CN110046455B - Aircraft design platform, aircraft design and software simulation system and method - Google Patents
Aircraft design platform, aircraft design and software simulation system and method Download PDFInfo
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- CN110046455B CN110046455B CN201910340325.7A CN201910340325A CN110046455B CN 110046455 B CN110046455 B CN 110046455B CN 201910340325 A CN201910340325 A CN 201910340325A CN 110046455 B CN110046455 B CN 110046455B
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- G06F30/10—Geometric CAD
- G06F30/15—Vehicle, aircraft or watercraft design
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- G06F30/00—Computer-aided design [CAD]
- G06F30/20—Design optimisation, verification or simulation
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- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
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Abstract
The invention discloses an aircraft design platform, an aircraft design and software simulation system and a method, wherein the system comprises the aircraft design platform, an aircraft simulation system and an aircraft steering control device; the aircraft design platform is used for designing an aircraft model and storing configuration data of the aircraft model; the aircraft simulation system is in data communication with the aircraft design platform and is used for receiving configuration data of an aircraft model of the aircraft design platform and providing a pilot flight scene for the aircraft model. The system and the method drive the aircraft through simulating the aircraft, do not have any safety risk, and can also hold various competitive games, propagate scientific innovation spirit and assist the propulsion of aviation science popularization education.
Description
Technical Field
The invention relates to the technical field of aircraft design and simulation, in particular to an aircraft design platform, an aircraft design and software simulation system and method.
Background
With the development of the aviation industry, aircrafts are known by ordinary people, but for designing and manufacturing aircrafts, known aircraft design software is used for designing professional real aircrafts, users are professional designers of aircraft manufacturers, ordinary people are difficult to touch, the threshold of the aircraft designer is very high, and the number of years, more decades, from development to trial run of an aircraft are short. The aviation science popularization education in the world is mostly to visit aircrafts, visit airports, learn simple flight driving, paper folding aircrafts and the like, and has no way to excite the innovative thinking and the practical ability of students.
Disclosure of Invention
Based on the defects of the prior art, the invention provides an aircraft design platform, an aircraft design and software simulation system and method, through the aircraft design platform, a user can create an aircraft model on a computer according to own ideas, through the aircraft design and software simulation system and method, the user can import data into a flight simulation system according to the aircraft data of the created aircraft model, and the user can drive the aircraft model to fly the created aircraft in the flight simulation system.
The technical scheme of the invention is as follows:
an aircraft design platform, characterized by: the system comprises an aircraft assembly database and a virtual aircraft assembly workshop, wherein the aircraft assembly database comprises data model information of various parts of an aircraft added with real aircraft performance, and the parts in the database comprise airframe structural parts with various shapes, aircraft main wings with various specifications, horizontal tail wings, vertical tail wings, various types of engines, motors, oil tanks, batteries, various landing gears, aircraft cabins and other part modules, and the performance parameters comprise unit volume and mass, provided lift coefficient, resistance coefficient and the like. The virtual aircraft assembly plant is configured to assemble a selected aircraft data model.
Further, the virtual aircraft assembly shop comprises an aircraft component collision detection module, an aircraft component automatic alignment module, and an aircraft geometry and performance data calculation module;
the aircraft component collision detection module is used for detecting the distance and the position relation of the aircraft component and adsorbing the component within a threshold range;
the automatic alignment module of the aircraft component is used for automatically adjusting the joint angle and alignment of the joint surface of the aircraft component;
the aircraft geometry and performance data calculation module is used for calculating the performance parameters of the aircraft components according to the positions and types of the models in the scene.
Further, a rendering module is included for selecting different colors to render for each component of the aircraft.
The system further comprises a data preview and check panel module, wherein the data preview and check panel module is used for displaying configuration parameters of the assembled aircraft model and determining whether the design requirements are met.
An aircraft design and software simulation system, characterized by: the system comprises an aircraft design platform, an aircraft simulation system and an aircraft steering control device;
the aircraft design platform is used for designing an aircraft model and storing configuration data of the aircraft model;
the aircraft simulation system is in data communication with the aircraft design platform and is used for receiving configuration data of an aircraft model of the aircraft design platform and providing a pilot flight scene for the aircraft model.
