Agile design method and system for display control interface
By combining manual design and intelligent design of large models, the aircraft display and control interface is quickly generated and optimized, and the problems of long design cycles and difficult to quickly adjust in the existing technology are solved, and efficient interface design and development are achieved.
Patent Information
- Application Number
- CN202411533874.3
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-10-30
- Publication Date
- 2025-02-18
AI Technical Summary
The existing aircraft display and control systems have a long design cycle, are expensive, and rely on the established hardware platform and software architecture, making it difficult to quickly adjust according to new flight missions or environments.
Using a method of combining manual design with intelligent large model design, the aircraft display and control interface files are quickly generated through natural language input, and combined with manual design, fine-tuning and data block binding are performed to quickly complete the design and construction of the display and control interface.
It realizes rapid iteration and diversity of aircraft display and control interface design, improves design and development efficiency, and promotes the development of ergonomic evaluation.
Smart Images
Figure CN119473229A_ABST
Abstract
Description
Technical Field
[0001] The present invention relates to the technical field of aircraft display and control interface design and ergonomics evaluation, and in particular to an agile design method and system for a display and control interface. Background Art
[0002] As the human-machine interface, the aircraft's display and control system is central to efficient aircraft operation. With the rapid advancement of aviation technology, the rapid and rational design of digital interactive interfaces for aircraft has become a crucial approach to improving pilot efficiency and reducing their workload. Consequently, the design and optimization of aircraft display and control systems has garnered significant research attention. Currently, aircraft display and control systems have evolved from traditional physical human-machine interfaces based on mechanical displays to digital interfaces based on electronic displays and digital screens. This has enhanced system stability and reliability, providing pilots with greater operational convenience and safety.
[0003] In reality, aircraft often face complex environments and diverse tasks during mission execution. However, existing aircraft display and control system designs often rely on established hardware platforms and software architectures. These relatively rigid architectures are difficult to flexibly adjust to new flight missions or environments. Summary of the Invention
[0004] The purpose of this invention is to address the shortcomings of the existing technology, such as: the design cycle of existing aircraft display and control systems is long, the cost is high, and they rely heavily on established hardware platforms and software architectures. The architecture is relatively fixed and difficult to quickly adjust to new flight missions or environments.
[0005] In order to achieve the above-mentioned objectives, the present invention provides the following technical solutions: an agile design method and system for a display and control interface, the method comprising: rapidly iterating the design of an aircraft display and control interface by combining manual design and large-model intelligent design, using the model to intelligently generate display and control interface files, test users can rapidly generate aircraft display and control interface files through natural language input, import them into the display and control interface agile design system to rapidly generate the aircraft display and control interface, and then fine-tune and bind data blocks in combination with manual design, thereby rapidly completing the design and construction of the aircraft display and control interface, publishing it to the aircraft display and control terminal device through the display and control interface agile design system, and testing, verification and ergonomic evaluation through interaction with external flight simulation data.
[0006] As a preferred solution of the present invention, the intelligent design implementation steps include: S11, setting a component information knowledge base, wherein the control information knowledge base includes an electronic blackboard of component information; S12. Set design requirements for each aircraft system, including flight performance display, flight path planning, flight parameter monitoring, and emergency response; S13. Input the aircraft interface design requirements described in S12 into the localized large model for understanding and learning. The model can work offline and has memory, and can realize functions such as language understanding, knowledge sorting, and code generation; S14: The model interactively learns and generates an aircraft display and control interface file that best meets the pilot's needs. The user can transmit their needs to the localized large model through manual and voice input; S15. Importing the aircraft display and control interface file described in S14 into the system, the system visualizes the data in the file as corresponding component information and displays it in real time on the editing panel, allowing the user to manually adjust and optimize. S16. Manually optimize the interface, create and edit sub-panels, select and add components in the component list, adjust component properties and delete components, etc. S17. Create multiple communication data sources and select data variables in the data sources and bind them to the input and output interfaces of the corresponding components; S18, simulation data test verification, based on the binding relationship between the component and the data block of the communication data source and the data identifier of the target data block, determine the corresponding target data from the data source, interact with the corresponding component, and realize the drive display and instruction issuance; S19. Publishing the designed aircraft display and control interface as an executable file corresponding to the aircraft display and control terminal platform.
