CN114141095A - Flight simulator semi-physical simulation instrument system and implementation method thereof - Google Patents
Flight simulator semi-physical simulation instrument system and implementation method thereof Download PDFInfo
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- CN114141095A CN114141095A CN202111388564.3A CN202111388564A CN114141095A CN 114141095 A CN114141095 A CN 114141095A CN 202111388564 A CN202111388564 A CN 202111388564A CN 114141095 A CN114141095 A CN 114141095A
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- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
- G09B9/16—Ambient or aircraft conditions simulated or indicated by instrument or alarm
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B17/00—Systems involving the use of models or simulators of said systems
- G05B17/02—Systems involving the use of models or simulators of said systems electric
Abstract
The invention relates to the field of aeromechanical instrument panels, in particular to a flight simulator semi-physical simulation instrument system and an implementation method thereof, which specifically take the development of an instruction horizon sensor as an example, the design methods of other types of simulation instrument systems are the same, and the instruction horizon sensor system specifically comprises the following steps: the system comprises a panda development board, a video signal driving board and a customized display; the specific implementation method comprises the following steps: s1, instructing the graphic preparation work of the horizon finder; s2, establishing a horizon model based on the instructions of GL Studio; s3, developing a horizon finder function software based on GL Studio in combination with an instruction of MS VC + +8.0, designing and developing texture subcomponents of various types of aeronautical instruments based on GL Studio, realizing design and realization of a flight simulator simulation instrument, completing the creation steps of various types of aeronautical instruments and generating corresponding executable files, deploying the executable files in a panda hardware platform with an embedded Win10 operating system, and having good expansibility.
Description
Technical Field
The invention relates to the field of aero-mechanical instrument panels, in particular to a flight simulator semi-physical simulation instrument system and an implementation method thereof.
Background
The traditional mechanical instrument is generally composed of an aviation bus interface, a motor, a transmission gear and a mechanical instrument panel, so the traditional mechanical instrument can also be understood as an electromechanical integrated instrument. Taking a certain engine exhaust temperature table as an example, the working mode is as follows: the electric signal is transmitted through the bus interface, the driving motor rotates, and then the transmission gear moves, and the pointer of the dial plate rotates.
The mechanical instrument has the greatest advantage of strong anti-interference performance during air combat flight, and the traditional mechanical instrument is adopted in the weapon fire control training flight simulator and the full-mission type flight simulator distributed by the Soviet series warplane in the active air combat military. However, in order to control the rotation of the mechanical instrument, especially when the angle spans 360 ° (namely 0 °), a complicated PID control algorithm needs to be designed to perform the rotation across the critical angle. Similarly, in order to improve the simulation fidelity of the simulator, higher requirements are put forward on the design precision of the mechanical instrument, the design requirements on precision devices such as gears and the like are increased virtually, and the design cost is improved.
The flight simulator is used as equipment for ground simulated flight training, the operation environment of the flight simulator is almost free from strong external interference compared with a real airplane, so that a non-mechanical instrument can be completely used for replacing in the simulation process of the cockpit instrument. At present, a mature scheme is that a mode of combining a mechanical dial plate with an embedded driving module is adopted to realize a simulation instrument of a flight simulator. Taking a flap cold air pressure gauge as an example, the disassembled view is shown in the following fig. 2, and the working mode is as follows: the electric signal is transmitted through the bus interface, the driving module is enabled, the motor is driven to move, and the pointer of the dial plate rotates.
It can be seen that the driving effect is the same as that of a mechanical instrument without considering the interference resistance factor. The control method is characterized in that the control method can be used for controlling the rotation of the instrument pointer at a critical point by programming the driving module, and the control algorithm design of the mechanical dial plate is greatly reduced. When the simulated aviation instrument is complex, such as an instruction horizon and a channel compass indicator, the design mode puts more requirements on the function selection of the driving module, and the number of the rotating motors also needs to be correspondingly increased step by step along with the increase of the steering dimension of the instrument pointer.
Summarizing the defects of the mechanical instrument, the problems of complex manufacturing process, higher economic cost, need of designing complex control algorithm, general pointer rotation precision and the like exist; for the simulation instrument of the mechanical dial plate combined with the embedded driving module, the problems of complex manufacturing process, difficult simulation of complex aviation instruments and the like exist.
Disclosure of Invention
In order to solve the problems, the invention provides a flight simulator semi-physical simulation instrument system and an implementation method thereof.
