KR101016916B1 - Method of Data Injection of Embedded System of Aircraft for Test and Flight Simulation - Google Patents

Abstract

The present invention relates to an aircraft embedded system for flight simulation and test, and a data injection method and a recording medium storing a program according to the method, comprising: (a) executing data patch software; (b) receiving a file in a data patch window; (c) displaying the input file in a list box; (d) Patch the contents of the list box in part or in whole or via the Mux, Word, Analog, Discrete, Dynamic patch subwindow. Selecting and delivering a patch to the data patch window; (e) receiving a value to be patched in the data patch window; (f) selecting and executing a patch or release in the data patch window; And (g) checking a patch type and a value performed in the data patch window in a view patch window, and receiving a patch list through file input / output. (Release) is possible, can be deleted and modified, and the effect of adding, saving and adjusting the patch list through the sub window.

Flight, Aircraft, Simulation, Data, Injection, Patch / Release

Description

Method of Data Injection of Embedded System of Aircraft for Test and Flight Simulation}

The present invention relates to an aircraft embedded system for flight simulation and test, a data injection method thereof, and a recording medium storing a program according to the method, and more particularly, an OFP (Operation Flight Program) verification in a mission computer of an avionics system. The present invention relates to an aircraft embedded system and a data injection method for flight simulation and test for controlling and injecting data and information of an actual flight environment and an avionics model.

In general, after manufacturing the aircraft and before performing the test flight of the aircraft to check the operation of the equipment mounted in the aircraft to determine whether there is an abnormality, the aircraft to enable repair and replacement of the equipment in the event of an error Onboard equipment testing is mandatory.

In order to test the onboard equipment, the test apparatus is conventionally connected to the check terminals provided in the onboard equipment of the aircraft, and the test result data transmitted from each test apparatus is collected, and the normal operation of the onboard equipment is performed based on the data. Determine whether or not.

However, in such a case, since there is no system that can collectively control the operation and result collection of each test apparatus, the operator must operate each test apparatus to command the test of the onboard equipment one by one, and the test apparatus is transmitted from the test apparatus. The test results should be collected by the operator and analyzed by hand.

Therefore, it is difficult to obtain a reliable test result, which is time-consuming and reliable when performing onboard equipment test, and it is true that it is difficult to determine the abnormality using the test result data unless it is an operator who has expert knowledge in the analysis.

Therefore, there is an urgent need to develop an onboard equipment test operation system that enables the control of each test device according to the needs of the operator when testing the onboard equipment, and as a result, facilitates the collection and output of data. It became.

To this end, in the published vehicle-mounted equipment test operation system (hereinafter referred to as 'prior art 1') of Patent Publication No. 2005-0092608, the schedule of the test apparatuses in conjunction with the test apparatuses for testing the equipment mounted on the vehicle And collectively controlling operation commands, thereby facilitating collection and output of test result data.

In addition, the published real-time flight simulator interface generation system (hereinafter, referred to as 'Prior Art 2') of the published Patent Publication No. 2006-0004803 receives input of aircraft design data, a list of input / output data for each part of the aircraft, a list of mux data, etc. After loading, the data structure, modeling function call file, mux database and scaling processing file are automatically generated as source code in the form of C and Fortran and transmitted to the real-time flight simulator. Only a simple compilation was done to make the aircraft design data available.

In addition, the published mux dump data error check system of the published Patent Publication No. 2006-0004802 (hereinafter referred to as 'prior art 3') receives the mux dump data from the flight test of the aircraft input protocol check, update rate check and By automatically performing the bus list check and storing the result, it is possible to provide human and time advantages and increase reliability over conventional manual error check.

However, the prior arts such as the prior arts 1 to 3 have the following problems.

