CN109558637B - Cross-platform interactive aircraft system dynamic schematic diagram design method - Google Patents

Cross-platform interactive aircraft system dynamic schematic diagram design method Download PDF

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CN109558637B
CN109558637B CN201811275587.1A CN201811275587A CN109558637B CN 109558637 B CN109558637 B CN 109558637B CN 201811275587 A CN201811275587 A CN 201811275587A CN 109558637 B CN109558637 B CN 109558637B
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schematic diagram
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software
dynamic schematic
dynamic
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CN109558637A (en
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刘涛
杨良勇
孙闻
孙义军
邴志光
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Anhui Huamin Avionics System Co ltd
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Abstract

The invention discloses a method for designing a dynamic schematic diagram of a cross-platform interactive airplane system, which comprises the steps of system requirement analysis, scheme making, software development, performance testing, unified specification of a dynamic schematic diagram technology, and cross-platform multi-terminal application and release; through a dynamic schematic diagram modularization assembly technology, according to the existing dynamic schematic diagram software specification, aiming at each system of a navigation aircraft, module resources capable of accurately and clearly displaying the principle of the aircraft system are manufactured, resources in a library are directly used in the later stage, the continuity and the uniformity of the software on the form and the content are guaranteed, GL Studio software is used for connecting the GL Studio software with HLA/DIS simulation application, generated C + + and OpenGL source codes can independently run and are embedded into other application programs, through adopting a cross-platform application compiling mode, the software source codes manufactured by using the dynamic schematic diagram module library have platform-independent attributes, are compiled into different formats and are issued to terminals such as a computer, a mobile phone, a tablet and the like.