A flight simulator semi-physical simulation instrumentation system comprising:
the panda developing board is connected with the flight simulator cabin and realizes UDP message transmission through network cable connection;
the video signal driving board is used for receiving the executable file deployment generated in the first stage of the panda lata development board, outputting and displaying the execution file operation result;
and the customized display displays specific instrument information to the user side through the HDMI video signal.
The flight simulator cockpit provides 5V2A electricity for latte panda development board.
The panda latte development board is provided with an operating system, develops a flight simulator simulation instrument based on GL Studio, and packages the developed instrument to generate a corresponding executable file.
The operating system is Windows XP and the operating systems above.
The method for realizing the semi-physical simulation instrument system of the flight simulator takes the development of an instruction horizon instrument as an example, the design methods of other types of simulation instrument systems are the same, and the method comprises the following specific steps:
s1, instructing graphic preparation work of the horizon finder: preparing a meter photo material and creating a meter texture through a drawing tool;
s2, establishing a horizon model based on the instructions of GL Studio;
and S3, developing the level-finder function software based on GL Studio combined with the instructions of MS VC + + 8.0.
The step S1 specifically includes the following steps:
a. through the component division of the command horizon instrument real object, the dial plate is designed into 5 subcomponents which can be spliced and combined independently;
b. and drawing texture pictures of 5 sub-components through drawing tools.
The step S2 specifically includes the following steps:
1) a project based on 'GL Studio3.2 Application Wizard' is newly built in MS VC + +8.0 and named as 'MeterHorizon';
2) opening a file of a suffix name of 'gls' in the project, and designing a horizon model of the instruction;
3) firstly, adding a 'Rectangle' object in a GL Studio drawing panel, and naming; then adding a texture to the named object;
4) repeating the third step, wherein the added "Rectangle" object and the corresponding texture are sequentially as follows: the scale plate part, the instrument rotation background part, the pointer scale plate part and the instrument inner shell part.
The step S3 specifically includes the following steps:
a. firstly, editing a control code of a meter sub-component in GL Studio; then generating a header file and a source file code of the command horizon finder object and further realizing the development work of the simulation instrument by combining MS VC + + 8.0;
b. editing command horizon control codes in a Code page of GL Studio, editing codes in void call (double time), and realizing simulation motion of the command horizon;
c. generating a header file and a source file code of the command horizon object;
d. and adding the header file and the source file in a MeterHorzon project, adding a network communication module based on a UDP protocol, and editing and generating an executable file of the level-finder simulation instrument.
The invention has the beneficial effects that: the method is characterized in that texture subcomponents of various types of aviation instruments are developed based on GL Studio design, design and implementation of flight simulator simulation instruments are achieved, model creation steps of various types of aviation instruments are completed, corresponding executable files are generated, the executable files are deployed in a panda hardware platform with an embedded Win10 operating system, and the simulation instruments are generated by encapsulation.
Drawings
The invention is further explained by combining the drawings and the embodiment, the invention takes the command horizon sensor as a case to carry out the research and development of the real object, and the design methods of other types of simulation instrument systems are the same.
FIG. 1 is a schematic structural diagram of a design and implementation flow of a flight simulator simulation instrument based on GL Studio in the invention;
FIG. 2 is a schematic structural diagram of an inner shell component of the command horizon sensor semi-physical simulation instrument of the present invention;
FIG. 3 is a schematic structural diagram of a pointer component of the command horizon semi-physical simulation instrument of the invention;
FIG. 4 is a schematic structural diagram of a pointer scale plate component of the command horizon finder semi-physical simulation instrument of the present invention;
FIG. 5 is a schematic structural diagram of a scale plate component of the command horizon finder semi-physical simulation instrument of the present invention;
FIG. 6 is a schematic structural diagram of a rotating background component of the command horizon semi-physical simulation instrument of the present invention;
FIG. 7 is a first three-dimensional schematic diagram of an instruction horizon sensor semi-physical simulation instrument according to the present invention;
FIG. 8 is a second three-dimensional schematic diagram of the command horizon finder semi-physical simulation instrument of the present invention;
FIG. 9 is a front view of the commanded horizon semi-physical simulation instrument of the present invention;
FIG. 10 is a left side view of the commanded horizon semi-physical simulation instrument of the present invention;
FIG. 11 is a right side view of the commanded horizon semi-physical simulation instrument of the present invention;
FIG. 12 is a top view of the commanded horizon semi-physical simulation instrument of the present invention;
FIG. 13 is a bottom view of the commanded horizon finder semi-physical simulation instrument of the present invention;
FIG. 14 is a rear view of the commanded horizon semi-physical simulation instrument of the present invention;
fig. 15 is a flowchart of development, deployment and implementation of the command horizon semi-physical simulation instrument of the present invention.
