CN104462669A - Flight simulation system - Google Patents
Flight simulation system Download PDFInfo
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- CN104462669A CN104462669A CN201410679078.0A CN201410679078A CN104462669A CN 104462669 A CN104462669 A CN 104462669A CN 201410679078 A CN201410679078 A CN 201410679078A CN 104462669 A CN104462669 A CN 104462669A
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Abstract
The invention discloses a flight simulation system. The flight simulation system comprises an information input unit, a converting unit, a first processing unit, a second processing unit and a display unit, wherein the information input unit is used for inputting analogue simulation information, the converting unit is used for converting the analogue simulation information into data information, the first processing unit is used for performing analogue simulation processing based on the data information and generating track information and parameter information, the second processing unit is used for generating image information based on the track information and parameter information, and the display unit is used for playing and displaying the image information. The flight simulation system has the advantages that the simulation effect is good, data reliability is high and accidents do not easily occur.
Description
Technical field
The present invention relates to aerial vehicle simulation modeling effort field, particularly relate to a kind of flight Simulation System.
Background technology
Aircraft all needs to carry out simulated experiment before flight, and guarantee flight safety, and simulation system analog simulation effect of the prior art is poor, data reliability is lower, easily causes accident to occur.
In sum, present inventor, in the process realizing invention technical scheme in the embodiment of the present application, finds that above-mentioned technology at least exists following technical matters:
In the prior art, it is poor to there is simulated effect in existing simulation system simulation, and data reliability is lower, easily causes the technical matters that accident occurs.
Summary of the invention
The invention provides a kind of flight Simulation System, solving the simulation of existing simulation system, to there is simulated effect poor, data reliability is lower, easily cause the technical matters that accident occurs, achieve flight Simulation System simulated effect better, data reliability is higher, is not easy the technique effect occurring accident.
For solving the problems of the technologies described above, the embodiment of the present application provides a kind of flight Simulation System, and described system comprises:
Information input unit, described information input unit is for inputting analogue simulation information;
Converting unit, described converting unit is used for changing described analogue simulation information, is converted to data message;
First processing unit, described first processing unit carries out analogue simulation process based on described data message, and generates trace information, parameter information;
Second processing unit, described second processing unit is used for based on described trace information, described parameter information synthetic image information;
Display unit, described display unit is used for described image information being carried out broadcasting display.
Wherein, described analogue simulation information specifically comprises: flight equipment information, geographical location information, fuel information, temperature information.
Wherein, described first processing unit carries out analogue simulation process based on described data message and is specially:
Detect based on described data message, if the data of noting abnormalities, point out; If data without exception, carry out data-driven process;
After described data-driven process completes, carrying out calculation process according to the first preset rules to driving the data after processing, generating described trace information, described parameter information.
Wherein, described system also comprises track record unit, and described track record unit is used for carrying out record to the transportation of system and result, and carries out record to the running orbit generated, and stores in the memory unit.
Wherein, described system also comprises space tracking generation unit, and described space tracking generation unit is used for based on geographical spatial data and track service data span track data, and based on described space trajectory data span running orbit.
Wherein, described system also comprises parameter evaluation unit, described parameter evaluation unit is used for generating desired guiding trajectory range of information and parameter information scope based on the analogue simulation information of user's input, and the described trace information described desired guiding trajectory range of information and parameter information scope and the first processing unit generated and described parameter information compare, obtain comparison range degree, generate parameter evaluation index based on described comparison range degree.
The one or more technical schemes provided in the embodiment of the present application, at least have following technique effect or advantage:
Flight Simulation System be designed to comprise owing to have employed: information input unit, described information input unit is for inputting analogue simulation information; Converting unit, described converting unit is used for changing described analogue simulation information, is converted to data message; First processing unit, described first processing unit carries out analogue simulation process based on described data message, and generates trace information, parameter information; Second processing unit, described second processing unit is used for based on described trace information, described parameter information synthetic image information; Display unit, described display unit is used for the technical scheme carrying out described image information to play display, so, efficiently solving the simulation of existing simulation system, to there is simulated effect poor, data reliability is lower, easily causes the technical matters that accident occurs, and then it is better to achieve flight Simulation System simulated effect, data reliability is higher, is not easy the technique effect occurring accident.
Accompanying drawing explanation
Fig. 1 is the schematic diagram of flight Simulation System in the embodiment of the present application one;
Wherein, 1-information input unit, 2-converting unit, 3-first processing unit, 4-second processing unit, 5-display unit.
