CN112749480B - Method for testing combination of bomb simulator and carrier - Google Patents
Method for testing combination of bomb simulator and carrier Download PDFInfo
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- CN112749480B CN112749480B CN202011521899.3A CN202011521899A CN112749480B CN 112749480 B CN112749480 B CN 112749480B CN 202011521899 A CN202011521899 A CN 202011521899A CN 112749480 B CN112749480 B CN 112749480B
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- 238000012360 testing method Methods 0.000 title claims abstract description 76
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- 238000004891 communication Methods 0.000 claims abstract description 11
- 238000002360 preparation method Methods 0.000 claims description 5
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Abstract
A method for testing the combination of a bomb simulator and a carrier machine includes that the bomb simulator communicates with the carrier machine 1553, and according to the communication protocol and the bomb throwing flow of an accurate guided bomb and the carrier machine, the accurate guided bomb is simulated to complete on-line simulation, flying and bomb throwing flow test; the panel controller displays the working state in the interaction process of the bomb simulator and the carrier, and switches the working flow; receiving and analyzing GPS data; and data interaction is carried out between the monitoring port and the test computer, and the telemetry data is sent to the test computer. The test computer receives, analyzes and stores the telemetry data; monitoring the working state of the bomb simulator in real time; when the bomb simulator is in the "extended flow" state, the test computer can set the bomb simulator working state.
Description
Technical Field
The invention relates to a method for testing a combination of a bomb simulator and a carrier, which is used for simulating the combination of an accurate guided bomb and the carrier, testing the online simulation, flying and throwing processes of the accurate guided bomb and the carrier, and preliminarily verifying whether the accurate guided bomb and the carrier can interact normally.
Background
The accurate guided bomb has the advantages of low cost, high striking precision, remarkable damage effect and the like, and is widely applied to modern war. The recent local warfare suggests that the number and proportion of precisely guided weapon uses are increasing.
Precisely guided bombs often require different carriers, which requires corresponding modification of the carriers and the precisely guided bombs, and new types of precisely guided bombs are also being introduced. To ensure proper interaction and cooperative operation of the precisely guided bombs and the carrier, a series of operations such as testing, flying, and throwing the precisely guided bombs and the carrier are organized.
Disclosure of Invention
The invention aims to solve the technical problems that: the method overcomes the defects of the prior art and provides a method for testing the combination of a bomb simulator and a carrier, wherein the bomb simulator communicates with the carrier 1553, and the accurate guided bomb is simulated to complete on-line simulation, flying and bomb throwing flow test according to the communication protocol and the bomb throwing flow of the accurate guided bomb and the carrier; the panel controller displays the working state in the interaction process of the bomb simulator and the carrier, and switches the working flow; receiving and analyzing GPS data; and data interaction is carried out between the monitoring port and the test computer, and the telemetry data is sent to the matched test computer. The test computer receives, analyzes and stores the telemetry data; monitoring the working state of the bomb simulator in real time; when the bomb simulator is in the 'extended flow', the working state of the bomb simulator can be set.
The invention aims at realizing the following technical scheme:
a method for testing a bomb simulator and a carrier in a combined way divides the combined test into a basic flow and an extended flow;
the basic flow comprises the following steps:
S11, installing a bomb simulator on a hanging point of a carrier, wherein the bomb simulator is set as a basic flow; the monitoring port of the bomb simulator is connected with the testing computer;
S12, the carrier supplies power to the bomb simulator through the plug-in cable, and sequentially downloads the description of the carrier, the alignment instruction, the parent inertial navigation data, the power supply of the carrier, the battery activation and the throwing instruction according to the throwing process, and the bomb simulator sequentially reports the description of the hanging object, the self-checking result, the alignment result and the throwing preparation result to the carrier; the panel controller of the bomb simulator controls the corresponding status indicator lamp and the buzzer to work according to the working status of the bomb simulator; the test computer is used for monitoring the state of the bomb simulator;
the expansion flow comprises the following steps:
S21, installing a bomb simulator on a hanging point of a carrier, wherein the bomb simulator is set to be an expansion flow; the monitoring port of the bomb simulator is connected with the testing computer;
S22, testing according to the process of S12; the method comprises the steps that a test computer is utilized to set fault types and fault codes, and a bomb simulator reports the corresponding fault types and fault codes at the appointed fault occurrence time; when the bomb simulator reports a fault, the panel controller indicates the fault type.