Detailed Description
In order to make the technical means, the creation characteristics, the achievement purposes and the effects of the invention easy to understand, the invention is further explained below.
As shown in fig. 15, a flight simulator semi-physical simulation instrument system includes:
the panda developing board is connected with the flight simulator cabin and realizes UDP message transmission through network cable connection;
the video signal driving board is used for receiving the executable file deployment generated in the first stage of the panda lata development board, outputting and displaying the execution file operation result;
and the customized display displays specific instrument information to the user side through the HDMI video signal.
As can be seen from the flowchart of fig. 15, the development, deployment and implementation processes are mainly divided into three main stages:
the first stage is as follows: developing a flight simulator simulation instrument based on GL Studio in Windows XP and the operating systems, and packaging to generate a corresponding executable file after the development is finished;
and a second stage: completing the installation of an operating system and the connection relation of hardware based on a latte panda development board, and installing a Win10 operating system in the development board; then 5V2A is led out through the flight simulator cabin for supplying power, and UDP messages are transmitted through network cable connection;
the third stage: and deploying the executable file generated in the first stage in a panda latte development board, operating the executable file, and finally displaying specific instrument information to a user terminal through a video signal driving board and a customized display through an HDMI video signal.
The embedded computer graphic simulation instrument based on GL Studio and latte panda hardware platforms can be used for software development of the computer graphic simulation instrument on Windows XP and above platforms, and mainly utilizes GL Studio tools to design the simulation instrument and generate class codes of the corresponding instrument; then, combining with an MS VC + +8.0 software design development platform, editing communication and control source codes of the simulation instrument, and issuing and generating an executable binary file; and finally, the execution file is deployed in a panda lata hardware platform provided with an embedded Win10 operating system, and a simulation instrument is generated by packaging, so that the simulation instrument has good expansibility, the design and development of different types of instruments can be realized by designing and modifying the form of GL Studio configuration files, and meanwhile, the hardware system has low cost, is easy to replace, has a simple connection mode, and can realize personalized customization of different requirements.
The flight simulator cockpit provides 5V2A electricity for latte panda development board.
The panda latte development board is provided with an operating system, develops a flight simulator simulation instrument based on GL Studio, and packages the developed instrument to generate a corresponding executable file.
The operating system is Windows XP and the operating systems above.
The background description of the conventional simulation instrument is specifically shown in table 1:
TABLE 1 comparison of the simulated instrument techniques in three ways
As shown in fig. 1, a method for implementing a semi-physical simulation instrument system of a flight simulator is described by taking an instruction horizon as an example, and other types of simulation instrument systems are designed in the same way, and the method includes the following specific steps:
s1, instructing graphic preparation work of the horizon finder: preparing meter photo material and creating a meter texture through a drawing tool, as shown in fig. 2 to 6;
a. instrument photo material: through the component division of the command horizon instrument real object, the dial plate is designed into 5 subcomponents which can be spliced and combined independently;
s2, establishing a horizon model based on instructions of GL Studio:
1) a project based on 'GL Studio3.2 Application Wizard' is newly built in MS VC + +8.0 and named as 'MeterHorizon';
2) opening a file of a suffix name of 'gls' in the project, and designing a horizon model of the instruction;
3) firstly, adding a 'Rectangle' object in a GL Studio drawing panel, and naming; then adding a texture to the named object;
4) repeating the third step, wherein the added "Rectangle" object and the corresponding texture are sequentially as follows: the scale plate part, the instrument rotation background part, the pointer scale plate part and the instrument inner shell part;
s3, developing the functional software of the horizon finder based on GL Studio combined with MS VC + + 8.0:
a. firstly, editing a control code of a meter sub-component in GL Studio; then generating a header file and a source file code of the command horizon finder object and further realizing the development work of the simulation instrument by combining MS VC + + 8.0;
b. editing command horizon control codes in a Code page of GL Studio, and editing the following codes in void call (double time) for realizing simulation motion of the command horizon;
realizing pitching movement of scale plate parts
f＝gRecvData.horizon_pitch*-2.5f；
ScalePitch->DynamicTranslate(0,f,0,false)；
Realizing a rolling movement of the scale plate part
f＝gRecvData.horizon_roll*-1；
ScalePitchGroup->DynamicRotate(f,Z_AXIS)；
V/effecting rotation of the aircraft beacon in the pointer unit
f＝gRecvData.horizon_plane；
PlaneLeft->DynamicTranslate(0,f,0,false)；
PlaneRight->DynamicTranslate(0,f,0,false)；
V/realizing the rotation of the airplane mark shadow in the pointer part
PlaneShaderL->DynamicTranslate(0,f,0,false)；
PlaneShaderR->DynamicTranslate(0,f,0,false)；
c. Generating a header file and a source file code of the command horizon object;
d. and adding the header file and the source file in a MeterHorzon project, adding a network communication module based on a UDP protocol, and editing and generating an executable file of the level-finder simulation instrument.