Further, the aircraft design platform comprises an aircraft assembly database and a virtual aircraft assembly workshop, wherein the aircraft assembly database comprises data model information of all parts of the aircraft added with real aircraft performance, and the virtual aircraft assembly workshop is used for assembling and configuring the selected aircraft data model;
the virtual aircraft assembly shop comprises an aircraft component collision detection module, an aircraft component automatic alignment module and an aircraft geometry and performance data calculation module;
the aircraft component collision detection module is used for detecting the distance and the position relation of the aircraft component and adsorbing the component within a threshold range; the automatic alignment module of the aircraft component is used for automatically adjusting the joint angle and alignment of the joint surface of the aircraft component;
the aircraft geometry and performance data calculation module is used for calculating the performance parameters of the aircraft components according to the positions and types of the models in the scene.
An aircraft design and software simulation method, the method comprising:
step 1, designing an aircraft model on an aircraft design platform, and storing configuration data of the aircraft model;
and 2, transmitting the configuration data of the aircraft model to an aircraft simulation system, analyzing the configuration data by the aircraft simulation system, and carrying out trial flight in a trial flight scene provided by the aircraft under the control of an aircraft driving control instruction.
Further, the method for designing an aircraft model on an aircraft design platform in step 1 includes:
step 11, establishing a database or a data file of each part of the aircraft model in a 3D game engine-based development environment;
step 12, selecting an aircraft model in an aircraft model database for assembly, and performing collision detection and automatic alignment on aircraft components in the assembly process to realize the adsorption of the aircraft model components, and realizing the angle adjustment of the splicing of the aircraft models through the automatic alignment of the models;
and step 13, saving the designed aircraft model data and transmitting the data to an aircraft simulation system.
Further, in step 12, the bonding surface obtained by adopting an adsorption algorithm in the automatic alignment of the model is used for automatically adjusting the splicing angle of the model.
Further, the performance parameters of the components are also derived by calculating the geometry and performance data of the aircraft during the assembly of the aircraft model in step 12.
The beneficial effects of the invention are as follows:
the aircraft design platform reduces the design threshold of contact aircraft such as aviation science popularization objects, aviation lovers, common people and the like, so that the common people can further know aviation and know aviation by designing flight; meanwhile, the cost of deep aviation science popularization education is greatly reduced, and the innovative thinking and creativity of a user can be stimulated; and combines an aircraft simulation system, and the aircraft is driven by simulating the aircraft, so that the aircraft has no safety risk, various competitive games can be held, the scientific innovation spirit is spread, and the propulsion of aviation science popularization education is assisted.
Drawings
FIG. 1 is a block diagram of an aircraft design and software simulation system of the present invention.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
The aircraft design platform of this embodiment is based on a three-dimensional scene editor, can use 3D game engine to develop, and the scene effect can accomplish lifelike, beautiful. The system comprises an aircraft component database, a virtual aircraft assembly workshop and a display module, and further comprises a test flight interface, wherein the aircraft component database comprises data model information of all parts of the aircraft with real aircraft performance, the data model information can be displayed on a menu bar of the display module and can be dragged for selection, and the virtual aircraft assembly workshop is used for assembling and configuring the selected aircraft data model and can display the assembly effect on the display module. The aircraft assembly database provides all component modules required for aircraft assembly, including components such as fuselage structural parts in various shapes, aircraft main wings in various specifications, horizontal tails, vertical tails, various types of engines, motors, oil tanks, batteries, various landing gears, aircraft cabins and the like, and corresponding options are provided in menu bars of display panels of the display modules, and all components are added with performance attributes such as unit volume and mass, lift coefficient, drag coefficient and the like according to the standards of real aircraft. The components in the aircraft component database can be designed by using three-dimensional modeling software such as 3DMax, the size proportion of the model is consistent with that of a real aircraft, and the performance data design can be based on the average value of the performance data of several typical real aircraft. The data of the aircraft model in the flight assembly database is stored in a database or data file in a tree structure.
The virtual aircraft assembly shop comprises an aircraft component collision detection module, an aircraft component automatic alignment module and an aircraft geometry and performance data calculation module.
