and use in various test sites.

[0006] To solve the above technical problems, the technical scheme of the utility model is:

[0007] The utility model relates to a portable continuous launch test control system for testing the overall performance of multiple targets, which is provided with an electrical device including a controller, a rudder system and a recorder, and the controller is connected with the rudder system and the recorder respectively, the system includes a box, the inside of the box is divided into three layers of storage space by multiple horizontal partitions, a host computer is arranged in the lower layer of storage space, an ephemeris receiver and a power supply are arranged in the middle layer of storage space, and a comprehensive test adapter is arranged in the upper layer of storage space, the power supply is connected with the comprehensive test adapter, the ephemeris receiver is used for receiving satellite signals and outputting ephemeris data to the host computer, the host computer communicates data with the comprehensive test adapter through a communication bus, the host computer communicates data with the controller on the target through the comprehensive test adapter, the controller receives the control instruction sent by the host computer and returns the state information of the target, and a state display and operation panel is arranged on the top of the box and connected with the comprehensive test adapter to input control operation and display the state information of the target in real time.

[0008] Further, the box is provided with a flip cover.

[0009] Further, one damping mechanism is arranged in each of the three layers of storage space, and the comprehensive test adapter, the ephemeris receiver and the host computer are arranged on the corresponding damping mechanism.

[0010] Further, the damping mechanism is a rubber damping pad.

[0011] Further, the box is provided with a heat dissipation hole, and the host computer and the ephemeris receiver are both provided with a cooling fan and a cooling fin.

[0012] Further, the host computer includes a PXI controller, a backboard, a serial communication module and an analog input and output module, the backboard is provided with a PXI bus, the PXI controller is connected with the serial communication module and the analog input and output module through the PXI bus, the serial communication module is used for communicating data with the controller on the target, and data is sent to the controller or data returned by the controller is received, the serial communication module is also used for communicating with the ephemeris receiver to obtain ephemeris data, and the analog input and output module is used for monitoring whether the power supply voltage of the electrical device on the target is normal.

[0013] Further, the host computer further includes a switching value input and output module, the PXI controller is connected with the switching value input and output module through the PXI bus, and the switching value input and output module is used for controlling a state indicating lamp arranged on the front side of the state display and operation panel to indicate whether the target is launched.

[0014] The utility model has the advantages that:

[0015] The utility model discloses a box body with upper and lower multilayer storage space, and the system internal device is arranged reasonably, wherein the host computer is arranged in the lower storage space, the ephemeris receiver and power supply are arranged in the middle storage space, and the comprehensive test adapter is arranged in the upper storage space, so as to reduce the space occupancy of the whole system, realize that the system is only the size of a suitcase, convenient transportation and carrying, and manpower and material resources can be saved. BRIEF DESCRIPTION OF DRAWINGS

[0016] Figure 1 It is the appearance schematic diagram of the utility model;

[0017] Figure 2 It is the measuring and control principle diagram of the utility model. DETAILED DESCRIPTION

[0018] In order to facilitate understanding the utility model, the utility model is explained further in detail below in combination with the drawings and specific embodiments. The person skilled in the art should understand that the embodiment is only to help understanding the utility model, and should not be regarded as the specific limitation of the utility model.

[0019] As Figure 1 , 2The utility model provides a portable continuous launch test control system for testing the overall performance of multiple targets, each target is provided with an electrical equipment, the electrical equipment includes a controller, a rudder system and a recorder, and the controller is connected with the rudder system and the recorder respectively, the portable continuous launch test control system includes a box body, the inside of box body is divided into three layers of storage space through multiple horizontal partitions, a host computer is arranged in the lower layer storage space, an ephemeris receiver and a power supply are arranged in the middle layer storage space, and a comprehensive test adapter is arranged in the upper layer storage space, the power supply is connected with the comprehensive test adapter, the ephemeris receiver is used for receiving satellite signals and outputting ephemeris data to the host computer, the host computer communicates data with the comprehensive test adapter through a communication bus, the host computer communicates data with the controller on the target through the comprehensive test adapter, the controller receives the control instruction (the specific instruction name and the function are shown in table 1) sent by the host computer, realizes the controller self-checking, the controller satellite receiving condition, the rudder system self-checking and the recorder self-checking project test, binds the data of the target and issues the control of the permission launch instruction, and returns the state information (including the controller self-checking result, the controller satellite receiving condition, the rudder system self-checking result, the recorder self-checking result, the data binding instruction response and the permission launch instruction response signal) of the target, a state display and an operation panel are arranged on the top of the box body, the state display and the operation panel are connected with the comprehensive test adapter, are used for inputting control operation and real -time display to the target state information.

[0020] Table 1 control instruction sent by portable continuous launch test control system to target

[0021] Serial number Control instruction name Control instruction function Sending sequence 1 Controller self-check instruction Check if the function of the controller is normal 1 2 Controller satellite reception condition instruction Check if the satellite reception condition of the controller is normal 2 3 Rudder system self-check instruction Check if the function of the rudder system is normal 3 4 Recorder self-check instruction Check if the function of the recorder is normal 4 5 Data binding instruction Write the binding data into the target 5 6 Allow launch instruction Make the electrical equipment on the target in the launch state 6

[0022] The portable continuous launch test control system uses the box body with upper and lower multi-layer storage space, reasonably arranges the internal devices of the system, reduces the space occupancy of the whole system, realizes that the system is only the size of a suitcase, and is convenient to carry.