The design and development work of the simulation instrument is mainly completed in a computer software platform, an executable file corresponding to the simulation instrument is finally generated, then an enterprise-version LatteBanda Win10 embedded hardware platform is selected according to engineering requirements, and the executable file is deployed on the platform, so that the semi-physical simulation instrument of the flight simulator can be completed.
The GL studio3.2 is composed of a graphic design area (Geometry), a Code editing area (Code), an Application design area (Application), a source Code Generation area (Generation) and a resource editing area (Resources). As design developers, a graphic design area and a source code generation area are mainly used. The graphic design area provides a 'what you see is what you get' graphic editing interactive window and provides interactive operation interfaces such as design Modes (models), design conversion (Convert), design adjustment (Modify) and design creation (Create), so that visual creation and design of a user are more convenient. And the code generation area is used for generating a corresponding C + + class module for the visual interface object created by the user, and the user can control the visual object by editing, debugging and calling the class.
As shown in fig. 7 to 14, for the design of the command horizon instrument semi-physical simulation instrument, the flight simulator simulation instrument based on GL Studio is provided with a shell corresponding to the simulation instrument, and the shell is changed in size according to the appearance requirement of the simulation instrument.
The method is characterized in that texture sub-components of various types of aviation instruments are developed based on GL Studio design, design and implementation of flight simulator simulation instruments are achieved, model creation steps of various types of aviation instruments are completed, corresponding executable files are generated, the executable files are deployed in a panda hardware platform with an embedded Win10 operating system, the simulation instruments are generated through encapsulation, and good expansibility is achieved.
The foregoing shows and describes the general principles, essential features, and advantages of the invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are merely illustrative of the principles of the invention, but that various changes and modifications may be made without departing from the spirit and scope of the invention, which fall within the scope of the invention as claimed. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (8)
1. The utility model provides a flight simulator semi-physical simulation instrument system which characterized in that: the method comprises the following steps:
the panda developing board is connected with the flight simulator cabin and realizes UDP message transmission through network cable connection;
the video signal driving board is used for receiving the executable file deployment generated in the first stage of the panda lata development board, outputting and displaying the execution file operation result;
and the customized display displays specific instrument information to the user side through the HDMI video signal.
2. The semi-physical simulation instrumentation system of a flight simulator according to claim 1, wherein: the flight simulator cockpit provides 5V2A electricity for latte panda development board.
3. The semi-physical simulation instrumentation system of a flight simulator according to claim 1, wherein: the panda latte development board is provided with an operating system, develops a flight simulator simulation instrument based on GL Studio, and packages the developed instrument to generate a corresponding executable file.
4. The semi-physical simulation instrumentation system of a flight simulator according to claim 1, wherein: the operating system is Windows XP and the operating systems above.
5. The method for implementing the semi-physical simulation instrument system of the flight simulator according to any one of claims 1 to 4, taking the development of an instruction horizon as an example, the design methods of other types of simulation instrument systems are the same, and the method is characterized in that: the method comprises the following specific steps:
s1, instructing graphic preparation work of the horizon finder: preparing a meter photo material and creating a meter texture through a drawing tool;
s2, establishing a horizon model based on the instructions of GL Studio;
and S3, developing the level-finder function software based on GL Studio combined with the instructions of MS VC + + 8.0.
6. The method for implementing the semi-physical simulation instrument system of the flight simulator according to claim 5, wherein the method comprises the following steps: the step S1 specifically includes the following steps:
a. through the component division of the command horizon instrument real object, the dial plate is designed into 5 subcomponents which can be spliced and combined independently;
b. and drawing texture pictures of 5 sub-components through drawing tools.