1. Because the operating system (OS) of the system is a Unix environment, it was inconvenient for general users.

2. In software (S / W), Data Injection only supports Word Patch.

3. Because patch unit is composed of word unit, if you want to change one bit, you have to patch all the words.

4. Since you need to do word-by-word patching, you must enter and verify the mask word each time.

5. There was no function to delete and modify the patch list displayed in the List Box.

6. When adding a list box, duplicate contents are added even if there are duplicate contents.

7. There is no patching function of dynamic data.

Therefore, there is an urgent need for Bit / Word unit data patch software (S / W) that injects arbitrary data from the Software Test Environment (STEM) to operate Avionics Hot Bench (AHB). It became.

The present invention has been proposed in order to solve the above technical problem, the data patch for controlling, observing and injecting data and information of the actual flight environment and avionics model for verification of Operation Flight Program (OFP) in the mission computer of the avionics system ( The purpose of the present invention is to provide an aircraft embedded system for flight simulation and test that provides a data patch function, a data injection method thereof, and a recording medium storing a program according to the method.

In addition, another object of the present invention is to provide a graphical user interface of STE (Software Test Environment) which can verify each equipment signal in real time by providing an interface with the mission computer and monitoring the signals between the interfaces. An aircraft embedded system for flight simulation and testing that provides a Graphic User Interface (GUI), a data injection method thereof, and a recording medium storing a program according to the method.

Another object of the present invention is to use wxWindow-based wxPython (a toolkit designed for GUI programming in Python and a Python version of the wxWindows library made in C ++). The present invention provides an aircraft embedded system for flight simulation and test that can be used in both Unix Xwindow and Linux Xwindow environments, a method of injecting data thereof, and a recording medium storing a program thereof.

In addition, another object of the present invention is to implement a bit patch (Bit Patch) to implement the aircraft embedded system for the flight simulation and test that can be patched only the desired bit (Bit) and its data injection method and program by the method It is to provide a stored recording medium.

In addition, another object of the present invention is to reconstruct the existing word patch to check the contents of the word list and patch (Patch) aircraft embedded system for flight simulation and test and its data injection method and program stored therein To provide a record carrier.

In addition, another object of the present invention is to provide an aircraft embedded system and a data injection method and method thereof for flight simulation and test capable of immediately deleting and modifying the content displayed on the list box and enabling selective patching. The present invention provides a recording medium storing a program.

In addition, another object of the present invention is to select the bit (Word) / Word (Word), Analog (Analog), Discrete (Discrete), Dynamic Patch (Type) The present invention provides an aircraft embedded system for flight simulation and test displaying a list corresponding to unit processing, a data injection method thereof, and a recording medium storing a program according to the method.

In addition, another object of the present invention is to include the aircraft embedded system and data injection method for flight simulation and test to avoid the duplication if there is duplicate content when adding the list box, and only change the value when the value of the list (Change) only; The present invention provides a recording medium storing a program according to the method.

It is still another object of the present invention to provide an aircraft embedded system for flight simulation and testing capable of a dynamic patch function, a data injection method thereof, and a recording medium storing a program thereof.

In addition, another object of the present invention is to receive a patch list (Patch List) through the file input and output, it is possible to selectively patch (Release), delete and modify, add a patch list through a sub-window To provide a flight embedded system for flight simulation and test that can be stored and adjusted, and a recording medium storing a data injection method thereof and a program according to the method.

As a means for solving the above problems, the method of data injection of the aircraft embedded system for flight simulation and test according to the present invention, as described in claim 1, (a) executing the data patch software and ; (b) receiving a file in a data patch window; (c) displaying the input file in a list box; (d) Patch the contents of the list box in part or in whole or via the Mux, Word, Analog, Discrete, Dynamic patch subwindow. Selecting and delivering a patch to the data patch window; (e) receiving a value to be patched in the data patch window; (f) selecting and executing a patch or release in the data patch window; And (g) checking a patch type and a value performed in the data patch window in a view patch window.

The data patch software includes an input program for receiving a patch / release list from a file open / save as described in claim 2 and displaying it in a patch list cue box; The list selected from the input program is patched according to the corresponding bit / word, or a mux patch, a word patch, an analog patch, a discrete patch, a dynamic patch A processing program for selecting and patching / releasing a desired patch from a user through a sub window; And an output program for checking a patch / released content in the processing program through a view patch and storing a file.