Description

Cross-platform interactive aircraft system dynamic schematic diagram design method
Technical Field
The invention belongs to the field of aircraft system simulation and training, and particularly relates to a cross-platform interactive aircraft system dynamic schematic diagram design method.
Background
With the development of the domestic navigation industry, training for flight and maintenance is also common. In the training process, the training of the airplane system principle is a key link of theoretical training and simulator operation training. A dynamic schematic diagram of a navigation aircraft system is an important component of training equipment such as a simulator and the like, and dynamically and clearly shows the system principle of the navigation aircraft for trainees.
At present, the development of the dynamic schematic diagram of the navigation aircraft in China is just started, the technology of the existing dynamic schematic diagram is various, but the technology of the schematic diagram which can be used universally across platforms does not exist, the level depth, UI display and platform foundation of a product are greatly different, the schematic diagrams of different devices of various platforms need to be developed independently, the universality is poor, the transportability is not realized, and a large amount of resources are wasted for the development and development of the schematic diagram in the later period.
Therefore, designing and developing an interactive cross-platform dynamic schematic diagram is an indispensable way for the navigation training industry, the principle of an airplane system is visually and interactively presented for trainees by using related software and methods, the cross-platform schematic diagram convenient to transplant is realized, and the cross-platform dynamic schematic diagram can be used for various training devices, different operating system platforms and various terminals, has a huge support effect on the navigation training industry and has great market value on navigation development.
Disclosure of Invention
The invention provides a method for designing a dynamic schematic diagram of a cross-platform interactive airplane system, which aims to solve the problems that the existing dynamic schematic diagram has various technologies, but a cross-platform universal schematic diagram technology is not available, the hierarchy depth, UI (user interface) display and platform foundation of a product are greatly different, the schematic diagrams of different devices of various platforms need to be developed independently, the universality is poor, the transportability is not provided, and a large amount of resources are wasted for the development and development of the schematic diagram at the later stage.
The invention relates to a method for designing a dynamic schematic diagram of a cross-platform interactive airplane system, which comprises the following steps:
the method comprises the following steps: analyzing system requirements: specific analysis is made according to the training requirements of the navigation aircraft, and the system principle needing simulation is determined;
step two: and (3) formulating a scheme: according to the system requirement analysis in the first step, a development scheme is formulated, the expression form of the dynamic schematic diagram of each system is determined, the simulation program of each system component is determined, required materials are collected, and target software is determined;
step three: software development: developing a schematic diagram by combining commercial software GL Studio and related software and plug-ins;
step four: and (3) performance testing: testing personnel are required to test the performance of the schematic diagram;
step five: unified specification of dynamic schematic techniques: making a uniform universal technical specification on software content, UI display forms and aircraft system logic depth;
step six: applying and releasing by multiple terminals in a cross-platform manner: the method adopts a cross-platform application compiling mode aiming at different use platforms.
Preferably, the software development in the third step adopts a dynamic principle graph modularization assembly technology.
Preferably, the dynamic schematic diagram modularized assembly technology takes a model driving architecture as guidance, designs a platform-independent model of a mechanical training dynamic schematic diagram, and researches and manufactures a software module of the dynamic schematic diagram which is independent of an operation platform.
Preferably, according to the unified dynamic schematic diagram design specification in the fifth step, module resources capable of accurately and clearly displaying the principle of the aircraft system are integrated for each system of the aircraft, and the resource modules and the platform-independent dynamic schematic diagram module form a unified general dynamic schematic diagram module library.
Preferably, the dynamic schematic diagram platform-independent model is developed by GL Studio software.
Preferably, the cross-platform application compiling mode is that a software source code manufactured by using a dynamic schematic diagram module library has a platform-independent attribute and aims at different use platforms.
Compared with the prior art, the invention has the beneficial effects that: by utilizing the dynamic schematic diagram modularized assembly technology and aiming at each system of the navigation aircraft, the module resource capable of accurately and clearly displaying the principle of the aircraft system is manufactured according to the existing dynamic schematic diagram software specification, so that in the later development process of the dynamic schematic diagram, the resource in a library is used for manufacturing the schematic diagram of the specific aircraft system in a 'building block' mode, and the continuity and the uniformity of the software in form and content are ensured. The GL Studio software is connected with HLA/DIS simulation application, generated C + + and OpenGL source codes can be independently operated to be embedded into other application programs, a cross-platform application compiling mode is adopted, software source codes manufactured by a dynamic schematic diagram module library have platform-independent attributes, are compiled into different formats and are issued to terminals such as a computer, a mobile phone, a tablet and the like.
Drawings
FIG. 1 is a general schematic diagram of an embodiment of the present invention.
FIG. 2 is a flowchart of software development according to an embodiment of the present invention.
Fig. 3 is a system architecture diagram of an embodiment of the present invention.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
Example 1
According to fig. 1-3, the invention provides a method for designing a dynamic schematic diagram of a cross-platform interactive aircraft system, which comprises the following steps:
the method comprises the following steps: analyzing system requirements: specific analysis is made according to the training requirements of the navigation aircraft, and the system principle needing simulation is determined;
step two: and (3) formulating a scheme: according to the system requirement analysis in the first step, a development scheme is formulated, the expression form of the dynamic schematic diagram of each system is determined, the simulation program of each system component is determined, required materials are collected, and target software is determined;
step three: software development: developing a schematic diagram by combining commercial software GL Studio, related software and plug-ins, developing the schematic diagram according to a formulated scheme, wherein the schematic diagram comprises picture collection, texture generation, UI design, a named entity, component creation, design behavior events, code generation and debugging components, if the schematic diagram needs to be changed, the schematic diagram returns to a UI design link for redesign, and when the codes need to be publicized and changed, the schematic diagram is stored in a GLs format and is embedded into other application programs, dll or so is generated; when the Active plug-in is used, the Active plug-in is packaged into a cab file; when the components are running independently, they are stored in the. Exe format.
Step four: and (4) performance testing: testing personnel are required to test the performance of the schematic diagram;
step five: unified specification of dynamic schematic techniques: making a uniform universal technical specification on software content, UI display forms and aircraft system logic depth;
step six: applying and releasing by multiple terminals in a cross-platform manner: the method adopts a cross-platform application compiling mode, and aiming at different use platforms, the current mainstream cross-terminal platform development technology is roughly divided into a cross-platform running engine mode and a cross-platform application compiling mode according to the implementation mode. The project adopts a cross-platform application compiling mode, software source codes manufactured by utilizing a dynamic schematic diagram module library have platform-independent attributes, and compiling linkers supporting multi-platform release are manufactured aiming at different using platforms, such as exe, OFFICE, browsers, iOS systems and android systems on Windows systems. The information is compiled into different formats and then is released to terminals such as computers, mobile phones and tablets. .