7. The method for implementing the semi-physical simulation instrument system of the flight simulator according to claim 5, wherein the method comprises the following steps: the step S2 specifically includes the following steps:
1) a project based on 'GL Studio3.2 Application Wizard' is newly built in MS VC + +8.0 and named as 'MeterHorizon';
2) opening a file of a suffix name of 'gls' in the project, and designing a horizon model of the instruction;
3) firstly, adding a 'Rectangle' object in a GL Studio drawing panel, and naming; then adding a texture to the named object;
4) repeating the third step, wherein the added "Rectangle" object and the corresponding texture are sequentially as follows: the scale plate part, the instrument rotation background part, the pointer scale plate part and the instrument inner shell part.
8. The method for implementing the semi-physical simulation instrument system of the flight simulator according to claim 5, wherein the method comprises the following steps: the step S3 specifically includes the following steps:
a. firstly, editing a control code of a meter sub-component in GL Studio; then generating a header file and a source file code of the command horizon finder object and further realizing the development work of the simulation instrument by combining MS VC + + 8.0;
b. editing command horizon control codes in a Code page of GL Studio, editing codes in void call (double time), and realizing simulation motion of the command horizon;
c. generating a header file and a source file code of the command horizon object;
d. and adding the header file and the source file in a MeterHorzon project, adding a network communication module based on a UDP protocol, and editing and generating an executable file of the level-finder simulation instrument.
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Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104269083A (en) * | 2014-09-04 | 2015-01-07 | 吉林医药学院 | Low-cost flight simulator cabin display and control system |
| CN204965047U (en) * | 2015-07-20 | 2016-01-13 | 北京创想联发科技有限公司 | Embedded synthesis shows emulation instrument based on ARM |
| CN106842984A (en) * | 2017-01-22 | 2017-06-13 | 北京航空航天大学 | A kind of dynamic electron instrument simulation method that real-time textures are rendered |
| CN106934132A (en) * | 2017-02-28 | 2017-07-07 | 西安交通大学 | A kind of flight management simulation system and analogy method |
| CN207602068U (en) * | 2017-09-01 | 2018-07-10 | 北京世纪晨数据技术有限责任公司 | A kind of simulation instrument system for flight simulator |
| CN108346343A (en) * | 2018-01-26 | 2018-07-31 | 四川翔步科技有限公司 | A kind of meter renderings method of flight simulation cockpit instrument simulation panel |
| CN108345223A (en) * | 2018-01-26 | 2018-07-31 | 四川翔步科技有限公司 | A kind of data transmission method of flight simulation cockpit instrument simulation panel |
| CN110634351A (en) * | 2019-09-29 | 2019-12-31 | 中仿智能科技（上海）股份有限公司 | Aviation horizon sensor control system of flight simulator |
-
2021
- 2021-11-22 CN CN202111388564.3A patent/CN114141095A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104269083A (en) * | 2014-09-04 | 2015-01-07 | 吉林医药学院 | Low-cost flight simulator cabin display and control system |
| CN204965047U (en) * | 2015-07-20 | 2016-01-13 | 北京创想联发科技有限公司 | Embedded synthesis shows emulation instrument based on ARM |
| CN106842984A (en) * | 2017-01-22 | 2017-06-13 | 北京航空航天大学 | A kind of dynamic electron instrument simulation method that real-time textures are rendered |
| CN106934132A (en) * | 2017-02-28 | 2017-07-07 | 西安交通大学 | A kind of flight management simulation system and analogy method |
| CN207602068U (en) * | 2017-09-01 | 2018-07-10 | 北京世纪晨数据技术有限责任公司 | A kind of simulation instrument system for flight simulator |
| CN108346343A (en) * | 2018-01-26 | 2018-07-31 | 四川翔步科技有限公司 | A kind of meter renderings method of flight simulation cockpit instrument simulation panel |
| CN108345223A (en) * | 2018-01-26 | 2018-07-31 | 四川翔步科技有限公司 | A kind of data transmission method of flight simulation cockpit instrument simulation panel |
| CN110634351A (en) * | 2019-09-29 | 2019-12-31 | 中仿智能科技（上海）股份有限公司 | Aviation horizon sensor control system of flight simulator |
Non-Patent Citations (1)
| Title |
|---|
| 高颖 郭淑霞: "虚拟现实视景仿真技术", 西北工业大学出版社 * |
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