阅读说明：本技术 一种基于过载激活起控导弹的半实物仿真上电装置及方法 (Semi-physical simulation electrifying device and method based on overload activation start-control missile ) 是由 张宁轩 刘龙 晏资湘 于 2020-12-14 设计创作，主要内容包括：本发明公开了一种基于过载激活起控导弹的半实物仿真上电装置及方法,包括一台可进行远程控制的直流电源,半实物仿真机可向所述直流电源发送编程数据远端控制其上电或下电。本发明设计的基于过载激活起控导弹的半实物仿真上电装置和方法,应用于某型号弹载武器系统仿真试验中,控制可编程电源在仿真中某一时间点上电,有效解决了传统仿真方法无法精确判断起控时间的问题,提高了半实物仿真的准确性,更加精准的模拟导弹实际飞行的过程；本发明可拓展用于各种需要模拟电源控制的场景,通过软件远程自动控制电源的输出电流或电压以及输出变化规律,模拟各种复杂的电源环境,可以在各种需要模拟电源场景的产品检验中使用。(The invention discloses a semi-physical simulation power-on device and a semi-physical simulation power-on method based on overload activation of a start-control missile. The semi-physical simulation electrifying device and method based on overload activation start-control missile is applied to a simulation test of a missile-borne weapon system of a certain model, and controls the programmable power supply to be electrified at a certain time point in simulation, so that the problem that the start-control time cannot be accurately judged by the traditional simulation method is effectively solved, the accuracy of semi-physical simulation is improved, and the actual flight process of the missile is simulated more accurately; the invention can be used for various scenes needing power supply simulation control, remotely and automatically controls the output current or voltage and the output change rule of the power supply through software, simulates various complex power supply environments, and can be used in product inspection of various scenes needing power supply simulation.)

1. A semi-physical simulation power-on device and a semi-physical simulation power-on method based on overload activation of a start-control missile are characterized by comprising a direct-current power supply capable of being remotely controlled, and a semi-physical simulation machine can send programming data to the direct-current power supply to remotely control the direct-current power supply to be powered on or powered off.

2. The semi-physical simulation power-on device based on the overload-activated start-control missile according to claim 1, further comprising a level shift cable, wherein the direct-current power supply is provided with a standard protocol interface matched with the level shift cable, one end of the level shift cable is connected with the direct-current power supply through the standard protocol interface, and the other end of the level shift cable is connected with the semi-physical simulation machine.

3. The semi-physical simulation power-on device of the overload-activated start-control missile according to claim 2, wherein the standard protocol interface is an RS232 interface, the dc power supply is specifically provided with a DB9 plug matching the RS232 interface, the level shift cable is an IT-E131 cable, and the level shift cable is connected to the dc power supply through the DB9 plug.

4. The power-on method of the semi-physical simulation power-on device according to any one of claims 1 to 3, characterized by comprising the following steps:

s1, connecting a DB9 plug on a power supply with one end of a level conversion cable, wherein the other end of the level conversion cable is connected with a DB9 interface of the semi-physical simulator, and equipment interfaces all follow an RS232 communication standard;

s2, configuring an RS232 serial port to enable the communication settings of the Baud rate, the data bit, the check bit, the stop bit and the like to be matched with the power supply remote control parameters;

and S3, controlling the power supply through instructions by using a programming grammar guide of the power supply, wherein the communication protocol of the programmable power supply is SCPI or PLC.

5. The method for power-on in semi-physical simulation according to claim 4, wherein the specific method matched in step S2 is: the communication baud rate is 115200, the data bit is 8bit, no check exists, and the stop bit is 1 bit.

6. The semi-physical simulation power-on method according to claim 5, wherein in step S3, a free port communication mode of a PLC is adopted, a non-protocol mode is adopted to control a power supply, and the specific sending instruction is as follows: and sending a remote mode instruction, a power supply voltage instruction, a power-on instruction and a power-off instruction to the programmable power supply.

Technical Field

The invention belongs to the field of semi-physical simulation, and particularly relates to a semi-physical simulation power-on device and method based on overload activation of a start-control missile.

Background

At present, the measurement of angular velocity information after the launching of a highly overloaded launching weapon (such as an artillery and a tank gun) is a well-recognized problem. The main reasons for this are that the angular velocity sensor is hard to be impacted by the high overload environment, and the damage to the sensor by the high overload process mainly has two ways: the direct impact of inertia force and the damage of stress wave generated by high overload to the structure. During the launching process, the cannonball is subjected to huge overload action to accelerate to the expected initial launching speed, the amplitude peak value of the overload process can reach over 20000g (g is gravity acceleration, the same applies below), and the action time is within tens of milliseconds. For example, a 155mm howitzer produces a maximum overload pulse amplitude of 20000g during firing for a duration of 5 ms. The method for adding the inertial guidance module in the cannonball can provide a reference for ballistic correction, and effectively improves the hitting precision of ammunition. Therefore, many developed countries have developed guidance upgrades for conventional ammunition, developing related inertial guidance modules. Among them, the united states advanced research program office (DARPA) lists the anti-high overload gyroscope as one of the key devices in the μ PNT program.