[0007] The beneficial effects of the present invention are: The present invention provides an agile design method and system for a display and control interface. Compared with traditional design systems, this system uses a large-model intelligent design method to quickly iterate the design of an aircraft display and control interface, and can transfer the design work of the aircraft display and control interface from the development level to the test user level. The test user can quickly generate an aircraft display and control interface through natural language input, and then fine-tune it and bind data blocks in combination with manual design, so as to quickly complete the design and construction of the aircraft display and control interface. It is published to the aircraft display and control terminal device through the display and control interface agile design system, and the aircraft display and control test and ergonomic evaluation are carried out in combination with flight simulation data. The interface configuration data and the result data of the ergonomic evaluation are used to train the intelligent model, and the understanding and design capabilities of the intelligent model are continuously optimized, thereby greatly improving the efficiency of the design and development of the aircraft display and control interface, enriching the diversity of the aircraft display and control interface design, and promoting the development of its ergonomic evaluation. BRIEF DESCRIPTION OF THE DRAWINGS
[0008] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the following briefly introduces the drawings required for use in the embodiments. Obviously, the drawings described below are only some embodiments described in the present invention. For ordinary technicians in this field, other drawings can also be obtained based on these drawings.
[0009] Figure 1 A diagram of the method steps provided by an embodiment of the present invention.
[0010] Figure 2 A system block diagram provided for an embodiment of the present invention. DETAILED DESCRIPTION
[0011] The following will be combined with the accompanying drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. However, the exemplary embodiments can be embodied in different forms and should not be construed as limited to the embodiments described herein. On the contrary, the purpose of providing these embodiments is to make this disclosure thorough and complete and to enable those skilled in the art to fully understand the scope of this disclosure.
[0012] In the absence of conflict, the various embodiments of the present disclosure and the various features therein may be combined with each other.
[0013] As used herein, the term "and / or" includes any and all combinations of one or more of the associated listed items.
[0014] The terms used herein are used only to describe specific embodiments and are not intended to limit the present disclosure. As used herein, the singular forms "a," "an," and "the" are also intended to include the plural forms, unless the context clearly indicates otherwise. It will also be understood that when the terms "comprising" and / or "made of" are used in this specification, the presence of the features, wholes, steps, operations, elements, and / or components is specified, but the presence or addition of one or more other features, wholes, steps, operations, elements, components, and / or groups thereof is not excluded.
[0015] The embodiments described herein may be described with reference to plan views and / or cross-sectional views, with the aid of idealized schematic diagrams of the present disclosure. Thus, the example illustrations may be modified based on manufacturing techniques and / or tolerances. Therefore, the embodiments are not limited to the embodiments shown in the accompanying drawings, but include modifications of the configurations formed based on the manufacturing process. Therefore, the regions illustrated in the accompanying drawings are schematic in nature, and the shapes of the regions shown in the drawings illustrate specific shapes of the regions of the elements, but are not intended to be limiting.
[0016] Unless otherwise defined, all terms (including technical and scientific terms) used herein have the same meaning as commonly understood by one of ordinary skill in the art. It will also be understood that terms such as those defined in commonly used dictionaries should be interpreted as having a meaning consistent with their meaning in the context of the relevant art and the present disclosure, and will not be interpreted as having an idealized or overly formal meaning unless expressly defined as such herein.
[0017] See also Figure 1 In this embodiment, the manual design implementation includes the following steps: S11, setting a component information knowledge base, wherein the control information knowledge base includes an electronic blackboard of component information; S12. Set design requirements for each aircraft system, including flight performance display, flight path planning, flight parameter monitoring, and emergency response; S13. Input the aircraft interface design requirements described in S12 into the localized large model for understanding and learning. The model can work offline and has memory, and can realize functions such as language understanding, knowledge sorting, and code generation; S14: The model interactively learns and generates an aircraft display and control interface file that best meets the pilot's needs. The user can transmit their needs to the localized large model through manual and voice input; S15. Importing the aircraft display and control interface file described in S14 into the system, the system visualizes the data in the file as corresponding component information and displays it in real time on the editing panel, allowing the user to manually adjust and optimize. S16. Manually optimize the interface, create and edit sub-panels, select and add components in the component list, adjust component properties and delete components, etc. S17. Create multiple communication data sources and select data variables in the data sources to bind and map to the input and output interfaces of the corresponding components; S18, simulation data test verification, based on the binding relationship between the component and the data block of the communication data source and the data identifier of the target data block, determine the corresponding target data from the data source, interact with the corresponding component, and realize the drive display and instruction issuance; S19. Publishing the designed aircraft display and control interface as an executable file corresponding to the aircraft display and control terminal platform.
[0018] Further explanation of the technical solution implemented by this system, please refer to the following Figure 2, a display and control interface agile design method and system, the method includes: quickly iterating the design of the aircraft display and control interface through a combination of manual design and large-scale intelligent design. Intelligent design uses the model to intelligently generate the display and control interface file, which is imported into the display and control interface agile design system to quickly generate the aircraft display and control interface. The system can read the component positioning, size and other information of the display and control interface file component layout; and display the relative screen position, color and other properties of each component. Combined with manual design, the user can manually adjust the component layout, add and delete components, adjust component properties and data block binding through the display and control interface agile design system.