In the method for using the bomb simulator and the carrier for the combined test, preferably, the panel controller is provided with a plurality of indicator lamps which are respectively used for indicating the carrier power supply, the panel communication, the bomb handshake, the self-checking state, the alignment state, the target data, the throwing instruction, the throwing preparation state and the GPS positioning state; meanwhile, a throwing instruction buzzer is arranged on the panel controller.
In the method for testing the bomb simulator and the carrier in a combined way, preferably, the test computer can store various telemetry data in a time axis sequence.
In the method for using the bomb simulator and the carrier in the combined test, preferably, in the expansion process, the carrier sends the instruction to the bomb simulator according to the throwing line and the bomb throwing process, the bomb simulator reports the working state in sequence according to the test computer, and the panel controller displays the current state of the bomb simulator. The test computer receives, parses and stores telemetry data to monitor the operational status of the bomb simulator.
In the method for testing the bomb simulator and the carrier in a combined way, preferably, the bomb simulator comprises a flight controller, a GPS receiver, a panel controller, a disengaging and inserting device and a lifting lug; the flight controller and the GPS receiver are the same as corresponding products on the accurate guided bomb, the panel controller is used for status display, sound warning and flow selection, the carrier supplies power to the bomb simulator through the plug-in cable of the bomb simulator, and the lifting lug is used for mechanical connection.
Compared with the prior art, the invention has the following beneficial effects:
(1) Compared with the traditional bomb simulator, the bomb simulator related by the method has the advantages that besides the time sequence of interaction with the carrier is consistent with that of the accurate guided bomb, the same flight controller and GPS receiver are adopted for the accurate guided bomb, so that the communication between the accurate guided bomb and the carrier can be simulated more truly, and software and hardware related to the interaction of the bomb and the machine can be verified in joint test;
(2) The flight controller supports a multi-section programming function, and can simultaneously program a plurality of types of guided bomb programs. The same bomb simulator can simulate the joint test of guided bombs of various types and carriers without repeated programming;
(3) The test flow of the combined machine is divided into a basic flow and an expansion flow. If the basic flow is the basic flow, the bomb simulator reports the normal bomb state in sequence at the set time according to the bomb throwing time sequence; if the flow is an extended flow, the test computer sets a fault type and a fault code through a monitoring port, and the bomb simulator reports the corresponding fault type and fault code at the appointed fault occurrence time;
(4) When the bomb simulator software operates, telemetry data can be periodically sent through a ground test port, and the test computer monitoring software receives and analyzes the telemetry data, so that various related bomb data can be displayed in real time through an interface, and the test data can be classified and stored into a 'dat file', such as 'GPS data, dat', 'voltage information, dat', 'key information_hex, dat', 'key information_text information, flash parameter, dat', and the like, so as to facilitate subsequent analysis.
(5) The bomb simulator related to the method can be used for testing the bomb simulator and the carrier at any time according to the needs, and problems possibly existing in the development and debugging stages of the carrier force control system software and the on-bullet system software can be found in time, so that unnecessary problems are reduced in the processes of testing, hanging and throwing the bomb by the accurate guidance bomb and the carrier, the working efficiency is improved, and the development cost is reduced.
Drawings
FIG. 1 is a schematic diagram of a bomb simulator workflow.
FIG. 2 is a schematic diagram of a bomb simulator.
FIG. 3 is a structural design of a bomb simulator.
Fig. 4 is a schematic diagram of a bomb simulator electrical system.
FIG. 5 is a schematic diagram of a basic flow connection of a bomb simulator.
FIG. 6 is a schematic diagram of a bomb simulator extension flow connection.
FIG. 7 is a schematic diagram of a panel controller.
FIG. 8 is a monitoring software interface of the test computer.