The aircraft component collision detection module is used for detecting the distance and the position relation of the aircraft component and adsorbing the component within a threshold range.
The automatic alignment module of the aircraft component is used for automatically adjusting the joint angle and alignment of the joint surface of the aircraft component.
The aircraft geometry and performance data calculation module is used for calculating and adjusting performance parameters of the assembled aircraft parts according to the positions and types of the models in the scene.
The user can drag, assemble and adjust each part of the aircraft by using input equipment such as a mouse and a keyboard in the menu bar, and the parts are automatically adsorbed, aligned and spliced by the aircraft part collision detection module and the aircraft part automatic alignment module in the assembling process; parameters such as the size, the gravity center and the weight of the aircraft can be calculated through the geometry and the performance of the aircraft, for example, the wing span of the aircraft is obtained by calculating the tip distances of two wings of the aircraft, the weight of the aircraft is the sum of the weights of all components, the gravity center is calculated according to the weight distribution proportion and the like, and whether the aspects such as mass balance, lifting resistance and power matching of the designed aircraft meet design requirements can be checked through a data preview and check panel in the assembly process.
The aircraft design platform further comprises a rendering module, wherein the rendering module is used for selecting different colors for each component of the aircraft, a rendering window capable of selecting multiple colors is formed in a display panel of the display module by the rendering module, and different colors can be rendered for different components of the aircraft by clicking the selected rendering colors after the components are selected.
The aircraft design platform further comprises a data preview and inspection panel module for displaying configuration parameters of the assembled aircraft model to determine whether design requirements are met. The data preview and check panel displays a floating window on the display module panel, and parameters of the aircraft model configuration are displayed in the floating window, wherein the parameters comprise the specifications of the structural parts of the aircraft body, the model of the engine, the performance indexes of each part and the engine, and the like.
The aircraft design platform further comprises a VR equipment calling module, and the VR equipment calling module is connected with VR equipment through calling and a computer interface, so that the aircraft design assembly can be assembled and displayed in a three-dimensional mode under mouse dragging and assembling and visual VR equipment environments.
As shown in fig. 1, an aircraft design and software simulation system includes an aircraft design platform, an aircraft simulation system, an aircraft pilot control device, and a network system;
the aircraft design platform is used for designing an aircraft model in a three-dimensional visual environment and storing configuration data of the aircraft model; the aircraft design platform adopts the aircraft design platform disclosed in the embodiment.
The aircraft simulation system is in data communication with the aircraft design platform through network equipment and is used for receiving configuration data of an aircraft model of the aircraft design platform and providing a test flight scene for the aircraft model, the aircraft simulation system is in communication connection with the aircraft design platform through the Ethernet, and in addition, the aircraft simulation system is also used for receiving an operation command of the aircraft steering operation equipment and realizing test flight under the control of the operation command. A user can control surfaces such as an elevator, an aileron, a rudder and the like of the aircraft through a flight control lever device, and can control thrust of an engine through an accelerator lever.
The aircraft simulation system can be built by adopting Simlink, is rapid and convenient to debug, can also adopt a simulation system of a common aircraft, and comprises an aerodynamic module and an engine module, wherein the aerodynamic module calculates the attitude angle and the acceleration of the aircraft in real time according to aerodynamic parameters and displays the attitude angle and the acceleration through a real-time data display module, the engine module is used for calculating the real-time thrust and the fuel consumption of the aircraft according to an engine driving gear input by an aircraft steering device, the longitude and latitude coordinates of the aircraft are sent to the real-time data display module to display data, and meanwhile, the vision module acquires the flight attitude data of the aircraft in real time and displays a flight scene in real time in a scene according to the view angle of an aircraft cabin.
The adopted aircraft simulation system also comprises a sound simulation module, and the sound simulation module generates and plays different sound effects according to different states of the aircraft.
A method of aircraft design and software simulation, the method comprising:
step 1, designing an aircraft model on an aircraft design platform, and storing configuration data of the aircraft model;
and 2, transmitting the configuration data of the aircraft model to an aircraft simulation system, analyzing the configuration data by the aircraft simulation system, and carrying out trial flight in a trial flight scene provided by the aircraft under the control of an aircraft driving control instruction.