The mux patch performs byte unit patch data of a mux signal, as described in claim 3, and the word patch performs word unit patch data of the mux signal. The analog patch performs a patch of the analog signal, the discrete patch performs a patch of the discrete signal, the dynamic patch performs a patch of the dynamic signal, and the view patch includes mux and word. ), Analog, discrete, and dynamics patch results are displayed.

In the data injection method, as described in claim 4, in the step (d), the patch list is received through the input / output of the file to perform a selective patch / release, and the list It is characterized by modifying and deleting the contents of the box.

The data injection method may further include adding or modifying an added patch to the list box between steps (f) and (g) as described in claim 5. .

The data patch window comprises a file box for opening, storing, and saving a file as described in claim 6; A command queue text box 220 for inputting a data patch or release list information file; A list box for displaying list information of the file input in the command queue text box; All cue apply buttons (231) for patching or releasing all lists in the list box; An application selection button 232 for patching or releasing only the list checked in the list box; A delete selection button 233 for deleting only the checked list in the list box; A modification selection button (234) for modifying the list checked in the list box; Item Type combo box 241 for popping up the Mux, Word, Analog, Discrete, Dynamic patch subwindows to select the corresponding patch Wow; An Item Name text box 242 for entering a patch (item) name; A patch value text box 243 for inputting a value according to the item type; A command definition selection box 244 for selecting the item type between a patch and a release; A patch applying button (245) for patching or releasing the item name and the item value; A delete button 246 for deleting the item type and the item value; A view patch button 250 for displaying or releasing the patched list; And a list box add / insert / replace box 260 for adding, inserting, and replacing the patch name and the patch value to the list box.

As described in claim 7, the data patch window avoids duplication if there is duplicate content when adding a list box, and changes only a corresponding value when only a value of the list is changed.

As described in claim 8, the data patch software can be used in MS Window, Unix Xwindow, and Linux Xwindow environments using wxPython based on wxWindow. It is done.

As a means for solving the above-described problems, the aircraft embedded system for flight simulation and test according to the present invention, as described in claim 9, performs the OFP (Operation Flight Program) verification in the mission computer of the avionics system. It provides data patch function that controls, observes and injects data and information of actual flight environment and avionics model, and provides interface with mission computer to monitor signals between the interfaces in real time. The data patch function includes: receiving a list of patches through file input and output and displaying the list in a list box, and patching some or all of the contents of the list box or mux, word, and analog. , Discrete, Dynamic Patch subwindow The patch is selected to perform a patch or release and to check, add, insert, modify, and replace the patch type and value through the view patch.

delete

An aircraft embedded system, a data injection method, and a recording medium storing a program according to the method for flight simulation and test according to the present invention have the following effects.

1. Using wxPython, which is based on wxWindow, can be used in MS Window, Unix Xwindow, Linux Xwindow environment.

2. Implement bit patch to patch only the bit you want.

3. It is possible to patch after checking the word list contents by reinforcing the existing word patch.

4. The contents displayed on the list box can be directly deleted and modified, and selective patching is possible.

5. List corresponding to Bit / Word unit processing when selecting Mux, Word, Analog, Discrete, Dynamic Patch type Is displayed.

6. If there are duplicate contents when adding list box, avoid duplication, and if only the value of the list is changed, only the corresponding value is changed.

7. Dynamic Patch function is available.

8. The patch list can be received through file I / O, allowing for selective patch / release, deletion and modification, and adding, saving, and adjusting the patch list through the subwindow. .

Hereinafter, exemplary embodiments of the present invention will be described in detail with reference to the accompanying drawings. In describing the embodiments of the present invention, the same reference numerals will be used for components having the same functions and functions.

Menu Configuration in STE Software

1 is a menu configuration diagram of flight simulation and test environment (STE) software of the aircraft embedded system according to a preferred embodiment of the present invention.