Fig. 9 is voltage information telemetry data.
Reference numerals: 1. the plug-in and plug-out connecting cable 2, the plug-out 3, the shell 4, the lifting lug 5, the integrated flight controller 6, the panel controller 7, the display operation panel 8, the GPS receiver 9 and the handle (also used as a bracket)
Detailed Description
For the purpose of making the objects, technical solutions and advantages of the present invention more apparent, embodiments of the present invention will be described in further detail below with reference to the accompanying drawings.
A method for testing by using a bomb simulator and a carrier in a combined way, wherein the bomb simulator is in 1553 communication with the carrier, and the accurate guided bomb is simulated to complete on-line simulation, flying and projectile throwing flow test according to the communication protocol and the projectile throwing flow of the accurate guided bomb and the carrier; the panel controller displays the working state in the interaction process of the bomb simulator and the carrier, and switches the working flow; receiving and analyzing GPS data; and data interaction is carried out between the monitoring port and the test computer, and the telemetry data is sent to the matched test computer. The test computer receives, analyzes and stores the telemetry data; monitoring the working state of the bomb simulator in real time; when the bomb simulator is in the "extended flow" state, the bomb simulator operating state may be set. A schematic of the bomb simulator workflow is shown in fig. 1.
Bomb simulators are more specific:
1. Structural design
The bomb simulator related by the method mainly comprises a flight controller, a GPS receiver, a panel controller, a disengaging and inserting device, a lifting lug and the like, and the whole overall dimension and the mass are as follows:
external dimensions:
Main body size:
mass:
Total mass: 7.5kg
And (3) paint spraying:
color: silver grey B04, GB/T3181-2008
The bomb simulator related to the method adopts a flight controller and a GPS receiver which are the same as those of an accurate guided bomb; the adopted lifting lug meets the double lifting lug form of GJB 1C; the panel controller comprises a plurality of indicator lamps for representing the state of the bomb, a buzzer, a flow selection switch and the like. The structural schematic diagram and the structural design diagram of the bomb simulator related to the method are shown in fig. 2 and 3.
2. Electrical system design
The electrical system schematic diagram of the bomb simulator involved in the method is shown in fig. 4. The carrier provides two paths of 28V power sources of V1 (28V for a long time) and V2 (28V/1 s) for the simulator through a hanging rack plug-and-plug connection cable-bomb simulator interface, and the power consumption of the simulator is not more than 30W.
The cable interface of the connection between the hanging rack and the plug is 'socket YF6A-46TJ, plug YF6A-46 ZK', and the point numbers are defined in table 1.
TABLE 1
The monitoring port adopts a connector DB-15S, the internal signals comprise a monitoring and programming RS422 serial port and a 28V ground power supply input port, and the definition of the point numbers is shown in Table 2.
TABLE 2
3. Test flow
The bomb simulator related by the method is in 1553 communication with the carrier, and is combined with the carrier to be tested and divided into a basic flow and an expansion flow. Simulating the accurate guided bomb to finish online simulation, flying and bomb throwing process test according to the communication protocol and the bomb throwing process of the accurate guided bomb and the loader; the panel controller displays the working state in the interaction process of the bomb simulator and the carrier, and switches the working flow; receiving and analyzing GPS data; and data interaction is carried out between the monitoring port and the test computer, and the telemetry data is sent to the test computer.
The test computer receives, analyzes and stores the telemetry data; monitoring the working state of the bomb simulator in real time; when the bomb simulator is in the "extended flow" state, the bomb simulator operating state may be set.
3.1 If the basic flow is the basic flow, the connection method of the bomb simulator and the carrier machine is shown in fig. 5, and the specific steps are as follows:
Step one: connecting the bomb simulator with the hanging point of the carrier machine according to the diagram of fig. 5, and programming in the soft part of the bomb simulator; if the software is programmed, selecting the software to be operated through a programming tool;
step two: dialing the process selection switch to the basic process;
Step three: the carrier supplies power to the bomb simulator through the plug-in and plug-out, the bomb simulator sequentially transmits the description of the carrier, the alignment instruction, the parent inertial navigation data, the V2 electricity, the battery activation and throwing instruction and the like according to the throwing process, and the bomb simulator sequentially reports the description of the suspended matters, the self-checking result, the alignment result and the throwing preparation result to the carrier. The panel controller controls the state indicator lamp and the buzzer to work according to the working state of the bomb simulator. The test computer receives, analyzes and stores the telemetry data, and displays the telemetry data, such as carrier instructions, bomb simulator reply instructions, bomb simulator status words, GPS data, voltage information, and the like, on the interface in real time.