The method for designing the aircraft model on the aircraft design platform in the step 1 comprises the following steps:
step 11, establishing a database or a data file of each part of the aircraft model in a 3D game engine-based development environment;
step 12, selecting an aircraft model in an aircraft model database for assembly, and performing collision detection and automatic alignment on aircraft components in the assembly process to realize the adsorption of the aircraft model components, and realizing the angle adjustment of the splicing of the aircraft models through the automatic alignment of the models;
and step 13, saving the designed aircraft model data and transmitting the data to an aircraft simulation system.
And 12, automatically adjusting the splicing angle of the model by adopting an attaching surface obtained by an adsorption algorithm in the automatic alignment of the model.
The performance parameters of the various components are also derived by calculating the geometry and performance data of the aircraft during the assembly of the aircraft model in step 12. The method specifically comprises the steps of calculating the length of an airplane, the widening of wings, the chord length of wings, the weight of an aircraft, the gravity center position, the engine thrust gravity center position and the aerodynamic gravity center position according to the position and the type of a model in a scene.
According to the embodiment, an aircraft design platform is used for designing an aircraft model, data of the aircraft model are stored, the stored basic data of the aircraft model are transmitted to an aircraft simulation system through a network system, the aircraft simulation system configures the basic data to generate simulation basic parameters of the aircraft simulation system, the aircraft simulation system realizes simulation flight under the control of an aircraft steering device, and the simulation effect is experienced in a vision module to give real test flight experience to people.
The invention reduces the design threshold of contact aircrafts of aviation science popularization objects, aviation lovers, common people and the like, and enables the common people to know aviation deeply by designing flying so as to know aviation. Greatly reduces the cost of deep aviation science popularization education and can excite the innovative thinking and creativity of users. Piloting the aircraft by simulating the aircraft without any safety risks; meanwhile, a user can not only reform the aircraft designed by the user, but also share the created aircraft with other people in the forms of an online network, a storage medium and the like; by using the invention, various competitive games can be held, the scientific innovation spirit is spread, and the promotion of aviation science popularization education is assisted.
Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (4)
1. An aircraft design platform, characterized by: the system comprises an aircraft assembly database, a virtual aircraft assembly workshop and a display module, wherein the aircraft assembly database comprises data model information of all parts of an aircraft added with real aircraft performance, and the virtual aircraft assembly workshop is used for assembling and configuring a selected aircraft data model; the data model information of each part of the aircraft is displayed in a menu bar of the display module and is used for dragging and selecting;
wherein the aircraft component database provides all component modules required for aircraft assembly, all of which are attached with performance attributes according to the standards of a real aircraft; all the component modules are provided with corresponding options in a menu bar of a display panel of the display module;
the virtual aircraft assembly shop comprises an aircraft component collision detection module, an aircraft component automatic alignment module and an aircraft geometry and performance data calculation module;
the aircraft component collision detection module is used for detecting the distance and the position relation of the aircraft component and adsorbing the component within a threshold range;
the automatic alignment module of the aircraft component is used for automatically adjusting the joint angle and alignment of the joint surface of the aircraft component;
the aircraft geometry and performance data calculation module is used for calculating performance parameters of all parts of the aircraft according to the positions and types of the models in the scene;
the aircraft design platform further comprises a data preview and inspection panel module, wherein the data preview and inspection panel module is used for displaying configuration parameters of the assembled aircraft model and determining whether the design requirements are met.
2. The aircraft design platform of claim 1, wherein: the system further comprises a rendering module for selecting different colors for each component of the aircraft.