The STE software is software for avionic system integration test equipment. Software that controls and injects data and information of actual flight environment and avionics model among GUI (Graphic User Interface) software for performing function and performance test of OFP (Operation Flight Program) and each avionics equipment in avionics mission computer (S / W).

The STE provides an interface with a mission computer, and provides a GUI (Graphic User Interface) of STEM capable of real-time verification of each equipment signal by monitoring signals between the interfaces.

The STE software provides an environment for independently testing the OFPs loaded on the MC and a simulated environment for performing avionic system-level tests. In addition, it provides a test function to solve a specific operation mode or a defect during operation of the OFP under test. The STE software also provides the ability to monitor controlled inputs and outputs for the OFP under test.

Simulation & Test Environment (STE) software for verifying Operation Flight Program (OFP) in the avionics mission computer is shown in FIG. 1, Simulation Setup (10), Mission Setup (20). , Cockpit Simulation (30), Data Analysis (40), Data Injection (50), Automatic Test (60), Utility (70), Admin (80) It is composed of details, etc., in each category. The parent frame, the STE, operates as a main window, and a child frame is configured through a drop-down menu of the main window. The data patch 100 of the present invention is one of several child frames.

First, the simulation setup (Simulation Setup: 10) is a menu for setting the entire STE environment, setting the section load (unload) for the simulation control (Simuation Control), and various flight models (Avionics Model) ) Set On (Model) / Off (Real), Flight Model (Avionics Configuration) Detail Settings (AVSR Settings, Flight Test), Loading IMDC OFP Settings, Operation Log Output Steps (All, Error) , Warning, Clear) settings are included.

The mission setup 20 is a menu for setting an aircraft mission of STE, and includes functions such as target setting (air-to-air, air-to-air), DTE setting (flight path, and armament information).

The cockpit simulation 30 simulates cockpit instrument panel simulation, mission computer power on / off simulation, MFDS simulation, IUFC simulation, sidestick simulation. Features include settings, throttle simulations, and simulation of flight and mission instrument information.

The Data Analysis 40 can display, record, and retrieve all information of STE, and includes functions such as setting up a function simulation for algorithm verification.

The Data Injection (50) is a menu that controls all data of the STE environment, and is forced through Mux, Word, Analog, and Discrete (Data Patch: 100). Discrete, Dynamic Data Injection, and Force Fault Simulation via Mux.

The automatic test 60 includes a function of adjusting an aircraft through a signal simulator or using an autopilot function.

The utility 70 is a menu for providing a utility related to STE, and includes functions such as a calculator, a database query, a joystick setting, and the like.

The Admin (80) functions such as administrator tool tool, H / W signal check, STE signal (CVT) automatic conversion, database operation, forced patch, etc. It includes.

Among the functions, the data patch (100) function controls, observes, and injects data and information of an actual flight environment and an anti-vibration model. In order to secure the reliability of the test, various test environments are provided by injecting arbitrary environmental data and model data. At this time, the type of data to be injected includes a mux patch, a word patch, an analog patch, a discrete patch, and a dynamics patch.

As shown in FIG. 2, the configuration of the data patch 100 includes an input program 110, a processing program 120, and an output program 130. .

The input program 110 receives a patch / release list from a file open / save 111 and displays the patch list queue in the patch list queue box 112. (Display). In this case, the file open / store 111 is a sub window.

The processing program 120 includes an All / Select patch 121, a Delete patch 122, a Modify patch 123, a Patch Select 124, a mux patch. (Mux Patch: 141), Word Patch: 142, Analog Patch: 143, Discrete Patch: 144, Dynamics Patch: 145, View Patch: 146 ), Patch / Release 125, Release 126, and the like.

Herein, the All / Select patch 121 selects (checks) a list from the list of the patch list cue box 112, and the Delete patch 122 selects the list. A function of deleting the checked list of the patch list cue box 112, and the Modify patch 123 functions to modify the checked list of the patch list cue box 112, and select the patch Patch Select 124 pops up the MUX, Word, Analog, Discrete, Dynamics patch windows to select the corresponding patch.