3.2 If the extended flow is used, the connection diagram of the bomb simulator and the carrier is shown in fig. 6, and the specific steps are as follows:
Step one: connecting the bomb simulator with the carrier hanging point as shown in fig. 6, and preparing bomb simulator software and a test computer;
step two: dialing the flow selection switch to an expansion flow;
Step three: using a test computer to set a bomb fault state, such as self-checking abnormality of a single machine, alignment abnormality and the like (the fault state can be not set);
step four: the carrier sends instructions to the bomb simulator according to the throwing line and the bomb throwing flow, the bomb simulator reports working states in sequence according to the setting of the test computer, and the panel controller displays the current state of the bomb simulator. The test computer receives, parses and stores telemetry data to monitor the operational status of the bomb simulator.
3.3 The panel controller is shown in fig. 7, and the operation is described as follows:
a) The carrier supplies power V1 indicator light. When the carrier supplies power to the bomb simulator, the panel controller indicator lights are sequentially lighted in three colors of red, green and blue. If the V1 power supplied by the carrier meets the requirement, the indicator light is lighted green, otherwise, the indicator light is lighted red.
B) "Panel communication" indicator light. If the handshake between the panel controller and the flight controller in the bomb simulator is successful, the indicator light is lightened to green, otherwise, the indicator light is lightened to red.
C) "bullet machine hand" pilot lamp. After the bomb simulator is electrified for a certain time, judging whether the handshake with the carrier is successful, if so, lighting green, otherwise, lighting red.
D) A self-checking status indicator light. If the bomb simulator self-tests are normal, the color is lightened green, otherwise, the color is lightened red.
E) An "alignment status" indicator light. If the bomb simulator is aligned normally, the color is lightened green, otherwise, the color is lightened red.
F) "target data" indicates a lamp. And if the target data is normally loaded, the target data is lightened green, otherwise, the target data is lightened red.
G) The carrier supplies power V2 indicator light. Judging whether the V2 electricity issued by the carrier meets the requirement, if so, lighting green, otherwise, lighting red.
H) An instruction-throwing indicator lamp and a buzzer. If a throwing instruction is received, the indicator lamp is lightened and blinks, and meanwhile the buzzer sounds, otherwise, the indicator lamp and the buzzer do not work.
I) "put ready" indicator light. The bomb simulator judges whether the bomb is ready for throwing and reports the bomb to the carrier machine, and if the bomb is ready for throwing, the indicator light is lighted green; if the bomb failed, the red color is lit.
J) "GPS location status" indicator light. The bomb simulator judges the GPS positioning state, if the positioning requirement is met, the bomb simulator lights green, otherwise, the bomb simulator lights red.
3.4 The test computer monitoring software interface is shown in fig. 8, and the interface is mainly divided into a bomb simulator working state setting module, a bomb interaction instruction display module and a telemetry data display module, and meanwhile, the software can store telemetry data in a classified manner and store the telemetry data into a 'dat file', such as 'GPS data, dat', 'voltage information, dat', 'key information_hex.dat', 'key information_text information, dat', 'Flash parameter, dat', and the like.
Various telemetry data storage forms are sequentially arranged according to the time of data generation by taking a time axis as an order, and take voltage information as an example, as shown in fig. 9: the first column of data is the system time corresponding to each telemetry period, the time interval is 10ms, and the telemetry data is sent once every 10 ms; the second column is the system voltage; the third column is the battery voltage; the fourth column is the enable put signal; the fifth column is the RT address; the sixth column is the GPS location state. Other types of data are also stored in this format, and the testing process can be more fully mastered by analyzing the telemetry data after the testing is completed.