[0019] When in use, the present invention can quickly construct an aircraft display and control interface. The test user can quickly generate the aircraft display and control interface by natural language input, and then fine-tune it and bind data blocks in combination with manual design, so as to quickly complete the design and construction of the aircraft display and control interface, and publish it to the aircraft display and control terminal device through the display and control interface agile design system. The aircraft display and control test and ergonomic evaluation are carried out in combination with flight simulation data. The result data of the test and ergonomic evaluation are used to train the intelligent model, and the understanding and design capabilities of the intelligent model are continuously optimized, thereby greatly improving the efficiency of the design and development of the aircraft display and control interface, and enriching the diversity of the aircraft display and control interface design, and promoting the development of its ergonomic evaluation.
[0020] The above description is only a preferred specific embodiment of the present invention, but the scope of protection of the present invention is not limited thereto. Any technician familiar with the technical field, within the technical scope disclosed by the present invention, who makes equivalent replacements or changes based on the technical solution and application concept of the present invention, should be covered by the scope of protection of the present invention.
Claims
1. A display and control interface agile design method and system includes large model intelligent design and manual design, characterized in that: The design of the aircraft display and control interface is quickly iterated through the intelligent design of a large model. The model is a localized artificial intelligence model that can realize functions such as language understanding and knowledge combing. It is then combined with manual design to fine-tune it and bind data blocks, so as to quickly complete the design and construction of the aircraft display and control interface. The test user can quickly generate the aircraft display and control interface file through natural language input, which includes text input and voice input. The text input method is mainly carried out through devices such as keyboards, and natural language commands are input by tapping letters, numbers or symbols on the keyboard. The voice input method is mainly completed through audio collection devices such as microphones, and the interface design requirements are input into the system in the form of voice. The system can realize the parsing and status display of the display and control interface file component layout. The reading of the display and control interface file component layout includes information such as component positioning and size; the status display is used to realize the display of the relative screen position, color and other properties of each component, and the manual design is used to realize fine-tuning and data block binding; thus, the design and construction of the aircraft display and control interface are quickly completed and published to the corresponding aircraft display and control terminal through the display and control interface agile design system; The method tests and evaluates ergonomics by interacting with external flight simulation data. The interface configuration data and the result data of the ergonomics evaluation are used to train the intelligent model, continuously optimizing the understanding and design capabilities of the intelligent model. The interface configuration data is an interface file generated by the large model, including information data such as component type, attributes and positioning.
2. The method and system for agile design of a display and control interface according to claim 1, characterized in that: The implementation steps of the intelligent design include: S11, setting a component information knowledge base, wherein the component information knowledge base includes an electronic blackboard of component information; S12. Set the design requirements for each aircraft system, including flight performance display, flight path planning, flight parameter monitoring and emergency handling; S13, inputting the aircraft interface design requirements described in S12 into the localized large model for understanding and learning. The model can work offline and has memory, and can realize functions such as language understanding, knowledge combing and code generation; S14, the model interactively learns and generates the aircraft display and control interface file that best meets the input requirements. Users can transmit their requirements to the localized large model through manual input and voice input; S15, importing the aircraft display and control interface file described in S14 into the system, the system visualizes the data in the file as corresponding component information and displays it in real time on the editing panel, and the user can manually adjust and optimize; S16. Manually optimize the interface, create and edit sub-panels, select and add components in the component list, adjust component properties and delete components, etc.; S17, create multiple communication data sources, and select data variables in the data sources and bind them to the input and output interfaces of the corresponding components; S18, simulation data test verification, according to the binding relationship between the component and the data block of the communication data source and the data identifier of the target data block, determine the corresponding target data from the data source, interact with the corresponding component, and realize the drive display and instruction issuance; S19. Publishing the designed aircraft display and control interface as an executable file corresponding to the aircraft display and control terminal platform.
3. The method and system for agile design of a display and control interface according to claim 2, characterized in that: The components are graphic interface elements used to implement various display and control functions, including switch buttons, instrument panels, and graphic display areas, etc., which are used to provide the pilot with necessary flight information, system status indications and operational control means.
4. The method and system for agile design of a display and control interface according to claim 2, characterized in that: The manual adjustment and optimization manually adjusts the component layout, adds and deletes components, and adjusts component properties and data block binding through the display and control interface agile design system.
5. The method and system for agile design of a display and control interface according to claim 1, characterized in that: The ergonomics evaluation is to evaluate the design effect, operating efficiency, user satisfaction and safety performance of the aircraft display and control interface. Furthermore, the interface configuration data and the result data of the ergonomics evaluation are used to train the intelligent model to continuously optimize the understanding and design capabilities of the intelligent model.