The mux patch (Mux Patch: 141), word patch (Word Patch: 142), analog patch (Analog Patch: 143), discrete patch (Discrete Patch: 144), dynamic patch (Dynamics Patch: 145), view patch ( View Patch: 146 is a sub window, and selects a patch point in each window to receive patch points in the data patch window. Run (Release).

The patches perform the following functions as shown in Table 1.

The mux patch 141 performs patch data in units of bytes of a mux signal by the patch selection 124, and the word patch 142 selects the patch ( 124 performs word unit patch data of a mux signal, and the analog patch 143 performs an analog signal patch by the patch selection 124. The discrete patch 144 performs a patch of a discrete signal by the patch selection 124, and the dynamics patch 145 is performed by the patch selection 124. Patching a Dynamics Signal is performed, and the View Patch 146 displays the results of Mux, Word, Analog, Discrete, and Dynamics patches. do.

The processing program 120 patches the list selected from the input program 110 according to the corresponding bit / word. Or, select the patch you want through the Mux Patch, Word Patch, Analog Patch, Discrete Patch, and Dynamic Patch subwindows. (Patch) / Release (125) (126).

The output program 130 outputs a patch / release 125 from the processing block 120 through a view patch 131 and stores a file. (File Save: 132). In this case, the view patch (131) and the file save (File Save: 132) are performed through a sub window.

The data patch 100 receives a patch list through a file input / output, and can be selectively patched / released and deleted and modified. In addition, patch lists can be added, stored, and adjusted through a sub window. Each mux patch 141, word patch 142, analog patch 143, discrete patch 144, dynamic patch 145, view patch 146 subwindow inquires and selects a corresponding patch point. This enables and forwards the selected patch point to the main window, Data Patch.

The data patch 100 inputs arbitrary data desired by a user by inputting a value of a selected patch point, and selects a command type from a command patch / release to patch / Release. The performed patch details can be checked through the view patch 131 window and the contents are displayed in a list box window. It also performs a release function that returns a patched value back to its original value.

Data Patch Window

3 is a screen illustrating an embodiment of a data patch window, and FIG. 4 is an explanatory diagram for describing a data patch operation in a data patch window.

The data patch window 200 includes a command queue box 210, a modify selected CVT box 240, a view patch button 250, a list box add / insert (Insert) / Replace box 260, EXIT button 271, HELP button 272, and the like.

The command queue box 210 may include a file open button 211, a save button 212, a save as button 213, and a command queue ( Command Queue text box 220, List Box 230, Apply All Ques button 231, Apply Selected button 232, Delete Selected button 233, a Modify Selected button 234, and the like.

Here, the command queue text box 220 is a place for inputting a data patch or release list information file. The list box 230 displays list information of a file input by the command queue text box 220. The apply all cue button 231 patches or releases all lists in the list box 230. The application selection button 232 patches or releases only the checked list of the list box 230. The delete selection button 233 deletes only the checked list of the list box 230. The Modify Selected button 234 modifies the checked list of the list box 230.

The Modify Selected CVT box 240 includes an Item Type combo box 241, an Item Name text box 242, a Patch Value text box 243, and a command. Command Definition selection box 244, Apply Patch button 245, Clear button 246, and the like are included.

Here, the item type combo box 241 may include a mux patch, a word patch, an analog patch, a discrete patch, and the like. Popup the Dynamic Patch window and select the patch. The Item Name text box 242 enters a patch (item) name, and the Patch Value text box 243 enters a value according to the item type. The command definition selection box 244 selects an item type from patch and release. The Apply Patch button 245 patches or releases the item name and item value. The clear button 246 functions to erase the item type and the item value.

The view patch button 250 performs a function of displaying or releasing a patched list.

The list box Add / Insert / Replace box 260 includes an Add button 261, an Insert button 262, and a Replace button 263. A patch (item) name and a patch (item) value are added, inserted, and replaced in the list box 230.