[0023] The portable continuous launch test control system is used for controlling the test and launch process of the target, and the controller on the target communicates data with the portable continuous launch test control system. The electrical equipment on the target is tested and controlled through the portable continuous launch test control system, the controller is used for navigation control and receiving satellite signals of the target, the rudder system is used for receiving the instruction of the controller and adjusting the attitude of the target, and the recorder is used for receiving the positioning information and flight data of the target sent by the controller. The ephemeris receiver is used for acquiring satellite signals and converting into ephemeris data to be transmitted to the host computer, and provides basic data support for the whole system, and the controller on the target executes specific navigation control tasks based on the data and satellite signals received by itself.

[0024] The host obtains target state information returned by the electrical equipment on the target through the comprehensive test adapter, and transmits the target state information to the state display and operation panel through the communication link, so that the target state information is presented on the state display and operation panel for the operator to understand the target state in real time. The operator performs instruction operation on the state display and operation panel and transmits the instruction to the host through the communication link, and the host sends the related instruction to the controller on the target through the comprehensive test adapter, so as to realize the test and control of the target.

[0025] A flip cover is arranged on the box body to protect the state display and operation panel.

[0026] One damping mechanism is arranged in each of the upper, middle and lower storage spaces, and the comprehensive test adapter, the ephemeris receiver and the host are arranged on the corresponding damping mechanisms. The damping mechanism can be a rubber damping pad. The key vulnerable components of the system are reinforced through the damping mechanism to ensure the mechanical stability during transportation and use.

[0027] The box body is provided with heat dissipation holes, and the host and the ephemeris receiver are both equipped with heat dissipation fans and heat dissipation fins. The heat dissipation fan is installed on one side of the host shell, and the heat dissipation fin is arranged on the heating chip inside the host. The heat dissipation fan is installed on the top of the shell of the ephemeris receiver, and the heat dissipation fin is pasted on the signal processing chip of the ephemeris receiver. The heat dissipation fan and the heat dissipation fin are provided for the host and the ephemeris receiver and other devices with large heat dissipation, so that their temperature is within the normal range during long time work, and the performance is stable.

[0028] The host comprises a PXI controller, a backplane, a serial communication module and an analog input and output module. The PXI bus is arranged on the backplane, the PXI controller is connected with the serial communication module and the analog input and output module through the PXI bus to communicate data, the serial communication module is used for communicating data with the controller on the target, and sends data to the controller or receives data returned by the controller; the serial communication module is also used for communicating with the ephemeris receiver to obtain ephemeris data; and the analog input and output module is used for monitoring whether the power voltage of the electrical equipment on the target is normal.

[0029] The host further comprises a switching value input and output module, the PXI controller is connected with the switching value input and output module through the PXI bus to communicate data, and the switching value input and output module is used for controlling the state indicator light arranged on the front side of the state display and operation panel to indicate whether the target is launched. The switching value input and output module controls the on-off of the state indicator light by outputting high and low levels.

[0030] Although the embodiments of the present application have been shown and described, it is to be understood that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present application, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A portable launch and control system for testing the overall performance of a plurality of targets, said targets having an electrical device disposed thereon, said electrical device including a controller, a rudder system and a recorder, said controller being connected to said rudder system and said recorder, respectively; characterized by, The system comprises a box, the inside of which is divided into three layers of storage space by horizontal partitions, a main machine is arranged in the lower layer of storage space, an ephemeris receiver and a power supply are arranged in the middle layer of storage space, and a comprehensive test adapter is arranged in the upper layer of storage space; the power supply is connected with the comprehensive test adapter, the ephemeris receiver is used for receiving satellite signals and outputting ephemeris data to the main machine, the main machine communicates data with the comprehensive test adapter through a communication bus, the main machine communicates data with a controller on the target through the comprehensive test adapter, the controller receives control instructions sent by the main machine and returns state information of the target. A state display and operation panel is arranged on the top of the box, which is connected with the comprehensive test adapter and used for inputting control operations and displaying state information of the target in real time.

2. The portable launch and monitor control system of claim 1, wherein, A flip cover is arranged on the box.

3. The portable launch and monitor control system of claim 1, wherein, A damping mechanism is arranged in each of the three layers of storage space, and the comprehensive test adapter, the ephemeris receiver and the main machine are arranged on the corresponding damping mechanism.

4. The portable launch and monitor control system of claim 3, wherein, The damping mechanism is a rubber damping pad.

5. The portable launch and monitor control system of claim 1, wherein, The box is provided with heat dissipation holes on the side, and the main machine and the ephemeris receiver are both equipped with cooling fans and cooling fins.

6. The portable launch and monitor control system of claim 1, wherein, The main machine comprises a PXI controller, a backboard, a serial communication module and an analog input and output module; the backboard is provided with a PXI bus, the PXI controller is connected with the serial communication module and the analog input and output module through the PXI bus, the serial communication module is used for communicating data with the controller on the target, sending data to the controller or receiving data returned by the controller; the serial communication module is also used for communicating with the ephemeris receiver to obtain ephemeris data; and the analog input and output module is used for monitoring whether the power supply voltage of the electrical equipment on the target is normal.

7. The portable launch and monitor control system of claim 6, wherein, The main machine further comprises a switching value input and output module, the PXI controller is connected with the switching value input and output module through the PXI bus, and the switching value input and output module is used for controlling a state indicating lamp arranged on the front side of the state display and operation panel to indicate whether the target is launched.