3. An aircraft design and software simulation system, characterized by: the system comprises an aircraft design platform, an aircraft simulation system and aircraft piloting control equipment;
the aircraft design platform is used for designing an aircraft model and storing configuration data of the aircraft model;
the aircraft simulation system is in data communication with the aircraft design platform and is used for receiving configuration data of an aircraft model of the aircraft design platform and providing a test flight scene for the aircraft model;
the aircraft design platform comprises an aircraft assembly database and a virtual aircraft assembly workshop, wherein the aircraft assembly database comprises data model information of all parts of the aircraft added with real aircraft performance, and the virtual aircraft assembly workshop is used for assembling and configuring the selected aircraft data model;
the virtual aircraft assembly shop comprises an aircraft component collision detection module, an aircraft component automatic alignment module and an aircraft geometry and performance data calculation module;
the aircraft component collision detection module is used for detecting the distance and the position relation of the aircraft component and adsorbing the component within a threshold range; the automatic alignment module of the aircraft component is used for automatically adjusting the joint angle and alignment of the joint surface of the aircraft component;
the aircraft geometry and performance data calculation module is used for calculating performance parameters of the aircraft parts according to the positions and types of the models in the scene;
the aircraft assembly database provides all component modules required for aircraft assembly, and all component modules are added with performance attributes according to the standard of a real aircraft;
the aircraft design platform further comprises a data preview and inspection panel module, wherein the data preview and inspection panel module is used for displaying configuration parameters of the assembled aircraft model and determining whether the design requirements are met.
4. An aircraft design and software simulation method, the method comprising:
step 1, designing an aircraft model on an aircraft design platform, and storing configuration data of the aircraft model;
step 2, transmitting configuration data of the aircraft model to an aircraft simulation system, analyzing the configuration data by the aircraft simulation system, and under the control of an aircraft driving control instruction, performing trial flight in a trial flight scene provided by an aircraft;
the method for designing the aircraft model on the aircraft design platform in the step 1 comprises the following steps:
step 11, establishing a database or a data file of each part of the aircraft model in a 3D game engine-based development environment;
step 12, selecting an aircraft model in an aircraft model database for assembly, and performing collision detection and automatic alignment on aircraft components in the assembly process to realize the adsorption of the aircraft model components, and realizing the angle adjustment of the splicing of the aircraft models through the automatic alignment of the models;
step 13, saving the designed aircraft model data and transmitting the data to an aircraft simulation system;
in the step 12, the model is automatically aligned with the joint surface obtained by adopting an adsorption algorithm, and the splicing angle of the model is automatically adjusted;
the performance and parameters of the aircraft are also calculated by calculating the geometry and performance data of the aircraft during the process of assembling the aircraft model in step 12.
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| CN112150886A (en) * | 2020-09-22 | 2020-12-29 | 中国商用飞机有限责任公司 | Method for evaluating validity of data package test flight data of flight simulator |
| CN114516427B (en) * | 2022-02-08 | 2024-05-14 | 上海斯化露航空科技发展有限公司 | Simulation system and method for aircraft cabin door design detection |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101398860A (en) * | 2007-09-25 | 2009-04-01 | 北京航空航天大学 | Cooperating design method of aircraft control system in different areas based on PDM//matlab |
| CN105488251A (en) * | 2015-11-13 | 2016-04-13 | 中国人民解放军国防科学技术大学 | Distributed aircraft simulation platform and implementation method thereof |
| CN106202669A (en) * | 2016-06-30 | 2016-12-07 | 北京航空航天大学 | A kind of intellectualized battle flight simulation device |
-
2019
- 2019-04-25 CN CN201910340325.7A patent/CN110046455B/en active Active
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101398860A (en) * | 2007-09-25 | 2009-04-01 | 北京航空航天大学 | Cooperating design method of aircraft control system in different areas based on PDM//matlab |
| CN105488251A (en) * | 2015-11-13 | 2016-04-13 | 中国人民解放军国防科学技术大学 | Distributed aircraft simulation platform and implementation method thereof |
| CN106202669A (en) * | 2016-06-30 | 2016-12-07 | 北京航空航天大学 | A kind of intellectualized battle flight simulation device |
Non-Patent Citations (3)
| Title |
|---|
| 张文苑.飞行器动力学虚拟样机模型库的研究.《计算机仿真》.2004,第32-35页. * |
| 航天器协同设计平台总体框架设计;胡庆军;《计算机工程与科学》;20070228;第129-131页 * |
| 飞行器动力学虚拟样机模型库的研究;张文苑;《计算机仿真》;20040531;第32-35页 * |
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