In the method for designing the dynamic schematic diagram of the cross-platform interactive aircraft system, software development in the third step adopts a dynamic schematic diagram modular assembly technology, a Model Driven Architecture (MDA) is used as guidance, a Platform Independent Model (PIM) of a engineering training dynamic schematic diagram is designed, and a dynamic schematic diagram software module independent of an operation platform is researched and manufactured. According to the existing dynamic schematic diagram software specification, module resources capable of accurately and clearly displaying the principle of the aircraft system are manufactured for each system of the navigation aircraft, and the dynamic schematic diagram modules irrelevant to the platform form a unified and general dynamic schematic diagram module library. In the later development process of the dynamic schematic diagram, the resources in the library are used to produce the schematic diagram of the specific airplane system in a 'building block' mode, and the consistency and the unity of the software on the form and the content are ensured.
The method for designing the dynamic schematic diagram of the cross-platform interactive airplane system adopts a dynamic schematic diagram modularized assembly technology, takes a model driving architecture as guidance, designs a platform-independent model of a dynamic schematic diagram for the engineering training, and researches and manufactures a software module of the dynamic schematic diagram which is independent of an operation platform.
According to the design specification of the unified dynamic schematic diagram in the step five, module resources capable of accurately and clearly displaying the principle of the aircraft system are integrated for each system of the aircraft, and the resource modules and the platform-independent dynamic schematic diagram module form a unified general dynamic schematic diagram module library which comprises a data layer, a function presentation layer and a man-machine interaction layer required by the system. The GL Studio is used for developing various system schematic diagrams of the navigation airplane, the states of the system schematic diagrams are represented on a function presentation layer, a data communication pipeline running in an independent thread (or process) is built at the same time, data of a bottom data layer are obtained, and a user can carry out interactive operation on the system on an interaction layer.
The design method of the cross-platform interactive aircraft system dynamic schematic diagram is characterized in that a dynamic schematic diagram platform independent model is developed by adopting GL Studio software, and the GL Studio software is utilized to develop the aircraft system dynamic schematic diagram. GL Studio is a specialized instrument simulation platform that is used as a platform-independent rapid prototyping tool to create real-time, three-dimensional, photo-level interactive graphical interfaces. The method can be connected with HLA/DIS simulation application, and the generated C + + and OpenGL source codes can be independently operated and can be embedded into other application programs, so that a large amount of complicated bottom-layer OpenGL development is avoided.
According to the method for designing the dynamic schematic diagram of the cross-platform interactive aircraft system, a cross-platform application compiling mode is adopted, software source codes manufactured by utilizing a dynamic schematic diagram module library have platform-independent attributes, and are compiled into different formats aiming at different use platforms and then are issued to terminals such as a computer, a mobile phone and a tablet.
Example 2
According to fig. 1-3, the invention provides a method for designing a dynamic schematic diagram of a typical navigation aircraft system, which comprises the following steps:
the method comprises the following steps: analyzing system requirements: specific analysis is made according to the training requirements of the navigation aircraft, and the system principle needing simulation is determined;
step two: and (3) formulating a scheme: according to the system requirement analysis in the first step, a development scheme is formulated, the expression form of the dynamic schematic diagram of each system is determined, the simulation program of each system component is determined, required materials are collected, and target software is determined;
step three: software development: developing a schematic diagram by combining commercial software GL Studio, related software and plug-ins, and according to a formulated scheme, developing the schematic diagram, wherein the schematic diagram comprises picture collection, texture generation, UI design, named entities, component creation, design behavior events, code generation and debugging components, if the schematic diagram needs to be changed, the schematic diagram returns to a UI design link for redesign, and when the codes need to be disclosed and changed, the schematic diagram is stored in a GLs format, and when other application programs are embedded, dll or so is generated; when the Active plug-in is used, the Active plug-in is packaged into a cab file; when the components are run independently, they are stored in the. Exe format.
Step four: and (3) performance testing: testing personnel are required to test the performance of the schematic diagram;
step five: unified specification of dynamic schematic techniques: making a uniform universal technical specification on software content, UI display forms and aircraft system logic depth;
step six: applying and releasing by multiple terminals across platforms: the method adopts a cross-platform application compiling mode, and aiming at different use platforms, the current mainstream cross-terminal platform development technology is roughly divided into a cross-platform operation engine mode and a cross-platform application compiling mode according to the implementation mode. The project adopts a cross-platform application compiling mode, software source codes manufactured by utilizing a dynamic schematic diagram module library have platform-independent attributes, and compiling linkers supporting multi-platform release are manufactured aiming at different using platforms, such as exe, OFFICE, browsers, iOS systems and android systems on Windows systems. The information is compiled into different formats and then is released to terminals such as computers, mobile phones and tablets. .
In the method for designing the dynamic schematic diagram of the typical navigation aircraft system, in the third step, the software development adopts a dynamic schematic diagram modular assembly technology, a Model Driven Architecture (MDA) is used as a guide, a Platform Independent Model (PIM) of a engineering training dynamic schematic diagram is designed, and a dynamic schematic diagram software module independent of an operation platform is researched and manufactured. According to the existing dynamic schematic diagram software specification, module resources capable of accurately and clearly displaying the principle of an airplane system are manufactured for each system of the navigation airplane, and the dynamic schematic diagram modules irrelevant to the platform form a unified general dynamic schematic diagram module library. In the later development process of the dynamic schematic diagram, the resources in the library are used to produce the schematic diagram of the specific airplane system in a 'building block' mode, and the continuity and the uniformity of the software in form and content are ensured.
The typical navigation aircraft system dynamic schematic diagram design method is a dynamic schematic diagram modularization assembly technology, takes a model driving architecture as guidance, designs a platform-independent model of a crew training dynamic schematic diagram, and researches and manufactures a platform-independent dynamic schematic diagram software module.
According to the design standard of the unified dynamic schematic diagram in the fifth step, module resources capable of accurately and clearly displaying the principle of the aircraft system are integrated aiming at each system of the aircraft, and the resource modules and the platform-independent dynamic schematic diagram module form a unified universal dynamic schematic diagram module library which comprises a data layer, a function presentation layer and a man-machine interaction layer required by the system. The GL Studio is used for developing various system schematic diagrams of the navigation airplane, the states of the system schematic diagrams are represented on a function presentation layer, a data communication pipeline running in an independent thread (or process) is built at the same time, data of a bottom data layer are obtained, and a user can carry out interactive operation on the system on an interaction layer.
According to the design method of the dynamic schematic diagram of the typical navigation aircraft system, a dynamic schematic diagram platform-independent model is developed by adopting GL Studio software, and the dynamic schematic diagram of the aircraft system is developed by utilizing the GL Studio software. GL Studio is a professional instrument simulation platform that is used as a platform-independent rapid prototyping tool to create real-time, three-dimensional, photo-level interactive graphical interfaces. The method can be connected with HLA/DIS simulation application, and the generated C + + and OpenGL source codes can be independently operated and can be embedded into other application programs, so that a large amount of complicated bottom-layer OpenGL development is avoided.
The design method of the dynamic schematic diagram of the typical navigation aircraft system adopts a cross-platform application compiling mode, software source codes manufactured by using a dynamic schematic diagram module library have platform-independent attributes, and are compiled into different formats aiming at different using platforms and then are issued to terminals such as a computer, a mobile phone, a tablet and the like.
In the description of the present invention, it is to be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on those shown in the drawings, and are used only for convenience in describing the present invention and for simplicity in description, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, are not to be construed as limiting the present invention. Further, in the description of the present invention, "a plurality" means two or more unless specifically defined otherwise.