The EXIT button 271 performs a function of closing the data patch window 200, and the HELP button 272 provides help for the data patch window 200.

The data patch window 200 provides the popup window as shown in FIG. 3 with the patch selected in the item type combo box 241. The data patch window 200 includes a mux patch, a word patch, an analog patch, a discrete patch, a dynamic patch, a view patch window. Calls (Window) and returns the patch point selected in each window. Data Patch executes Patch / Release by inputting the returned value and Value.

Input of software (S / W) is Patch List through file open 211 or Mux Patch, Word Patch, Analog Patch, Discrete Patch. The patch and value values selected via the Dynamic Patch window.

The content patched in the data patch window 200 may be viewed and released through a view patch window that displays patched / released content.

Data patch

5 is a flowchart of a data patch.

First, after initializing the class, mux, word, analog, discrete, and dynamic lists are created (step S10).

Then, open the file (step S30), mux patch (step S40), word patch (step S50), discrete patch (step S60), dynamic patch ( Step S70), an analog patch (step S80), a view patch (step S90), and an exit function are selected (step S20).

If the file open (step S30) is selected, a patch list is provided to the sub window (step S31), the mux patch (step S40), the word patch (step S50), and the discrete patch (Discrete Patch) (step S60), the dynamic patch (step S70), and the analog patch (step S80) are selected through the mux patch subroutine (steps S41, S51, S61, S71). S81) Perform the patch (step S110). Then, release (step S91) can be performed through the view patch (step S90). If exit is clicked, the program is initialized after the variable is initialized (step S101).

Data injection method

A data injection method of the aircraft embedded system is described below with reference to FIG. 3.

First, when the data patch software is executed, the data patch window 200 as shown in FIG. 3 is opened.

Next, when a file is input through the data patch window 200, the input file is displayed in the list box 230.

Next, the contents of the list box 230 are partially or completely patched, modified, or deleted. If there are no files to be patched in the contents of the list box 230, the user can select a user from the MUX, Word, Analog, Discrete, and Dynamic patch subwindows. The patch is selected and delivered to the data patch window.

Next, the data patch window 200 receives a value to be patched.

Next, the patch or release is selected and executed in the data patch window 200. In this case, the added patch may be added to or modified in the list box 230.

Next, the patch type and the value performed in the data patch window 200 are checked in the view patch window. In this case, the patch may be searched through the view patch window or released to return to the original value.

Finally, when the patch and release is complete, terminate the data patch.

The data patch window 200 avoids duplication if there is duplicate content when adding the list box, and changes only the corresponding value when only the value of the list is changed. The data patch software can be used in all of MS Window, Unix Xwindow, and Linux Xwindow environments using wxPython, which is based on wxWindow.

It will be apparent to those skilled in the art that various modifications and changes can be made in the present invention without departing from the spirit or scope of the present invention as defined by the appended claims. It will be appreciated that such modifications and variations are intended to fall within the scope of the following claims.

Although the present invention has been described using an aircraft embedded system for flight simulation and testing as an example, the present invention is not limited thereto and may be applied to all software and systems in which data patches are performed.

1 is a menu diagram of the flight simulation and test environment software of the aircraft embedded system

2 is a block diagram of a data patch of the aircraft embedded system according to a preferred embodiment of the present invention

3 is a screen showing an embodiment of a data patch

4 is an explanatory diagram for explaining a data patch operation on a data patch screen;

5 is an operation flowchart of a data patch

[Description of Code for Major Parts of Drawing]

10: Simulation Setup

20: Mission Setup

30: Cockpit Simulation

40: Data Analysis

50: Data Injection

60: Automatic Test

70: Utility

80: Admin

110: input block

111: Open / Save File

112: Patch List Queue Box

120: Processing Block

121: All / Select Patch

122: Delete patch

123: Modify Patch

124: Patch Select

125: Patch / Release

126: Release (126)