Embodiment
The invention provides a kind of flight Simulation System, solving the simulation of existing simulation system, to there is simulated effect poor, data reliability is lower, easily cause the technical matters that accident occurs, achieve flight Simulation System simulated effect better, data reliability is higher, is not easy the technique effect occurring accident.
Technical scheme during the application implements is for solving the problems of the technologies described above.General thought is as follows:
Have employed and flight Simulation System be designed to comprise: information input unit, described information input unit is for inputting analogue simulation information; Converting unit, described converting unit is used for changing described analogue simulation information, is converted to data message; First processing unit, described first processing unit carries out analogue simulation process based on described data message, and generates trace information, parameter information; Second processing unit, described second processing unit is used for based on described trace information, described parameter information synthetic image information; Display unit, described display unit is used for the technical scheme carrying out described image information to play display, so, efficiently solving the simulation of existing simulation system, to there is simulated effect poor, data reliability is lower, easily causes the technical matters that accident occurs, and then it is better to achieve flight Simulation System simulated effect, data reliability is higher, is not easy the technique effect occurring accident.
In order to better understand technique scheme, below in conjunction with Figure of description and concrete embodiment, technique scheme is described in detail.
Embodiment one:
In embodiment one, provide a kind of flight Simulation System, please refer to Fig. 1, described system comprises:
Information input unit 1, described information input unit 1 is for inputting analogue simulation information;
Converting unit 2, described converting unit 2, for changing described analogue simulation information, is converted to data message;
First processing unit 3, described first processing unit 3 carries out analogue simulation process based on described data message, and generates trace information, parameter information;
Second processing unit 4, described second processing unit 4 is for based on described trace information, described parameter information synthetic image information;
Display unit 5, described display unit 5 is for carrying out broadcasting display by described image information.
Wherein, in the embodiment of the present application, described analogue simulation information specifically comprises: flight equipment information, geographical location information, fuel information, temperature information.
Wherein, in the embodiment of the present application, described first processing unit carries out analogue simulation process based on described data message and is specially:
Detect based on described data message, if the data of noting abnormalities, point out; If data without exception, carry out data-driven process;
After described data-driven process completes, carrying out calculation process according to the first preset rules to driving the data after processing, generating described trace information, described parameter information.
Wherein, in the embodiment of the present application, described system also comprises track record unit, and described track record unit is used for carrying out record to the transportation of system and result, and carries out record to the running orbit generated, and stores in the memory unit.
Wherein, in the embodiment of the present application, described system also comprises space tracking generation unit, and described space tracking generation unit is used for based on geographical spatial data and track service data span track data, and based on described space trajectory data span running orbit.
Wherein, in the embodiment of the present application, described system also comprises parameter evaluation unit, described parameter evaluation unit is used for generating desired guiding trajectory range of information and parameter information scope based on the analogue simulation information of user's input, and the described trace information described desired guiding trajectory range of information and parameter information scope and the first processing unit generated and described parameter information compare, obtain comparison range degree, generate parameter evaluation index based on described comparison range degree.
Wherein, in actual applications, system in the embodiment of the present application can carry out the display of earth three-dimensional view angle picture by adjustment viewing angle, the effect of three-dimensional flight path band flight profile, mission profile can be shown in real time, can be real-time according to latitude and longitude coordinates on two-dimensional map, show flight path exactly, flight path can be shown on the map of space, the prediction locus of track and short time under asterism, star can be illustrated quick, star storehouse, the sun, the moon, astronomical, air weather data, aircraft planimetric map can be illustrated, rudder face, RCS sprays, undercarriage etc., can key parameter, comprise the time, longitude and latitude, phase identification malfunction, aircraft temperature can be shown, speed, highly, air pressure, rudder face, residual fuel amount, injection situation etc., heat flow can press through a year display such as image such as grade, prediction voyage-energy trace, can landing period lateral deviation apart from display, front yaw rudder curve display, brake pressure shows in real time, all Data logger grids can be got off, and provide playback to carry out off-line analysis to parameters.
Technical scheme in above-mentioned the embodiment of the present application, at least has following technique effect or advantage:
Flight Simulation System be designed to comprise owing to have employed: information input unit, described information input unit is for inputting analogue simulation information; Converting unit, described converting unit is used for changing described analogue simulation information, is converted to data message; First processing unit, described first processing unit carries out analogue simulation process based on described data message, and generates trace information, parameter information; Second processing unit, described second processing unit is used for based on described trace information, described parameter information synthetic image information; Display unit, described display unit is used for the technical scheme carrying out described image information to play display, so, efficiently solving the simulation of existing simulation system, to there is simulated effect poor, data reliability is lower, easily causes the technical matters that accident occurs, and then it is better to achieve flight Simulation System simulated effect, data reliability is higher, is not easy the technique effect occurring accident.