Claims (6)

1. A method for designing a dynamic schematic diagram of a cross-platform interactive airplane system is characterized by comprising the following steps:
the method comprises the following steps: analyzing system requirements: specific analysis is made according to the training requirements of the navigation aircraft, and the system principle needing simulation is determined;
step two: and (3) formulating a scheme: according to the system requirement analysis in the first step, a development scheme is formulated, the expression form of the dynamic schematic diagram of each system is determined, the simulation program of each system component is determined, required materials are collected, and target software is determined;
step three: software development: developing a schematic diagram by combining commercial software GL Studio and related software and plug-ins;
step four: and (4) performance testing: testing personnel are required to test the performance of the schematic diagram;
step five: unified specification of dynamic schematic techniques: making a uniform universal technical specification on software content, UI display forms and aircraft system logic depth;
step six: applying and releasing by multiple terminals across platforms: the method adopts a cross-platform application compiling mode aiming at different use platforms.
2. The method for designing a dynamic schematic diagram of a cross-platform interactive aircraft system according to claim 1, wherein the software development in the third step adopts a dynamic schematic diagram modular assembly technology.
3. The method as claimed in claim 2, wherein the dynamic schematic diagram modular assembly technique is guided by a model-driven architecture to design a platform-independent model of the engineering training dynamic schematic diagram, and to study and manufacture a software module of the platform-independent dynamic schematic diagram.
4. The method according to claim 3, wherein module resources capable of accurately and clearly displaying the principle of the aircraft system are integrated for each system of the aircraft, and the resource modules and the platform-independent dynamic principle drawing module form a unified general dynamic principle drawing module library.
5. The method of claim 4, wherein the method comprises: the dynamic schematic diagram platform independent model is developed by GL Studio software.
6. The method of claim 1, wherein the method comprises: the cross-platform application compiling mode is characterized in that a software source code manufactured by using a dynamic schematic diagram module library has a platform-independent attribute and aims at different use platforms.
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CN101814024A (en) * 2009-10-23 2010-08-25 深圳创维-Rgb电子有限公司 Framework and tool for designing cross-platform 3D interface

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