The invention is suitable for the avionics test of various loaders and various accurate guided bombs, and is used for preliminary verification of normal interaction of the loaders and the accurate guided bombs. In the development and debugging stages of the mechanical and electrical control system software of the carrier and the mechanical and electrical system software of the bullet, technicians can use the invention to conduct avionics test at any time, discover possible problems of communication protocols, bullet throwing processes and bullet machine software interaction in advance, solve the problems of joint test, flying and bullet throwing which are unnecessary, improve the working efficiency, shorten the research and development period and reduce the cost.
The basic flow and the extended flow of the bomb simulator are matched for use, so that whether the interaction functions of the bomb and the machine are provided or not can be detected more comprehensively; the test computer receives, analyzes and stores the remote measurement data sent by the bomb simulator, so that the working state of the bomb simulator in the joint test process can be monitored in real time, and technicians can conveniently analyze the data after the joint test.
What is not described in detail in the present specification is a well known technology to those skilled in the art.
Although the present invention has been described in terms of the preferred embodiments, it is not intended to be limited to the embodiments, and any person skilled in the art can make any possible variations and modifications to the technical solution of the present invention by using the methods and technical matters disclosed above without departing from the spirit and scope of the present invention, so any simple modification, equivalent variation and modification to the embodiments described above according to the technical matters of the present invention fall within the scope of the technical matters of the present invention.
Claims (4)
1. A method for testing a bomb simulator and a carrier in a combined way is characterized in that the combined test is divided into a basic flow and an extended flow;
the basic flow comprises the following steps:
S11, installing a bomb simulator on a hanging point of a carrier, wherein the bomb simulator is set as a basic flow; the monitoring port of the bomb simulator is connected with the testing computer;
S12, the carrier supplies power to the bomb simulator through the plug-in cable, and sequentially downloads the description of the carrier, the alignment instruction, the parent inertial navigation data, the power supply of the carrier, the battery activation and the throwing instruction according to the throwing process, and the bomb simulator sequentially reports the description of the hanging object, the self-checking result, the alignment result and the throwing preparation result to the carrier; the panel controller of the bomb simulator controls the corresponding status indicator lamp and the buzzer to work according to the working status of the bomb simulator; the test computer is used for monitoring the state of the bomb simulator;
the expansion flow comprises the following steps:
S21, installing a bomb simulator on a hanging point of a carrier, wherein the bomb simulator is set to be an expansion flow; the monitoring port of the bomb simulator is connected with the testing computer;
s22, testing according to the process of S12; the method comprises the steps that a test computer is utilized to set fault types and fault codes, and the bomb simulator reports the corresponding fault types and fault codes at the appointed fault occurrence time; when the bomb simulator reports a fault, the panel controller indicates the fault type;
In the expansion flow, the carrier sends instructions to the bomb simulator according to the throwing line and the bomb throwing flow, the bomb simulator reports working states in sequence according to the setting of the test computer, and the panel controller displays the current state of the bomb simulator; the test computer receives, parses and stores telemetry data to monitor the operational status of the bomb simulator.
2. The method for combined testing of a bomb simulator and a carrier machine according to claim 1, wherein the panel controller is provided with a plurality of indicator lamps for indicating the power supply of the carrier machine, the communication of the panel, the handshake of the bomb machine, the self-checking state, the alignment state, the target data, the throwing instruction, the throwing preparation state and the GPS positioning state respectively; meanwhile, the panel controller is also provided with a throwing instruction buzzer.
3. The method of claim 1, wherein the test computer is capable of storing the telemetry data in time series.
4. The method of claim 1, wherein the bomb simulator comprises a flight controller, a GPS receiver, a panel controller, a de-plug, a lifting lug; the flight controller and the GPS receiver are the same as corresponding products on the accurate guided bomb, the panel controller is used for status display, sound warning and flow selection, the carrier supplies power to the bomb simulator through the plug-in cable of the bomb simulator, and the lifting lug is used for mechanical connection.
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