130: output block

131: View Patch

132: File Save

141: Mux Patch

142: Word Patch

143: Analog Patch

144: Discrete Patch

145: Dynamics Patch

146: View Patch

200: Data Patch Window

210: Command Queue Box

211: Open button

212 Save button

213: Save As button

220: Command Queue text box

230: List Box

231: Apply All Ques button

232: Apply Selected button

233: Delete Selected button

234: Modify Selected button

240: Modify Selected CVT Box

241: Item Type combo box

242: Item Name text box

243: Patch Value text box

244 Command Definition Selection Box

245: Apply Patch button

246 Clear button

250: View Patch Button

260: Add / Insert / Replace box of list box

261: Add button

262: Insert button

263: Replace button

271: EXIT button

272: HELP button

Claims (10)

(a) executing data patch software; (b) receiving at least one file to be patched in a data patch window opened when the data patch software is executed; (c) If at least one file to be patched is displayed in a list box, or if there are no files to be patched in the list of the list box, mux, word, and analog. Selecting a file to be patched through a discrete or dynamic patch subwindow and transferring the file to the data patch window to display in the list box; (d) receiving a patch value which is a patch unit according to the file to be patched displayed in the list box in step (c); (e) selecting and executing a patch or release in the data patch window; And (f) checking a type and a patch value of a patch performed in the data patch window in a view patch window. The software of claim 1 wherein the data patch software is: An input program for receiving a patch / release list from file open / save and displaying the patch list in a patch list cue box; The list selected from the input program is patched according to the corresponding bit / word, or a mux patch, a word patch, an analog patch, a discrete patch, a dynamic patch A processing program for selecting and patching / releasing a desired patch from a user through a sub window; And And an output program for checking a patch / released content in the processing program through a view patch and storing a file. 2. The method of claim 2, The mux patch performs patch data in byte units of a mux signal, the word patch performs word unit patch data of the mux signal, and the analog patch performs patch of an analog signal. And the discrete patch performs a patch of the discrete signal, the dynamic patch performs a patch of the dynamic signal, and the view patch includes mux, word, analog, discrete, and discrete. , Dynamics patch data display method of the aircraft embedded system, characterized in that for displaying. The method of claim 1, wherein the data injection method is: In the step (d), receiving a patch list through the input and output of the file to perform a selective patch (Release), the contents of the list box of the aircraft embedded system, characterized in that for deleting Data injection method. The method of claim 1, wherein the data injection method is: Between (f) and (g), adding or modifying the added patch to the list box; Data injection method of the aircraft embedded system further comprises. The method of claim 1, wherein the data patch window is: A file box for opening, saving, and saving a file; A command queue text box 220 for inputting a data patch or release list information file; A list box for displaying list information of the file input in the command queue text box; All cue apply buttons (231) for patching or releasing all lists in the list box; An application selection button 232 for patching or releasing only the list checked in the list box; A delete selection button 233 for deleting only the checked list in the list box; A modification selection button (234) for modifying the list checked in the list box; Item Type combo box 241 for popping up the Mux, Word, Analog, Discrete, Dynamic patch subwindows to select the corresponding patch Wow; An Item Name text box 242 for entering a patch (item) name; A patch value text box 243 for inputting a value according to the item type; A command definition selection box 244 for selecting the item type between a patch and a release; A patch apply button 245 for patching or releasing the item name and the item value; A delete button 246 for deleting the item type and the item value; A view patch button 250 for displaying or releasing the patched list; And And a list box add / insert / replace box 260 for adding, inserting and replacing the patch name and the patch value to the list box. Injection method. 7. The method of claim 6, wherein the data patch window is: Method of injecting data in an aircraft embedded system, characterized in that if there are duplicate contents when adding a list box, avoid duplication, and only the value is changed when only the value of the list is changed. The software of claim 1 wherein the data patch software is: Using wxPython, which is based on wxWindow, can be used in MS Window, Unix Xwindow, Linux Xwindow environment. delete delete

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