Although describe the preferred embodiments of the present invention, those skilled in the art once obtain the basic creative concept of cicada, then can make other change and amendment to these embodiments.So claims are intended to be interpreted as comprising preferred embodiment and falling into all changes and the amendment of the scope of the invention.
Obviously, those skilled in the art can carry out various change and modification to the present invention and not depart from the spirit and scope of the present invention.Like this, if these amendments of the present invention and modification belong within the scope of the claims in the present invention and equivalent technologies thereof, then the present invention is also intended to comprise these change and modification.
Claims (6)
1. a flight Simulation System, is characterized in that, described system comprises:
Information input unit, described information input unit is for inputting analogue simulation information;
Converting unit, described converting unit is used for changing described analogue simulation information, is converted to data message;
First processing unit, described first processing unit carries out analogue simulation process based on described data message, and generates trace information, parameter information;
Second processing unit, described second processing unit is used for based on described trace information, described parameter information synthetic image information;
Display unit, described display unit is used for described image information being carried out broadcasting display.
2. system according to claim 1, is characterized in that, described analogue simulation information specifically comprises: flight equipment information, geographical location information, fuel information, temperature information.
3. system according to claim 2, is characterized in that, described first processing unit carries out analogue simulation process based on described data message and is specially:
Detect based on described data message, if the data of noting abnormalities, point out; If data without exception, carry out data-driven process;
After described data-driven process completes, carrying out calculation process according to the first preset rules to driving the data after processing, generating described trace information, described parameter information.
4. system according to claim 1, it is characterized in that, described system also comprises track record unit, and described track record unit is used for carrying out record to the transportation of system and result, and record is carried out to the running orbit generated, store in the memory unit.
5. system according to claim 1, it is characterized in that, described system also comprises space tracking generation unit, and described space tracking generation unit is used for based on geographical spatial data and track service data span track data, and based on described space trajectory data span running orbit.
6. system according to claim 1, it is characterized in that, described system also comprises parameter evaluation unit, described parameter evaluation unit is used for generating desired guiding trajectory range of information and parameter information scope based on the analogue simulation information of user's input, and the described trace information described desired guiding trajectory range of information and parameter information scope and the first processing unit generated and described parameter information compare, obtain comparison range degree, generate parameter evaluation index based on described comparison range degree.
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| CN201410679078.0A CN104462669A (en) | 2014-11-24 | 2014-11-24 | Flight simulation system |
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| CN201410679078.0A CN104462669A (en) | 2014-11-24 | 2014-11-24 | Flight simulation system |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN108521797A (en) * | 2017-07-27 | 2018-09-11 | 深圳市大疆创新科技有限公司 | Flight simulation control method, server, terminal device |
| CN111475930A (en) * | 2020-03-20 | 2020-07-31 | 中车青岛四方机车车辆股份有限公司 | Fan switching test system and method |
| CN111915933A (en) * | 2020-08-04 | 2020-11-10 | 唐牧 | Method and system for monitoring and managing aircraft flight landing process |
| WO2022056663A1 (en) * | 2020-09-15 | 2022-03-24 | 南京智导智能科技有限公司 | Augmented reality flight simulation system |
| TWI803309B (en) * | 2022-05-05 | 2023-05-21 | 智崴資訊科技股份有限公司 | Construction method of augmented navigation in flight simulation system and its flight simulation system |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108521797A (en) * | 2017-07-27 | 2018-09-11 | 深圳市大疆创新科技有限公司 | Flight simulation control method, server, terminal device |
| CN108521797B (en) * | 2017-07-27 | 2021-04-06 | 深圳市大疆创新科技有限公司 | Flight simulation control method, server and terminal equipment |
| CN111475930A (en) * | 2020-03-20 | 2020-07-31 | 中车青岛四方机车车辆股份有限公司 | Fan switching test system and method |
| CN111915933A (en) * | 2020-08-04 | 2020-11-10 | 唐牧 | Method and system for monitoring and managing aircraft flight landing process |
| WO2022056663A1 (en) * | 2020-09-15 | 2022-03-24 | 南京智导智能科技有限公司 | Augmented reality flight simulation system |
| TWI803309B (en) * | 2022-05-05 | 2023-05-21 | 智崴資訊科技股份有限公司 | Construction method of augmented navigation in flight simulation system and its flight simulation system |
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Application publication date: 20150325 |