Researches find that the anti-high overload capacity of the sensing device under the condition of no power-on is obviously superior to that under the condition of power-on, and related experiments show that the anti-overload capacity of the sensing device under the condition of power-on is about 5000g, and the anti-overload capacity of the sensing device under the condition of no power-on is about 10000 g. Therefore, in order to solve the influence of high overload on a sensing device, a feasible scheme is to design an overload switch on the missile, when the missile is sensitive to high overload, namely the missile is taken out of a hearth, a thermal battery is electrified, a control system is started, and if the control system is designed to be the scheme, the traditional semi-physical simulation method has infeasible risk. In the traditional semi-physical simulation, a control system is powered on for waiting, and the trajectory is judged to be zero second after an off-line signal is received or the acceleration of a virtual inertial measurement unit sent by a simulator is received, so that control is started; and the missile is provided with an overload switch, and the scheme of starting control of the command control system on the thermal battery by utilizing overload activation cannot be used for powering up in advance, and the precision of starting control time cannot be ensured if a simulator is used for manually powering up. If the power-on starting and controlling time of the overload activation missile needs to be simulated more accurately, a semi-physical simulation power-on device and method for remotely controlling the power supply to be powered on need to be developed.

Disclosure of Invention

Aiming at the defects and improvement requirements of the prior art, the invention aims to solve the problem that the control starting time cannot be accurately judged for the semi-physical simulation scheme of the overload-activated missile by the traditional simulation method.

In order to achieve the purpose, the technical scheme of the invention is as follows:

a semi-physical simulation power-on device based on overload activation of a start-control missile comprises a direct-current power supply capable of being remotely controlled, and a semi-physical simulation machine can send programming data to the direct-current power supply to remotely control the direct-current power supply to be powered on or powered off.

And the system further comprises a level conversion cable, the direct current power supply is provided with a standard protocol interface matched with the level conversion cable, one end of the level conversion cable is connected with the direct current power supply through the standard protocol interface, and the other end of the level conversion cable is connected with the semi-physical simulation machine.

Specifically, the standard protocol interface is an RS232 interface, the dc power supply is specifically provided with a DB9 plug matching the RS232 interface, the level shift cable is an IT-E131 cable, and the level shift cable is connected to the dc power supply through the DB9 plug.

The invention also provides a power-on method of the power-on device based on the semi-physical simulation, which comprises the following steps:

s1, connecting a DB9 plug on a power supply with one end of a level conversion cable, wherein the other end of the level conversion cable is connected with a DB9 interface of the semi-physical simulator, and equipment interfaces all follow an RS232 communication standard;

s2, configuring an RS232 serial port to enable the communication settings of the Baud rate, the data bit, the check bit, the stop bit and the like to be matched with the power supply remote control parameters;

and S3, controlling the power supply through instructions by using a programming grammar guide of the power supply, wherein the communication protocol of the programmable power supply is SCPI or PLC.

Specifically, the specific method for matching in step S2 is: the communication baud rate is 115200, the data bit is 8bit, no check exists, and the stop bit is 1 bit.

Preferably, in step S3, the power supply is controlled by using a free port communication method of a PLC and a non-protocol mode, and the specific sending instruction is as follows: and sending a remote mode instruction, a power supply voltage instruction, a power-on instruction and a power-off instruction to the programmable power supply.

Compared with the prior art, the technical scheme of the invention can obtain the following beneficial effects:

1. the semi-physical simulation electrifying device and method based on overload activation start-control missile is applied to a simulation test of a missile-borne weapon system of a certain model, and controls the programmable power supply to be electrified at a certain time point in simulation, so that the problem that the start-control time cannot be accurately judged by the traditional simulation method is effectively solved, the accuracy of semi-physical simulation is improved, and the actual flight process of the missile is simulated more accurately;

2. the invention can be used for various scenes needing power supply simulation control, remotely and automatically controls the output current or voltage and the output change rule of the power supply through software, simulates various complex power supply environments, and can be used in product inspection of various scenes needing power supply simulation.

Drawings

FIG. 1 is a schematic diagram of a simulation test provided by an embodiment of the present invention;

FIG. 2 is a schematic diagram of a hardware connection for simulation test according to an embodiment of the present invention;

fig. 3 is a flowchart of a simulation test according to an embodiment of the present invention.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be obtained by a person skilled in the art without any inventive step based on the embodiments of the present invention, are within the scope of the present invention.

Example 1

The invention designs a semi-physical simulation scheme aiming at overload activation of the missile by combining with the actual requirements of the weapon system semi-physical simulation, controls the programmable power supply to be electrified at a certain time point in the simulation, effectively solves the problem that the traditional simulation method cannot accurately judge the start-control time, improves the accuracy of the semi-physical simulation, and more accurately simulates the actual flight process of the missile. The specific implementation mode is as follows:

a semi-physical simulation power-on device based on overload activation of a start-control missile comprises a direct-current power supply capable of being remotely controlled, and a semi-physical simulation machine can send programming data to the direct-current power supply to remotely control the direct-current power supply to be powered on or powered off.

The device is characterized by further comprising a level conversion cable, wherein the direct current power supply is provided with a standard protocol interface matched with the level conversion cable, one end of the level conversion cable is connected with the direct current power supply through the standard protocol interface, and the other end of the level conversion cable is connected with the semi-physical simulation machine.

The standard protocol interface is an RS232 interface, the direct-current power supply is specifically provided with a DB9 plug matched with the RS232 interface, the level conversion cable is an IT-E131 cable, and the level conversion cable is connected with the direct-current power supply through the DB9 plug.

Example 2

A power-on method of a semi-physical simulation power-on device based on overload activation of a start-control missile comprises the following steps:

s1, connecting a DB9 plug on the rear panel of one power supply in an ITECH IT6800 series of programmable direct-current power supplies with one end of a level conversion cable (the specific connection interface is an RS232 interface), connecting the other end of the level conversion cable with the DB9 interface of the semi-physical simulator, and enabling equipment interfaces to conform to the RS232 communication standard; the semi-physical simulator is communicated with an upper computer through a CAN bus and an RS422 to exchange data and transmit instructions;

s2, configuring an RS232 serial port to enable the communication settings of the Baud rate, the data bit, the check bit, the stop bit and the like to be matched with the power supply remote control parameters;

the concrete matching method comprises the following steps: the communication baud rate is 115200, the data bit is 8 bits, no check exists, and the stop bit is 1 bit;

s3, controlling the power supply through instructions by using a programming grammar guide of the power supply, wherein the communication protocol of the programmable power supply is SCPI or PLC;

in this embodiment, a free port communication mode of the PLC is adopted, a non-protocol mode is adopted to control the power supply, and the specific sending instruction is as follows: and sending a remote mode instruction, a power supply voltage instruction, a power-on instruction and a power-off instruction to the programmable power supply.

The method is applied to a simulation test of a certain type of missile-borne weapon system, a programmable power supply is controlled to be powered on at a certain time point in simulation, the problem that the control starting time cannot be accurately judged by a traditional simulation method is effectively solved, the accuracy of semi-physical simulation is improved, and the actual flight process of a missile is simulated more accurately, in the embodiment, the semi-physical simulator specifically controls the power supply, and the sending instruction is as shown in the following table 1:

TABLE 1 control of a semi-physical simulator on power supply and instruction transmission

As shown in the table above, the initiator sends a command to the power source in the form of a HEX, ending with a 0D 0A linefeed.

Step S3 specifically includes the following steps:

s31, powering on the simulator, sending a remote mode instruction to the programmable power supply, namely sending a frame of ASCII code 'SYST: REM' instruction to the power supply through the RS262 port, and actually sending '535953543A 52454D 0D 0A' in a HEX form; the remote mode is that the remote control of the simulator is realized through the communication interface, and if the remote mode is not set, the power supply can be controlled only through a button;

s32, configuring the power supply to be in a far-end mode; at this time, the power supply voltage is set, namely, a frame of ASCII code command of APP VOLT 28, 28 and 5 is sent to the power supply through an RS262 port, and the three paths of voltages are configured to be 28V, 28V and 5V respectively by actually sending 4150503A 564F 4C 542032382C 32382C 350D 0A in a HEX form; one or two voltages may be configured as needed, and this is only a specific example of this embodiment.

S33, the simulator starts simulation, when a certain overload condition is met (2000g), the simulation is judged to be the power-on time of the control system, a frame of command with ASCII code of 'APP: OUT1,0, 0', actually '4150503A 4F 555420312C 302C 300D 0A', is sent to the power supply, and the 1 st circuit of the power supply is powered on; the control system power-on time represents the time when the sensor senses overload and triggers;

s34, when the simulator judges that the preset stop condition is satisfied and the simulation is stopped, the simulator sends a command that one frame of ASCII code is APP OUT 0,0,0, actually '4150503A 4F 555420302C 302C 300D 0A' to the power supply to power down the 1 st circuit of the power supply, and the simulation is finished. The stop condition set in advance is specifically a condition for landing the shell or judging a hit target.